JP2014101853A - Various energy storing cycle integrated mechanism - Google Patents

Various energy storing cycle integrated mechanism Download PDF

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JP2014101853A
JP2014101853A JP2012255794A JP2012255794A JP2014101853A JP 2014101853 A JP2014101853 A JP 2014101853A JP 2012255794 A JP2012255794 A JP 2012255794A JP 2012255794 A JP2012255794 A JP 2012255794A JP 2014101853 A JP2014101853 A JP 2014101853A
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blade
bearing load
turbine
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Hiroyasu Tanigawa
浩保 谷川
Kazunaga Tanigawa
和永 谷川
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    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
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    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/40Solar thermal energy, e.g. solar towers
    • Y02E10/46Conversion of thermal power into mechanical power, e.g. Rankine, Stirling or solar thermal engines

Abstract

PROBLEM TO BE SOLVED: To provide a various energy storing cycle integrated mechanism in which existing steam turbine power generation has a half stator vane of zero output to block a steam speed to realize approximate zero output power generation, such as reduction of the steam speed to 1/10 and 43000 times a capacity of maximum speed part water.SOLUTION: A power generation amount is improved to 1/10 or less by having a half stator vane of zero output to block a light steam speed etc. and light object power generation. All rotor blades are doubly inverted by a lateral shaft 1h gear to realize water gravity acceleration power generation in 30 mmHg vacuum in order to achieve Mach 20, and 100 units of water injection turbines 100 are combined to achieve 100 times the existing power generation amount per unit power generation amount in order to achieve bearing load integration of zero. Thereby it is realized that a facility 3D supplies electricity generated by means of a solar heating driven with electricity inexpensive due to zero fuel cost and 1/100 power generation cost etc., a liquid air, and super heated steam heating. Cars, ships, aircrafts, and so on are driven by means of liquid oxygen pressurization to achieve 21/60000 times a capacity compression work rate compared to air compression to realize 1/10 times the fuel cost and 10 times the speed. Aircrafts are aimed to reach to the outer space in 1/500000 the cost and enable day trip etc. anywhere on the earth. An operation margin percentage over all products is aimed to the exceptional and eternal best in the world.

Description

本発明の横型全動翼水重力タービン8B発電やタービン翼8bは、宇宙を重力+引力+超高速度利用で回転する無数の熱効率無限大永久機関に近いと考えて、スペースシャトルの落下速度マッハ22.6に近付ける真空度上昇中の重力加速度利用する、全動翼二重反転比重大物質重力タービン発電も永久機関に近付け、燃料費0地球温暖化防止の横型全動翼水重力タービン8B発電にし、揚水発電との比較では揚水電力は略同じですが発電電力が略速度に比例して、仕事率=kg重m/秒や運動エネルギ=1/2×質量×速度の2乗に比例等から、揚水発電電力は落差×水や水銀等の噴射速度×真空中の比重大物質重力加速度で大増大し、落差10倍×速度10倍で100倍揚水発電電力狙いになり、50サイクル発電や60サイクル発電や比重大物質の直線落下加速に合せた回転速度が必要となるため、サイクル数や比重大物質性質仕事速度や周速度に合せた角度や曲線のタービン翼8bとして、50サイクル発電や60サイクル発電や比重大物質の性質に合せた回転半径のタービン翼8b発電とし、例えば液体噴射速度マッハ3+真空中重力加速度加速でマッハ20狙い水駆動や、超高速円周速度狙う横型全動翼水重力タービン8B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、対向同期歯車4Cや直列同回転歯車4D多数の吸引磁石反発磁石具備歯車滑り面荷重0接近で、対向同期回転や直列同回転を超高速回転大出力狙い、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 horizontal full blade hydro-gravity turbine 8B power generation and turbine blade 8b of the present invention are considered to be close to the infinite number of thermal efficiency infinite permanent engines that rotate the universe by using gravity + attractive force + ultra high speed. Gravity acceleration while raising the degree of vacuum approaching 22.6, using full rotor blade reversal ratio critical material gravity turbine power generation is also approaching the permanent engine, fuel cost is zero horizontal warming blade water gravity turbine 8B power generation preventing global warming In comparison with pumped-storage power generation, the pumped power is almost the same, but the generated power is approximately proportional to the speed, power = kg weight m / sec, kinetic energy = 1/2 x mass x speed squared, etc. Therefore, the pumped-storage power generation is greatly increased by the drop x jet velocity of water or mercury x specific gravity material gravity acceleration in vacuum, and the target is 100 times pumping power generation by 10 times the drop x 10 times the speed. 60 cycle power generation and specific gravity Since a rotational speed that matches the linear fall acceleration of a large material is required, the turbine blade 8b has an angle or curve that matches the number of cycles, specific material properties work speed, or peripheral speed, and 50 cycle power generation or 60 cycle power generation or specific gravity. Turbine blade 8b power generation with a radius of rotation that matches the properties of a large material, for example, liquid jet velocity Mach 3 + horizontal full-wing blade water gravity turbine 8B power generation aiming at Mach 20 with acceleration of gravity acceleration in vacuum and super high speed circumferential velocity The counter repulsive permanent magnet 9B and the attracting permanent magnet 9C make the bearing load close to 0 and the super high speed peripheral speed, and the counter synchronous gear 4C and the series co-rotating gear 4D have a large number of attracting magnet repulsive magnets and the gear sliding surface load approaches the counter synchronous rotation. In addition, the present invention relates to various energy storage cycle coalescence engines and various energy conservation coalescence techniques aiming at super-high-speed rotation and large output.

横型全動翼水重力タービン8B発電電気駆動や電気製造物駆動は、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等高速噴射追加+タービン数無制限落差無制限追加して、例えばマッハ20等狙う水噴射真空中重力加速や、落差500〜828mにタービン100組で1台等既存揚水発電の800倍発電量狙いにし、ボイラや原子炉全廃の燃料費0資源価格0実験が必要な発電として、横型全動翼水重力タービン8B発電電気駆動や電気製造物駆動の、両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近や、内側圧縮翼8q+外側圧縮翼8r+内側出力翼8s+外側出力翼8tの、直線圧縮+直線膨張加速駆動二重反転にした、簡単多段圧縮機3i+液体酸素製造機88pや、簡単ガス機関88qや簡単空気噴射機関88rや簡単噴射機関88s等簡単多段圧縮機3i連結等とし、太陽光加熱器21加熱の空気を圧縮高温として熱回収液体酸素等各種熱製造して、24〜200MPa過熱蒸気50温熱+液体空気28a冷熱に分割保存し、電気+液体空気冷熱+高温水52a〜過熱蒸気50温熱供給設備3Dとして、各種熱利用+液体利用無限用途対応や船舶類や車両類や飛行機類駆動とし、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、簡単ガス機関88qの回転力駆動や、簡単噴射機関88sや簡単空気噴射機関88r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。 Horizontal type full-blade water gravity turbine 8B power generation electric drive and electric product drive are the largest unutilized renewable energy of the earth for existing pumped-storage power generation, additional gravitational acceleration during rising vacuum + addition of high-speed injection such as Mach 3 + unlimited number of turbines For example, Mach 20 and other water jets are targeted for acceleration of gravity in vacuum, and 100 turbines with a head of 500 to 828m, aiming to generate 800 times the power generation of existing pumped-storage power generation. 0 Resource price 0 Power generation that requires experimentation, such as horizontal full-blade hydrogravity turbine 8B power generation electric drive and electric product drive, both sides center support bearing combined load 0 approach + horizontal shaft bearing load 0 approach, inner compression blade 8q + A simple multistage compressor 3i + liquid oxygen production machine 88p or a simple gas machine in which the outer compression blade 8r + the inner output blade 8s + the outer output blade 8t are linearly compressed + linearly expanded and accelerated. 88q, simple air injection engine 88r, simple injection engine 88s and other simple multistage compressors 3i connected, etc., and the solar heater 21 heated air is compressed to high temperature to produce various heat such as heat recovery liquid oxygen, 24-200MPa superheated steam 50 heat + liquid air 28a cold and stored separately, electricity + liquid air cold + high temperature water 52a ~ superheated steam 50 heat supply equipment 3D, various heat use + liquid use infinite use correspondence, ship, vehicle and airplane drive For example, ships, vehicles, airplanes and the like receive liquid oxygen, make the compression volume work rate 21/60000 volume work rate of air compression, make liquid oxygen and water compression pressure 20 times easy, etc. 88q torque drive, simple injection engine 88s and simple air injection engine 88r combined injection propulsion, ship combined injection propulsion 2a natural phenomenon speed up 2a Nitrogen and oxygen in seawater Supplying CO2 Microorganisms and seaweeds will increase, and the food chain will greatly increase food for humans such as fish. Airplanes and ships aim at 10 times speed, and relate to technologies of various energy conservation cycle coalescence engines and various energy conservation 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、横型全動翼水重力タービン8B真空中水重力加速度発電電気製造の、電気+液体空気冷熱+高温水52a〜過熱蒸気50温熱供給設備3Dより供給、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減圧や切削等で、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、液体空気は液体酸素室5Kに液体酸素5Kで受給して液体酸素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に夫々を供給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高圧高温水加熱管5Hの高温水52aを加熱過熱蒸気50にして、液体酸素0でも簡単ガス機関88q等の駆動可能を含めた、両側中心支持軸受荷重合体0接近+内側圧縮翼8q外側圧縮翼8r内側出力翼8s外側出力翼8t+横軸軸受荷重0接近で、超高速二重反転の研究にし、理論燃焼室4Qで超高圧の燃焼ガス49+過熱蒸気50として、過熱蒸気ロケット噴口6Aより噴射燃焼ガス49を吸引噴射し、簡単ガス機関88q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 an enormous amount of fuel due to air compression. Electric + liquid air cold + high-temperature water 52a to superheated steam produced by horizontal full-blade water gravity turbine 8B Supplied from 50D heat supply facility 3D, superheated steam is injected into methane hydrate under permafrost or under the sea floor by depressurization or cutting, methane and water are divided into methane recovered with liquid nitrogen cooled liquid methane, liquid air is liquid oxygen chamber 5K is received as liquid oxygen 5K and compressed into liquid oxygen 5K, the compression volume work rate is set to 21/60000 volume work rate of air compression, 24-200 MPa ultra-high pressure compression injection, liquid oxygen 5K + liquid fuel 1b + high temperature water Fuel injection combustion in the process of heating 52a to an ultra-high pressure in the compression combustion chamber 4Q inner periphery, etc., heating to an ultra-high temperature or optimum temperature, and supplying and injecting each to the combustion chamber 4Q , High-pressure oxygen + ultra-high pressure fuel high-temperature combustion, high-temperature water 52a of high-pressure high-temperature water heating pipe 5H is heated to superheated steam 50, and both sides center support bearing load, including the ability to drive simple gas engine 88q etc. even with liquid oxygen 0 Combining 0 approach + inner compression blade 8q outer compression blade 8r inner output blade 8s outer output blade 8t + horizontal axis bearing load approaching 0, research on ultra-high speed double reversal, super high pressure combustion gas 49 + superheated steam in theoretical combustion chamber 4Q 50, the injection combustion gas 49 is sucked and injected from the superheated steam rocket nozzle 6A, the simple gas engine 88q is driven, various vehicles such as automobiles and tillers, the propeller 7A, the rotor blade 7B and the screw 7C are driven. Driving vehicles, propeller airplanes and screw ships, aiming for fuel costs of 1/10 or 10 times faster by using liquid oxygen 5K for electricity generation electricity generation, the world's best operating profit rate Cormorants, relates to a technology of various energy conservation cycle combined institutions and coalescence method.

既存ジェット機も静翼で塞き止め静翼0出力や静翼等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ているため、空気抵抗01日に地球を16周狙いとし、宇宙ロケットとジェットを合体した液体圧縮の簡単噴射機関88s噴射推進狙いとして、横型全動翼水重力タービン8B発電電気駆動多数の簡単多段圧縮機3i液体酸素製造機88p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+高温水52a〜過熱蒸気50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+高圧高温水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容積仕事率で超高圧圧縮して、夫々を簡単噴射機関88s理論燃焼室4Q内周図に無い等の、燃料加熱管1L高圧高温水加熱管5H酸素加熱管5Fで加熱最適温度にし、図に無い燃料制御弁25b+酸素制御弁24D+過熱蒸気制御弁25を開放して、夫々を1以上の理論空燃比超高圧燃焼狙う開閉弁1Q閉止理論燃焼室4Qに噴射燃焼し、酸素噴射ノズル6L燃料噴射ノズル6X複数燃焼として、過熱蒸気50で熱回収過熱蒸気ロケット噴口6A噴射+燃焼ガス噴射ノズル6Y噴射で、ロケット噴射や吸引噴射等の合体噴射狙いにし、両側中心支持軸受荷重合体0接近+内側圧縮翼8q外側圧縮翼8r内側出力翼8s外側出力翼8t+横軸軸受荷重0接近で、超高速直線二重反転圧縮空気28a+燃焼ガス49超高速直線噴射回転出力にして、ロケット外箱77B内過熱蒸気ロケット噴口6A+燃焼ガス噴射ノズル6Y200MPa狙いロケット噴射では、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 jets are also blocked by the stationary blades, and the stationary blades 0 output and the stationary blades, etc. consume a huge amount of fuel by compressing the air, and the rotational output and the jet propulsion output are negligible. As an aim of propulsion injection of liquid compression simple injection engine 88s combined with space rocket and jet, horizontal full rotor blade water gravity turbine 8B power generation electric drive many simple multistage compressor 3i liquid oxygen production machine 88p, etc. Heat pump 1G + sunlight By heat production of the heater 21, it is divided and stored in high-temperature water of 24-200 MPa to superheated steam temperature 50 + liquid air cooling heat 28a, and as electric + liquid air cooling heat + high temperature water 52a to superheated steam 50 temperature supply equipment 3D, propulsion of airplane injection Is received with liquid oxygen 5K + liquid fuel 1c + high-pressure high-temperature water 52a, and the compression volumetric power exceeds 21/60000 volumetric power of air compression by liquid oxygen compression. Fuel compression valve 25b + which is compressed and compressed to an optimum heating temperature by the fuel heating pipe 1L high pressure high temperature water heating pipe 5H oxygen heating pipe 5F, such as the simple injection engine 88s in the theoretical combustion chamber 4Q inner circumference view, etc. The oxygen control valve 24D + superheated steam control valve 25 is opened, and each of them is injected and burned into the open / close valve 1Q closed theoretical combustion chamber 4Q aiming at one or more stoichiometric air-fuel ratio ultra-high pressure combustion, as oxygen injection nozzle 6L fuel injection nozzle 6X multiple combustion With the superheated steam 50, heat recovery superheated steam rocket nozzle 6A injection + combustion gas injection nozzle 6Y injection, aiming for combined injection such as rocket injection and suction injection, both sides center support bearing load combined 0 approach + inner compression blade 8q outer compression blade 8r inner output wing 8s outer output wing 8t + horizontal axis bearing load close to 0, ultra high speed linear contra-rotating compressed air 28a + combustion gas 49 ultra high speed linear injection rotation output, outside rocket With 77B superheated steam rocket nozzle 6A + combustion gas injection nozzle 6Y 200MPa target rocket injection, aiming for space arrival cost of 1 / 500,000 and making 16 orbits of the earth a day in space flight near zero fuel cost The present invention relates to various energy conservation cycle coalescence engines and coalescence techniques that enable day trips anywhere and aim at the world's best profitability with various space return planes.

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容積仕事率を含有にして、液体酸素製造機88pの空気圧縮機も理論簡単の簡単多段圧縮機3i使用追加とし、横型全動翼水重力タービン8B発電電気駆動1〜複数段簡単多段圧縮機3i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、高圧高温水加熱管5H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+高温水52a〜過熱蒸気50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、図に無い液体酸素制御弁5T+液体燃料制御弁1K+水制御弁5Qを開放して、簡単空気噴射機関88r理論燃焼室4Q内周で夫々最適温度に加熱し、両側中心支持軸受荷重合体0接近+内側圧縮翼8q外側圧縮翼8r内側出力翼8s外側出力翼8t+横軸軸受荷重0接近の簡単空気噴射機関88rや簡単ガス機関88q夫々を駆動して、簡単空気噴射機関88rの水吸引噴射推進や簡単ガス機関88q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、スクリュウ推進簡単ガス機関88q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. / The addition of 60000 volumetric power, the air compressor of the liquid oxygen production machine 88p is also added to the use of simple multistage compressor 3i, which is theoretically simple, horizontal all-blade water gravity turbine 8B power generation electric drive 1 to multistage simple multistage compression As the heat pump 1G compression of the machine 3i, etc., the solar heater 21 is made into a heat production in which the solar heating air is compressed to a high temperature, and the high pressure high temperature water heating pipe 5H is recovered and stored separately. Liquid oxygen 5K + liquid fuel 1c + high temperature water 52a is received as electricity + liquid air cold heat + high temperature water 52a to superheated steam 50 heat supply equipment 3D. The target is about 200 MPa pump compression, and the liquid oxygen control valve 5T + liquid fuel control valve 1K + water control valve 5Q (not shown) are opened and heated to the optimum temperature on the inner periphery of the simple air injection engine 88r theoretical combustion chamber 4Q. Easy air injection by driving the simple air injection engine 88r and the simple gas engine 88q approaching the center support bearing load combined 0 approach + inner compression blade 8q outer compression blade 8r inner output blade 8s outer output blade 8t + horizontal shaft bearing load 0 approach. The engine 88r water suction injection propulsion and the simple gas engine 88q screw 7C rotation propulsion, with the aim of 10 times the existing ship speed and 1/10 fuel cost, the screw propulsion simple gas engine 88q exhaust is the bottom bottom exhaust injection propulsion. Accelerate natural phenomena in the course of friction-reducing jet propulsion and supply oxygen, nitrogen, CO2, etc. into the sea, microbial, phytoplankton, seaweed and sun The fish and the like to increase the food of growth humanity, aiming profit margin preeminent world, relates to a technology of various energy conservation cycle combined institutions and coalescence method.

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、横型全動翼水重力タービン8B仕事率の1/1700と僅少に加えて、蒸気速度を堰止めて0出力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、発電熱量全部で海水温度を7度上昇し、海面全部を温度上昇自然現象不可能にして、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 the 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 a little less than 1/1700 of the horizontal all blade water gravity turbine 8B power, The steam speed is stopped and the stationary vanes with zero output are alternately half-damped with the moving blades, the steam speed is approaching 1/100, the seawater temperature is increased by 7 degrees with the total amount of generated heat, and the entire sea surface The natural phenomenon of temperature rise is made impossible, abnormal weather without an upper limit is increased, and the danger of human beings approaching extinction due to heavy rain of seawater around 50 to 100 years is increasing. 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1700倍水仕事率にして、真空中水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17倍仕事率発電ですが、高さ500m以上に100組で1700倍発電量等膨大な発電量が予想され、水資源は膨大で深層海洋水を使用すると公知の副産物も多く、熱帯地方の海水使用にすると膨大な蒸留水製造になる等、更に実験が必要な真空中水重力加速度マッハ20狙い燃料費0発電の無限大発電にし、横型全動翼水重力タービン8B発電円筒タービン翼群8A水平軸板16精密組立容易にして、円筒組立固定の円筒タービン翼群8Aを含めて全自動加工容易や組立容易にし、全自動加工100組組立で1700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20狙いの水重力エネルギで駆動し、安価大量の水資源による燃料費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、水重力タービン8R燃料費0発電電気駆動の、1〜複数段簡単多段圧縮機3i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に分割保存した、電気+液体空気冷熱+高温水〜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短時間1/10燃料費駆動や10倍速度駆動にして、宇宙飛行や空気浮上船舶等や、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 / sec, are set to 1700 times the water power of the existing steam turbine power generation, and the water gravity acceleration power generation in the vacuum, the same speed 1/100 volumetric power is obtained. It is expected to generate a huge amount of power generation such as 1700 times power generation in 100 pairs at a height of 500m or more, water resources are enormous, and there are many known by-products when using deep ocean water, The use of seawater makes enormous amounts of distilled water. For example, in-vacuum water gravity acceleration Mach 20 requires further experimentation, and the fuel cost is 0. The horizontal axis plate 16 facilitates precision assembly, facilitates fully automatic processing including the cylindrical turbine blade group 8A fixed to the cylindrical assembly, and facilitates assembly. Driven by water gravity energy aimed at gravity acceleration acceleration Mach 20 in vacuum, shifted to expanding the use of low-cost electricity with zero fuel cost power generation by a large amount of cheap water resources, solar heating the air by solar heater 21, Water gravity turbine 8R Fuel cost 0 Power generation Electric drive, 1 to multi-stage simple multi-stage compressor 3i, etc. Compressed multiple times with heat pump 1G, 24 to 200MPa hot water 52a to superheated steam temperature 50 + liquid air cold heat 28a is divided and stored, supplied from electricity + liquid air cold heat + hot water to superheated steam temperature heat supply equipment 3D, and received in the liquid oxygen chamber 5K, storage battery, etc., for a short time 1 / 10 Background of the fuel cost drive and 10x speed drive, space flight, air flotation ship, etc., storage battery drive and electric drive of extremely inexpensive power generation, and prevention of global warming with little CO2 exhaust A.

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。そこで例えば横型全動翼水重力タービン8B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、複数段簡単多段圧縮機3i+液体酸素製造機88p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、液体空気合体駆動の自動車や船舶や宇宙往還機全盛として宇宙到達費用1/50万狙いにし、船舶駆動の過程では自然現象高速化2aして、微生物や海草類やサンゴ等を増殖食物連鎖等で魚類等人類の食物を増大し、海水の豪雨を阻止して人類絶滅を先送り出来る背景があり。燃料費僅少で10倍速度狙いの船舶革命や飛行機革命となって、運用利益率が既存運用利益率の10倍等膨大となり、世界規模100%独占した製造運用とし、雇用を増大する雇用増大革命に出来る背景がある。 In high school and university, the existing engine is described as the best engine, and when we return to elementary school science without brainwashing and think about the best engine, the unit of work is kg weight m / sec. The engine is the best engine in terms of generating rotational output at a high speed, but there is no trace of thought. Therefore, for example, if the horizontal full-blade hydrogravity turbine 8B power generation is used, there is a background that the fuel cost is low and the power generation is cheap. Zero heating is the best. Therefore, the fuel cost 0 power generation electric drive solar heater 21 is used, and the solar heating air 28a is compressed a plurality of times by a fuel stage 0 power generation electric drive, a multistage simple multistage compressor 3i + a liquid oxygen production machine 88p, and a plurality of times. Collected and stored in cold liquid oxygen 5K and liquid nitrogen 5L + hot high-temperature water 52a to superheated steam 50, and injecting superheated steam 50 into methane hydrate under permafrost, for example, in the process of infinite use of heat Methane is recovered with liquid nitrogen-cooled liquid methane and superheated steam injection is continued forever, and the methane recovery enclosure is made to graze pasture with appropriate temperature and many water droplets, increasing the use of human food and increasing heat The aim is to reach 1 / 500,000 as the cost of reaching the universe as an automobile, ship and spacecraft that is driven by liquid-air coalescence. In the process of driving the ship, the natural phenomenon is accelerated 2a, and microorganisms, seaweeds, corals, etc. The food of fish such as the human race increased in 殖食 products 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. 11986119, 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2012−234242号出願日平成24年10月24日まで48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 48 applications including PCT up to October 24, 2012, the filing date of Japanese Patent Application No. 2012-234242.

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南海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 To make the ocean floor rock expansion earthquake and tsunami huge, the Tonankai earthquake and tsunami also become huge, increase the risk of human extinction, prevent heavy rain in seawater, prevent sea warming such as seawater temperature rise 0, 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.

横型全動翼水重力タービン8B燃料費0発電安価電気駆動全部にして、太陽光加熱器21+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近とした、簡単多段圧縮機3i+液体酸素製造機88p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ロケット燃焼理論燃焼室4Qとして、過熱蒸気50〜高温水52aと熱交換加熱することで理論空燃比燃焼を可能にし、ロケット燃焼と既存技術改良発明と合体にして、合体理論燃焼室4Q駆動両側中心支持軸受荷重合体0接近+内側圧縮翼8q外側圧縮翼8r内側出力翼8s外側出力翼8t+横軸軸受荷重0接近の、簡単ガス機関88qや簡単空気噴射機関88rや簡単噴射機関88s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短時間ロケット噴射で急速浮上推進や自然現象高速化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、飛行機も短時間ロケット噴射で宇宙飛行全盛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。 Horizontal full blade hydrogravity turbine 8B fuel cost 0 power generation low cost electric drive all, solar heater 21 + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + horizontal Heat is produced by a simple multistage compressor 3i + liquid oxygen producing machine 88p with a shaft bearing load approaching zero, and the supplied liquid oxygen 5K is compressed into air as electricity + liquid air cold heat + high temperature water to superheated steam temperature heat supply equipment 3D. As the rocket combustion theoretical combustion chamber 4Q, which has a compression work rate of 21/60000 volumetric compression and easy for ultra high pressure combustion and ultra high temperature combustion, heat exchange heating with superheated steam 50 to high temperature water 52a enables theoretical air-fuel ratio combustion. Combined with rocket combustion and existing technical improvement invention, coalescence theoretical combustion chamber 4Q drive both sides center support bearing load coalescence 0 approach + inner compression blade 8q outer compression blade 8r inner output blade 8s outer output blade 8t A simple gas engine 88q, a simple air injection engine 88r, and a simple injection engine 88s that approach zero on the horizontal axis bearing load are used to drive vehicles, such as automobiles, ships, and airplanes, and to drive and inject vessels. In driving, quick levitation propulsion and natural phenomenon acceleration 2a are performed by short-time rocket injection, supplying oxygen, nitrogen, CO2 etc. into the sea, increasing microorganisms, phytoplankton, seagrass, coral, fish, etc., and increasing human food The airplane also makes 16 rounds of the Earth a day in a cosmic flight with a short rocket injection, making it a day trip anywhere on the earth and aiming for a little CO2 exhaust in the atmosphere. Power generation, ships, airplanes, automobiles, etc., making it the best in the world with outstanding profitability and the best in new employment, and increasing droughts, torrential rains, typhoons, seasonal winds, heavy rains in seawater, and earthquake tsunamis Sealed and, to put off the human race extinct prevent global warming.

横型全動翼水重力タービン8B燃料費0安価発電の、対向同期歯車4Cにより対向同期回転にして、直列同回転歯車4Dで100組等同速度回転にする効果が非常に大きく、円筒タービン翼群8A1種類を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の羅列に近い竪型全動翼水重力タービン8M発電を、最大速度の最終動翼群と同真空駆動で比較説明すると、大気圧100℃760mmHgで水の1700倍容積の水蒸気は、排気温度29℃真空度30mmHgでボイルの法則により、760mmHg×1700=30mmHg×V2倍容積の水蒸気となり、V2=760/30×1700=水の43000倍容積水蒸気となり、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20狙いで更に30倍発電量が狙える等、実験結果が正解ですが発電原価を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。 Horizontal type full-blade hydrogravity turbine 8B Fuel cost 0 Low cost power generation The counter synchronous rotation by the counter synchronous gear 4C, and the effect of rotating the same speed by the same series gear 4D, such as 100 sets, is very large. Cylindrical turbine blade group 8A1 100 types of fully automatic manufacturing of 100 types, the effect of 100 sets manufacturing is very large, the effect of simplifying the structure without the need of a boiler or nuclear reactor is also very large, and a vertical type close to the enumeration of the last moving blade group of existing steam turbines Comparing and explaining the total blade hydrogravity turbine 8M power generation with the same maximum speed as the last blade group, the steam of 1,700 times the volume of water at an atmospheric pressure of 100 ° C. and 760 mmHg is boiled at an exhaust temperature of 29 ° C. and a vacuum degree of 30 mmHg. Is 760 mmHg × 1700 = 30 mmHg × V2 volume water vapor, V2 = 760/30 × 1700 = water 43,000 times volume water vapor, 100 will be 430 times the amount of power generation by volume water 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 20 is aimed at, and the experimental result is correct, such as aiming for 30 times the amount of power generation, but it has the effect of greatly reforming the power generation cost to 1/10 etc. and infinitely increasing the employment of electrical products.

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の増大として、理論燃焼室4Qにより両側中心支持軸受荷重合体0接近+内側圧縮翼8q外側圧縮翼8r内側出力翼8s外側出力翼8t+横軸軸受荷重0接近の、簡単ガス機関88qや簡単空気噴射機関88rや簡単噴射機関88sを、最も効率良く超高速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を簡単ガス機関88q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, etc. 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 increases the number of super high pressure superheated steam 50 in the vicinity of the center of the theoretical combustion chamber 4Q. As a result of the theoretical combustion chamber 4Q, the both side center support bearing load merge 0 approach + outer compression blade 8q outer compression blade 8r inner output blade 8s outer The simple gas engine 88q, simple air injection engine 88r, and simple injection engine 88s approaching the output vane 8t + horizontal shaft bearing load close to 0 have the effect of being able to drive the super-high speed most efficiently. In addition to the effect of aiming at 10 times speed, etc., it has the effect that the space arrival cost can be aimed at 1 / 500,000 of the existing space rocket, and the wheel, screw 7C, propeller 7A, etc. The blade 7B is driven by a simple gas engine 88q to drive the rotational force of ships, airplanes, automobiles, etc., and the ship injection propulsion drive speeds up natural phenomena 2a, and digestion capacity of CO2 etc. of underwater microorganisms is tens of thousands times that of forests Greatly aimed at increasing effects, such as phytoplankton, seaweeds, corals, etc., greatly increasing fish and other marine foods in the food chain, etc. It is effective to prevent the enormous increase in humanity, postpone the most important human race extinction, and aim for the best profit rate in the world.

飛行機駆動は、燃料費0横型全動翼水重力タービン8B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3Dより液体酸素+高温水を受給し、理論燃焼室4Q内周の高温水加熱管5H等で超高圧水や超高圧燃料等を最適加熱して、燃料噴射ノズル6X+酸素噴射ノズル6L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+酸素+高温水加熱管5Hを最適加熱し、超高圧高温過熱蒸気50等に加熱するロケット燃焼理論燃焼室4Qとして、既存技術改良発明の理論燃焼室4Q複数個所合体とし、大幅に簡単とした両側中心支持軸受荷重合体0接近+内側圧縮翼8q外側圧縮翼8r内側出力翼8s外側出力翼8t+横軸軸受荷重0接近の、簡単噴射機関88s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、過熱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やマッハ20等の帰還速度は最悪と考え、帰還速度はマッハ3以下として宇宙上昇時には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49+高圧高温過熱蒸気50のロケット噴射量増大にして、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。 Plane drive receives liquid oxygen + high temperature water from electricity + liquid air cold heat + high temperature water to superheated steam temperature heat supply equipment 3D of fuel drive 0 horizontal all blade water gravity turbine 8B power generation electric drive, inside theoretical combustion chamber 4Q The super high pressure water or super high pressure fuel is optimally heated by the surrounding high-temperature water heating pipe 5H, etc., and the fuel injection nozzle 6X + oxygen injection nozzle 6L is opened, and oxygen gas + fuel gas is mixed and ignited near the center of the multiple injection ignition combustion. As a rocket combustion theoretical combustion chamber 4Q that optimally heats the fuel + oxygen + high-temperature water heating pipe 5H in the inner periphery of the theoretical combustion chamber 4Q and heats it to the super-high pressure / high temperature superheated steam 50, etc. Drive the simple injection engine 88s, which is a single united unit, which is substantially simplified on both sides center support bearing load uniting 0 approach + inner compression blade 8q outer compression blade 8r inner output blade 8s outer output blade 8t + horizontal shaft bearing load approaching 0 It has the effect of targeting the space arrival cost at 1 / 500,000 that of an existing space rocket and aiming to make the best use of space with the same fuel cost 10 times the injection propulsion output. For example, the injection propulsion output is 100 times the pressure of existing jets 10 times the calorie injection short Aiming at 1000 times the time of propulsion propulsion output, in the atmosphere, propeller flight, rotor blade flight and injection propulsion aiming at low fuel cost, and superheated steam injection speed and combustion gas injection speed are the largest in vacuum, so a lot of existing space rockets above ground The return speed of injection and Mach 20 is considered the worst, the return speed is Mach 3 or less, and the rocket injection amount of high-pressure high-temperature combustion gas 49 + high-pressure high-temperature superheated steam 50 of 24-200MPa from the vicinity of the highest flight altitude of the existing aircraft when the space rises In other words, it is possible to aim for a prime use of space that allows a day trip anywhere on the earth, such as making 16 orbits of the earth a day.

横型全動翼水重力タービン8Bの4C4Dの説明図(実施例1)Explanatory drawing of 4C4D of horizontal type full-blade water gravity turbine 8B (Example 1) 横型全動翼水重力タービン8Bの8A8b9C9Bの説明図(実施例2)Explanatory drawing (Example 2) of 8A8b9C9B of the horizontal type | mold whole blade water gravity turbine 8B 太陽光加熱器21の説明図(実施例3)Explanatory drawing of the solar heater 21 (Example 3) 液体酸素製造機88pの説明図(実施例4)Explanatory drawing of the liquid oxygen production machine 88p (Example 4) 簡単多段圧縮機3iの説明図(実施例5)Explanatory drawing of simple multistage compressor 3i (Example 5) 簡単ガス機関88qの説明図(実施例6)Explanatory drawing of simple gas engine 88q (Example 6) 簡単空気噴射機関88rの説明図(実施例7)Explanatory drawing of the simple air injection engine 88r (Example 7) 簡単噴射機関88sの説明図(実施例8)Explanatory drawing of the simple injection engine 88s (Example 8) 簡単ガス機関自動車7Iの説明図(実施例9)Explanatory drawing of simple gas locomotive car 7I (Example 9) 簡単ガス機関船舶7Jの説明図(実施例10)Explanatory drawing of simple gas engine ship 7J (Example 10) 簡単ガス機関飛行機7Kの説明図(実施例11)Illustration of Simple Gas Engine Airplane 7K (Example 11) 簡単空気噴射機関船舶7Lの説明図(実施例12)Explanatory drawing of the simple air injection engine ship 7L (Example 12) 簡単噴射機関飛行機7Mの説明図(実施例13)Explanatory drawing of the simple injection engine airplane 7M (Example 13) 回転翼飛行機7Nの説明図(実施例14)Explanatory drawing of rotary wing airplane 7N (Example 14) 回転翼噴射飛行機7Oの説明図(実施例15)Explanatory drawing of the rotary wing jet airplane 70 (Example 15) 特大オスプレイ7Pの説明図(実施例16)Illustration of extra large Osprey 7P (Example 16) 大型オスプレイ7Qの説明図(実施例17)Illustration of Large Osprey 7Q (Example 17)

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発電利用が阻止され、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、出力0の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、横型全動翼水重力タービン8B以外を3種類実施例で代用説明して、磁気軸受等既存技術使用は常識を省略した発明の具体化に挑戦し、真空中の重力加速度発電電気製造物駆動の、両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近の、簡単多段圧縮機3i+液体酸素製造機88pや、簡単ガス機関88qや簡単空気噴射機関88rや簡単噴射機関88s駆動の、自動車類や船舶類や飛行機類にします。   The use of gravity acceleration power generation in a vacuum for a long period of time with brainwashing such as existing steam turbine power generation is blocked, and the target of 43,000 times the power generation amount of one existing steam turbine power generation is blocked by one unit of 100 sets, for example, the existing best steam turbine The power generation pressure, the same speed, the same volumetric power, kg weight m / sec, are reduced to 1/1700 of the water power, and the stationary vanes with output 0 are alternately arranged with the moving blades to dam and close the rotation output to 0. The total heat generated by the steam turbine power generation increases by 7 degrees in the seawater temperature, the fish drastically decreases, the bottom bedrock expands into earthquakes and tsunamis, and the typhoons, seasonal winds, and tornadoes in the sea around Japan become huge around 20 years 100 m / s For example, there is a risk of drastic reduction of food and human extinction by providing salt coating on land around 50 to 100 years, such as heavy rain of suctioned seawater expected over the sea. That is, since the invention becomes too large due to many fatal drawbacks of the existing technology, the invention is described in the explanation of the reference numerals, and the parts that have been repeatedly described in the previous application are omitted, and the parts other than the horizontal type full-blade water gravity turbine 8B are omitted. Substituting explanation in the type embodiment, the use of existing technology such as magnetic bearings challenged the realization of the invention omitting common sense, driven by gravity acceleration power generation electrical product drive in vacuum, both sides center support bearing combined load 0 approach + side Simple multi-stage compressor 3i + liquid oxygen production machine 88p approaching zero shaft bearing load, simple gas engine 88q, simple air injection engine 88r and simple injection engine 88s driven cars, ships and airplanes.

図1真空中重力加速度+水噴射速度でマッハ30駆動等極限狙う、横型全動翼水重力タービン8B発電は、発電量がkg重m/秒に比例するため、図2円筒タービン翼群8A両側や中央等複数個所に反発永久磁石9B吸引永久磁石9Cを具備し、円筒タービン翼群8A側をリング型内周1極外周1極着磁として、タービン外箱77a側をリング型内周2極の上側吸引永久磁石9C下側反発永久磁石9Bとし、複数箇所具備で回転部重量を反発力や吸引力により0に近付け軸受荷重を0接近にして、超高速タービン周速度記録更新狙いにし、真空中水重力加速度マッハ30タービン駆動接近狙いにして、水平軸16Aを水平軸板16で固定回転速度や回転外径の無限増大狙いにし、1種類を2個製造1組として100組の対向直列全動翼弾み車タービン製造として、又は1種類を1組として200組の直列全動翼弾み車タービンや食込直列全動翼弾み車タービンとし、全自動鋳造や全自動加工等で夫々垂直に100〜200組具備の1台製造にして、既存最高建築物高さ垂直828mに100組等具備して1台具備とし、比重大物質上昇装置2Fにより水3Eを垂直等に50〜828m等上昇して、比重大物質加速機6Wで水3Eをマッハ28噴射狙い噴射し、重力加速度加速真空加速駆動して円筒タービン翼群8Aを対向同期歯車4Cにより対向同期回転にして、直列同回転歯車4Dで100組等同速度同方向回転にし、4C4D歯車に多数の吸引磁石反発磁石具備歯車滑り面荷重0接近超高速回転大出力で、安価大量生産容易とボイラや原子炉不要にして、水を真空加速する重力加速部1gをタービン8R上部等に夫々具備し、発電機1は対向同期歯車4C主軸や直列同回転歯車4D主軸に選択具備して、タービン外箱77a外で100組以上駆動発電原価を1/10狙いとし、構造極端に簡単極端に安価な電気製造物駆動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 Horizontal full-blade hydrogravity turbine 8B power generation aiming at the limit such as Mach 30 drive with gravity acceleration in water + water injection speed, because the power generation amount is proportional to kg weight m / sec, both sides of cylindrical turbine blade group 8A in Fig. 2 And repulsive permanent magnets 9B attracting permanent magnets 9C at a plurality of locations such as the center, and the cylindrical turbine blade group 8A side as a ring type inner periphery 1 pole outer periphery 1 pole magnetization, and the turbine outer box 77a side as a ring type inner periphery 2 poles The upper attraction permanent magnet 9C is the lower repulsion permanent magnet 9B, and the weight of the rotating part is made close to 0 by the repulsive force or the attraction force at multiple locations, the bearing load is made close to 0, and the aim is to update the super high speed turbine peripheral speed record. Middle water gravity acceleration Mach 30 Aiming at turbine drive approach, aiming at infinite increase of fixed rotation speed and rotation outer diameter with horizontal axis plate 16 with horizontal axis 16A, one type is manufactured 2 sets, 100 sets of opposed series all Moving blade -Bin manufacturing or 200 types of series full blade impeller turbines and bite in series full blade impeller turbines, one set of one type, and 100 to 200 sets vertically each with fully automatic casting and fully automatic processing, etc. 100 units, etc., are installed in the existing highest building height of 828m vertical, and one unit is built, and the specific material riser 2F raises the water 3E vertically by 50-828m, etc. The machine 6W jets water 3E aiming at Mach 28 injection, gravity acceleration acceleration vacuum acceleration drive, the cylindrical turbine blade group 8A is counter-synchronously rotated by the counter-synchronous gear 4C, and 100 sets of the same speed and the same speed in the same direction and the same speed by the series co-rotating gear 4D Gravity to rotate the 4C4D gear with a large number of attracting magnet repulsion magnets, gear sliding surface load close to 0, ultra high speed rotation, high output, easy mass production at low cost and no need for boilers or reactors, and vacuum acceleration of water The speed unit 1g is provided in the upper part of the turbine 8R, etc., and the generator 1 is selectively provided as the counter synchronous gear 4C main shaft or the series co-rotating gear 4D main shaft. With 10 targets, the structure is extremely simple and extremely inexpensive, and the electric product drive infinity and electric drive infinity are used to make the world's best energy conservation cycle coalescence engine power generation and coalescence method power generation with outstanding profitability.

横型全動翼水重力タービン8B発電タービン翼8bは、50サイクル発電や60サイクル発電や比重大物質性質仕事速度や周速度に合せた、角度や曲線や回転半径のタービン翼8b対向同期歯車4C等とし、超高速噴射速度で回転駆動させる、例えば液体噴射速度マッハ3+真空中重力加速度加速でマッハ20狙い水駆動の、タービン翼8b円筒タービン翼群8Aとして、タービン外箱77a内に既存最高建築物828mに100組等垂直具備で1台とし、比重大物質加速器6Wによる水噴射速度+真空中重力加速度加速でマッハ28狙いとして、円筒タービン翼群8Aに噴射し、横型全動翼水重力タービン8B駆動発電してマッハ28速度狙いを維持して、次のタービンを駆動して落差を有効利用する横型全動翼水重力タービン8B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組使用等選択とし、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倍容積水蒸気として、100組重ねた1台のタービン8T発電量と比較説明すると、1/1000容積の水をマッハ1速度噴射で43×100=4300倍水発電量となり、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。 Horizontal full-blade water gravity turbine 8B power generation turbine blade 8b is a turbine blade 8b facing synchronous gear 4C having an angle, a curve, or a rotating radius in accordance with 50 cycle power generation, 60 cycle power generation, specific critical material property work speed or peripheral speed, etc. As a turbine blade 8b cylindrical turbine blade group 8A, which is driven to rotate at an ultra-high-speed injection speed, for example, a liquid injection speed Mach 3 + accelerated gravity acceleration acceleration in vacuum and Mach 20 aiming water, the existing highest building in the turbine outer casing 77a. 100 units in 828m, one vertical unit, one unit, water injection speed by specific material accelerator 6W + gravity acceleration in vacuum, Mach 28 aimed at Mach 28 and injected into cylindrical turbine blade group 8A, horizontal full blade water gravity turbine 8B Driven power generation to maintain the target of Mach 28 speed and drive the next turbine to effectively use the head to generate a horizontal full-blade water gravity turbine 8B , Friction heat cooling and air extractor 51 makes it easy to exceed the existing power generation maximum vacuum degree such as 30mmHg, etc., and select 100 sets for drop 828m, etc. As a volumetric water vapor, when compared with the power generation amount of one turbine 8T in which 100 sets are stacked, the water power generation amount is 43 × 100 = 4300 times by Mach 1 speed injection of 1/1000 volume of water. The energy saving cycle combined engine fuel cost becomes 0 extremely low power generation.

図2の横型全動翼水重力タービン8B超高速周速度発電は、円筒タービン翼群8A両側や中央等複数個所に反発永久磁石9B吸引永久磁石9Cを具備し、円筒タービン翼群8A側をリング型内周1極外周1極着磁として、タービン外箱77a側をリング型内周2極の上側吸引永久磁石9C下側反発永久磁石9Bとし、複数箇所具備で回転部重量を反発力や吸引力により0に近付け軸受荷重を0接近にして、超高速タービン周速度記録更新狙いにし、円筒タービン翼群8Aで最も重要な構成は超撥水性として、摩擦損失を最低が最重要なため、耐摩耗の撥水鍍金3a容易や運転停止時の撥水コーティング3b容易な構成とし、内筒面全面切削で軽量化して大径にする、円筒タービン翼群8A両側に水平軸16Aを水平軸板16で固定1種類として、横型全動翼水重力タービン8B簡単製造や全自動加工や精密組立容易とし、可能な限り実験最大径として垂直828mに100組製造等で1台製造として、水平軸16Aに対向同期歯車4Cを具備することで横型全動翼対向水重力タービン8Tとし、対向同速度同期回転にして直列同回転歯車4Dで連結することで同方向同速度回転にして、横型全動翼対向直列水重力タービン8Tや、横型全動翼直列水重力タービン8Tや、横型全動翼食込直列水重力タービン8Tとし、熱帯砂漠地帯等蒸留水最大量生産する場合は、比重大物質加速機6W具備を1組毎に近付けた水3E噴射として、蒸留水製造量や摩擦熱気化水の冷却量に合せた比重大物質加速機6W具備量とし、水平軸16Aに発電機1を具備してタービン外箱77aの外で100組以上駆動発電にして、構造極端に簡単やボイラや原子炉不要等で製造原価を極端に安価とし、運用利益率も燃料消費0等比較物皆無の抜群世界一にする、横型全動翼水重力タービン8B極端に安価発電にする。   2 has a repulsive permanent magnet 9B attracting permanent magnet 9C at a plurality of locations such as both sides and the center of the cylindrical turbine blade group 8A, and the cylindrical turbine blade group 8A side is a ring. The inner periphery 1 pole outer periphery 1 pole magnetization, the turbine outer box 77a side is an upper attracting permanent magnet 9C lower repulsion permanent magnet 9B of the ring inner periphery 2 poles, and there are a plurality of locations, and the weight of the rotating part is repulsive or attracted. The bearing load is brought close to 0 by force, aiming to update the super high speed turbine peripheral speed record, the most important configuration in the cylindrical turbine blade group 8A is super water repellency, and the lowest friction loss is the most important. The horizontal shaft 16A is arranged on both sides of the cylindrical turbine blade group 8A so that the water repellent plating 3a is easy to wear and the water repellent coating 3b is easy when the operation is stopped. With one fixed type The horizontal fully moving water-gravity turbine 8B is easy to manufacture, fully automatic, and easy to assemble. As much as possible, 100 units can be manufactured as a vertical diameter of 828m, and one unit can be manufactured. By providing a horizontal all-blade opposed water-gravity turbine 8T, it is counter-rotating at the same speed synchronous rotation and connected in series and co-rotating gear 4D to be rotated in the same direction and at the same speed, so Or a horizontal all-blade series water gravity turbine 8T or a horizontal all-blade bite-in series water gravity turbine 8T. When producing the maximum amount of distilled water in tropical deserts, etc. As the water 3E injection approached, the specific material accelerator 6W equipped in accordance with the amount of distilled water produced and the amount of cooling of frictional heat vaporized water, the generator 1 on the horizontal shaft 16A and the outside of the turbine outer box 77a At 100 Horizontal power blade hydrogravity with a driving power generation system that makes it extremely easy to construct, makes boilers and nuclear reactors unnecessary, makes manufacturing costs extremely cheap, and makes the operating profit rate unsurpassed in the world, with no fuel consumption and other comparisons. Turbine 8B extremely low power generation.

図3の太陽光加熱器21の熱製造は、横型全動翼水重力タービン8B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図に無い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、簡単多段圧縮機3i液体酸素製造機88p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。 The heat production of the solar heater 21 of FIG. 3 is to make the horizontal full-blade water gravity turbine 8B fuel cost 0 power generation extremely cheap electric drive, cheap electricity + liquid air cold heat + superheated steam temperature supply equipment 3D. The solar heater 21 has a buoyancy on the water surface or is provided with a circular railroad on a flat surface, and the solar heater 21 is used as a water device or land device not shown in the figure for maintaining and rotating the 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 multi-stage heat pump 1G for suction, simple multi-stage compressor 3i liquid oxygen production machine 88p and the like as heat pump 1G are set to 800 to 1200 ° C. multiple times and compressed by 1 to multi-stage compression heat recovery unit 2C Each heat recovery is repeated, and the cold air of the liquid air 28a is stored in the liquid oxygen chamber 5K + the liquid nitrogen chamber 5L. Divided and stored in room 5N, used as electric + liquid air cold heat + superheated steam heat supply facility 3D for various purposes, and used as an electric drive prime and storage battery drive prime, various hot and cold use prime of electric products and various cold use prime To.

図4の液体酸素製造機88pは、両側中心支持軸受荷重合体0接近+内側圧縮翼8q外側圧縮翼8r内側出力翼8s外側出力翼8t+横軸軸受荷重0接近とし、超高速二重反転直線圧縮翼や直線膨張出力翼の回転速度や周速度や回転半径に合せた、回転半径角度や曲線とした圧縮翼や出力翼にする、長大高速二重反転容易とした液体酸素製造機88pは、、横軸1h二重反転にすることで圧縮翼や出力翼を簡単環状部品の嵌合組立部9M組立として、全自動大量製造容易や全自動加工容易や組立容易や部品数1/100狙い、簡単多段圧縮機3i連結狙いとし、横型全動翼水重力タービン8B燃料費0発電極端に安価電気駆動等として、複数段圧縮の場合は簡単多段圧縮機3iと連結駆動圧縮とし、1〜複数段圧縮の場合は簡単圧縮機3sの水冷却+水噴射圧縮空気多段冷却とした、太陽光加熱器21の熱製造加熱空気28aを圧縮熱回収として、高圧高温水加熱管5H温熱製造+精留塔排ガス管5h冷却で液体酸素+液体窒素等製造準備し、超高圧圧縮空気28aを空気タービン3uに超高速噴射二重反転駆動して、軸受荷重合体0接近超高速回転の大回転出力を発生することで、電動機駆動電力の大幅低減として排気を精留塔に供給し、既存技術と同様に液体酸素+液体窒素等に精製して排気を精留塔排ガス管5hに供給して、液体酸素製造機88pの駆動を継続温熱+冷熱の大量生産にし、電気+液体空気冷熱+高温水〜過熱蒸気温熱の供給設備3Dに供給して、例えば温熱供給では海底や永久凍土地下のメタンハイドレートに注入メタンを回収し、永久凍土地下のメタン回収は透明な囲いを突設して比重差利用最上部先端から回収として、囲い内を永遠の温室牧草地放牧として食肉製造等無限に近い各種温熱利用全盛狙いにし、液体酸素供給では圧縮仕事率を空気圧縮の21/60000容積圧縮仕事率の、液体酸素駆動との合体とした、簡単ガス機関88q駆動や簡単空気噴射機関88r駆動や簡単噴射機関88s駆動とし、自動車駆動や船舶駆動や飛行機駆動等各種回転駆動や超高速噴射推進駆動として、飛行機駆動の場合は宇宙到達費用1/50万狙い地球上何処でも日帰り旅行狙いを可能にする、液体酸素製造機88pにする。   The liquid oxygen producing machine 88p in FIG. 4 has an ultra-high speed counter-rotating linear compression with both-side center support bearing load merge 0 approach + inner compression blade 8q outer compression blade 8r inner output blade 8s outer output blade 8t + horizontal shaft bearing load 0 approach. The liquid oxygen production machine 88p, which is a long, high-speed, double-reversible and easy-to-reverse compressed oxygen wing and output wing in accordance with the rotational speed, peripheral speed and rotational radius of the wing and linear expansion output wing, By making the horizontal axis 1h double-reversing, the compression blade and output blade can be easily assembled as a 9M assembly of an annular part, making it easy to manufacture fully automatically, fully automated, easy to assemble, and aim for 1/100 parts. Assuming that the multistage compressor 3i is connected, the horizontal full-blade water gravity turbine 8B has no fuel cost, 0 power generation, extremely low-cost electric drive, etc. In the case of multistage compression, the multistage compressor 3i is connected to the multistage compressor 3i. In the case of the simple compressor 3s Cooling + water injection compressed air multi-stage cooling Heat production heating air 28a of solar heater 21 is compressed heat recovery, high pressure high temperature water heating pipe 5H thermal production + rectification tower exhaust pipe 5h cooling liquid oxygen + liquid nitrogen Etc., production of ultra-high pressure compressed air 28a to the air turbine 3u and reverse rotation drive to generate a large rotation output of the bearing load coalescence 0 approaching ultra-high speed rotation, thereby significantly reducing the motor drive power Is supplied to the rectification column, purified to liquid oxygen + liquid nitrogen, etc., as in the existing technology, and the exhaust gas is supplied to the rectification column exhaust pipe 5h, and the liquid oxygen production machine 88p is continuously driven with a large amount of hot and cold. Produced and supplied to 3D of electricity + liquid air cold heat + hot water to superheated steam heat supply equipment, for example, in the heat supply, the injected methane is recovered into the methane hydrate under the seabed or permafrost land, and the methane cycle under the permafrost land A transparent enclosure is projected to recover from the tip of the top of the specific gravity difference utilization, and the enclosure is an eternal greenhouse pasture grazing, aiming at the prime of various heat sources such as meat production, and liquid oxygen supply reduces the compression work rate Simple gas engine 88q drive, simple air injection engine 88r drive, simple injection engine 88s drive combined with liquid oxygen drive of 21/60000 volumetric compression power of air compression, automobile drive, ship drive, airplane drive, etc. In the case of airplane drive as various types of rotational drive and ultra-high speed jet propulsion drive, the liquid oxygen production machine 88p that makes it possible to aim for a day trip anywhere on the earth with a space arrival cost of 1 / 500,000.

図5の簡単多段圧縮機3iは、両側中心支持軸受荷重合体0接近+内側圧縮翼8q外側圧縮翼8r内側出力翼8s外側出力翼8t+横軸軸受荷重0接近とし、超高速二重反転直線圧縮翼や直線膨張出力翼の回転速度や周速度や回転半径に合せた、回転半径角度や曲線とした圧縮翼や出力翼にする、長大高速二重反転容易とした簡単多段圧縮機3iは、横軸1h二重反転にすることで圧縮翼を簡単環状部品の嵌合組立部9M組立として、全自動大量製造容易や全自動加工容易や組立容易や部品数1/100狙いとし、横型全動翼水重力タービン8B燃料費0発電極端に安価電気駆動等として、複数段圧縮の場合に液体酸素製造機88p等と連結駆動圧縮とし、太陽光加熱器21で加熱の空気28a等空気圧縮熱回収を1〜複数回繰り返して、水加熱等過熱蒸気50温熱製造+圧縮空気28a冷熱製造を1〜複数回繰り返し、超高圧過熱蒸気50温熱+超高圧圧縮空気28a冷熱の大量生産にして、既存の液体酸素製造原価の1/10製造原価狙い等にするため、内側軸装置60A両側中心支持軸受荷重を0接近にし、長大大型超高速二重反転圧縮機やマイクロ超高速二重反転圧縮機を可能にして、あらゆる条件に対応可能な簡単多段圧縮機3iにし、組立時には二重反転機外箱77Cを横軸1h部で2分割組立として、先ず二重反転歯車装置85Yを組立てることで、外側軸装置60B60Bの外側圧縮翼8r出口翼と入口翼+内側軸装置60A60Aの内側圧縮翼8q出口翼と入口翼を組立し、夫々に1〜複数の内側圧縮翼8q中間翼中間翼+外側圧縮翼8r中間翼中間翼を嵌合組立部9M組立して、夫々の内側圧縮翼8q入口翼出口翼+外側圧縮翼8r入口翼出口翼を嵌合組立部9M組立し、圧縮機外箱77b77bを二重反転機外箱77Cに嵌合組立部9M組立して、圧縮機外箱77bを次の二重反転機外箱77Cに嵌合組立部9M組立し、簡単2段圧縮機3tを構成次々に嵌合組立部9M組立連結して、簡単圧縮機3s具備を繰り返す1〜複数段の簡単多段圧縮機3iにし、前記液体酸素製造機88p連結駆動する等、横軸1h二重反転駆動簡単多段圧縮機3iにします。 The simple multistage compressor 3i shown in FIG. 5 has a double-sided center support bearing load combined 0 approach + inner compression blade 8q outer compression blade 8r inner output blade 8s outer output blade 8t + horizontal shaft bearing load 0 approach, A simple multistage compressor 3i that is a long, high-speed, double-reversible and easy-to-reverse compressor blade or output blade with a rotational radius angle or curve that matches the rotational speed, peripheral speed, or rotational radius of the blade or linear expansion output blade. By rotating the shaft 1h in the reverse direction, the compressor blade can be used as a simple annular part fitting assembly part 9M assembling, fully automatic mass production, fully automatic processing, easy assembly, and 1/100 parts count. Water gravity turbine 8B Fuel cost 0 Power generation Extremely inexpensive Electric drive, etc. In the case of multi-stage compression, liquid oxygen production machine 88p etc. are connected to drive compression, and solar heater 21 is used to recover air compressed heat such as heated air 28a Repeat one or more times with water Manufacturing of superheated steam 50 heat + compressed air 28a cold manufacturing one or more times, mass production of super high pressure superheated steam 50 heat + ultrahigh pressure compressed air 28a cold, 1/10 manufacturing of existing liquid oxygen production cost In order to aim for cost etc., the inner side shaft device 60A both side center support bearing load is made close to 0, and a long and large ultra high speed counter rotating compressor and a micro ultra high speed counter rotating compressor are possible, which can respond to all conditions. In the simple multistage compressor 3i, when assembling, the contra-rotating machine outer box 77C is divided into two parts and assembled on the horizontal shaft 1h, and the counter-rotating gear device 85Y is assembled first, so that the outer compression blade 8r outlet blade of the outer shaft device 60B60B And the inlet blade + inner shaft device 60A60A, the inner compressor blade 8q outlet blade and the inlet blade are assembled, and one to a plurality of inner compressor blades 8q intermediate blade intermediate blade + outer compressor blade 8r intermediate blade intermediate blade are fitted together. 9M is assembled, and each inner compression blade 8q inlet blade outlet blade + outer compression blade 8r inlet blade outlet blade is assembled and assembled assembly portion 9M is assembled, and compressor outer box 77b77b is fitted into counter rotating machine outer box 77C. Assemble the assembly part 9M, assemble the compressor outer box 77b into the next counter-rotating machine outer box 77C, assemble the fitting assembly part 9M, and construct the simple two-stage compressor 3t one after another. The simple multi-stage compressor 3i with 1 to multiple stages that repeats the simple compressor 3s, and the liquid oxygen production machine 88p is connected and driven.

図6の簡単ガス機関88qは、両側中心支持軸受荷重合体0接近+内側圧縮翼8q外側圧縮翼8r内側出力翼8s外側出力翼8t+横軸軸受荷重0接近とし、超高速二重反転直線圧縮翼や直線膨張出力翼の回転速度や周速度や回転半径に合せた、回転半径角度や曲線とした圧縮翼や出力翼にする、長大高速二重反転容易とした簡単ガス機関88qは、、横軸1h二重反転にすることで圧縮翼や出力翼を簡単環状部品の嵌合組立部9M組立として、全自動大量製造容易や全自動加工容易や組立容易や部品数1/100狙い、簡単多段圧縮機3i連結狙いとし、横型全動翼水重力タービン8B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、安価電気製造物駆動の理論燃焼室4Q等に液体酸素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+液体燃料+高温水を24〜200MPa等超高圧に圧縮、高圧高温水加熱管5H等で加熱して、複数入口の開閉弁1Qを閉止2種類としたロケット燃焼理論燃焼室4Q内の、酸素噴射ノズル6L+燃料噴射ノズル6Xより最適温度に加熱した酸素+燃料噴射燃焼し、理論燃焼室4Q内壁で燃料+酸素+高温水〜過熱蒸気50を最適温度に加熱理論空燃比燃焼にして、既存ジェット機燃焼の40倍圧力40倍燃焼量狙いにし、既存技術改良理論燃焼室4Qでは既存技術の4倍燃料の理論空燃比燃焼量として、増大熱量で200MPa等の過熱蒸気50を製造過熱蒸気ロケット噴口6Aより噴射して、ロケット噴射により4倍燃焼量の高圧高温燃焼室5M燃焼ガス49を吸引噴射し、既存ガスタービンを大改良した簡単ガス機関88qとして、圧縮仕事率を空気圧縮の21/60000容積圧縮仕事率の、液体酸素駆動理論燃焼室4Q複数の合体とし、液体酸素0でも使用する簡単ガス機関88qとする。 The simple gas engine 88q in FIG. 6 has a double-sided center support bearing load combined 0 approach + inner compression blade 8q outer compression blade 8r inner output blade 8s outer output blade 8t + horizontal bearing load 0 approach, A simple gas engine 88q, which is a long, high-speed, double-reversible and easy-to-reverse compression blade or output blade with a rotational radius angle or curve that matches the rotational speed, peripheral speed, or rotational radius of the linear expansion output blade, 1h Double reversal makes the compression blade and output blade a simple annular part fitting assembly part 9M assembly, fully automated mass production, fully automated processing, easy assembly, aiming at 1/100 parts count, simple multistage compression The aim is to connect machine 3i, horizontal full-blade water gravity turbine 8B fuel cost 0 power generation extremely cheap electricity production, electricity + liquid air cold heat + hot water to superheated steam temperature supply facility 3D, theoretical combustion driven by cheap electricity products Liquid oxygen in chamber 4Q etc. By receiving K + electricity + high temperature water and compressing liquid oxygen 5K, the compression volume work rate becomes 21/60000 volume compression work rate of air compression, and liquid oxygen + liquid fuel + high temperature water exceeds 24 to 200 MPa etc. Compressed to high pressure, heated by high-pressure high-temperature water heating pipe 5H, etc., heated to optimum temperature from oxygen injection nozzle 6L + fuel injection nozzle 6X in rocket combustion theoretical combustion chamber 4Q with two types of on-off valves 1Q closed Oxygen + fuel injection combustion, fuel + oxygen + hot water ~ superheated steam 50 is heated to the optimum temperature on the inner wall of the theoretical combustion chamber 4Q, and the target is 40 times the pressure 40 times the combustion amount of the existing jet combustion, In the existing technology improved theoretical combustion chamber 4Q, as the theoretical air-fuel ratio combustion amount of the quadruple fuel of the existing technology, the superheated steam 50 of 200 MPa or the like with an increased heat quantity is injected from the manufactured superheated steam rocket nozzle 6A. As a simple gas engine 88q, in which a high-pressure high-temperature combustion chamber 5M combustion gas 49 having a fourfold combustion amount is sucked and injected by rocket injection and the existing gas turbine is greatly improved, the compression work rate is 21/60000 volumetric compression work rate of air compression, The liquid oxygen drive theoretical combustion chamber 4Q is composed of a plurality of units, and a simple gas engine 88q that uses even liquid oxygen 0 is used.

液体酸素0既存技術改良理論燃焼室4Qで簡単ガス機関88q駆動の場合を説明すると、既存ジェットエンジンやガスタービンの静翼を略全廃して、二重反転磁気装置85〜二重反転歯車装置85Yにより、両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近の内側軸装置60A+外側軸装置60Bを二重反転駆動し、内側圧縮翼8q+外側圧縮翼8rで入口静翼6Gから吸入した空気28aを直線圧縮して、二重反転直線超高速膨張大出力駆動で圧縮800〜1200℃上昇過程で、直線圧縮簡単多段圧縮機3i連結し、相対速度既存ガスタービン等の2〜5倍狙いとして、2倍圧縮空気圧力以上等を容易超高圧とし、二重反転機外箱77Cの圧縮空気噴射用静翼6Gより理論燃焼室4Qに圧縮空気噴射して、燃料噴射ノズル6Xより燃料噴射燃焼し、高圧高温水加熱管5Hで熱回収200MPa等の過熱蒸気50を製造理論空燃比燃焼にすることで、同一圧縮空気量既存ガスタービン等の4倍燃料燃焼量として、燃焼ガス49の3/4熱量以上や20倍圧力等の過熱蒸気50をロケット噴射し、燃焼ガス49と共同で内側出力翼8s+外側出力翼8tを二重反転駆動して、同一圧縮空気量既存ジェットエンジンやガスタービンの10倍噴射推進出力や10倍回転出力狙いとし、横軸1h叉は内側軸装置60Aを延長して、発電機や自動車類や船舶類や飛行機類を回転駆動し、飛行機類や船舶類は排気で噴射推進追加駆動すると共に、特に発電の場合は簡単ガス機関88q排気全部を熱交換加熱空気28aで熱回収して、内側圧縮翼8q+外側圧縮翼8rで圧縮水噴射熱回収の高温水52bは高圧高温水加熱管5Hに圧入し、空気28aは理論燃焼室4Qで燃料噴射燃焼を繰り返す発電にして、更に図3太陽光加熱器21加熱の高温空気28a合体発電で発電量増大にし、排熱や地熱も同様に空気28aの温度に変換して吸入圧縮水噴射圧縮して、同様に発電量増大の簡単ガス機関88qにする。 In the case of driving the simple gas engine 88q in the liquid oxygen 0 existing technology modified theoretical combustion chamber 4Q, the existing jet engine and the stationary blade of the gas turbine are almost completely abolished, and the counter rotating magnetic device 85 to the counter rotating gear device 85Y. As a result, the inner shaft device 60A + the outer shaft device 60B approaching both sides of the center support bearing load combined 0 approaching + horizontal shaft bearing load approaching the double inversion drive, and the air sucked from the inlet stationary blade 6G by the inner compression blade 8q + outer compression blade 8r In the process of linearly compressing 28a, inverting linear ultra-high speed expansion high power drive and increasing the compression 800-1200 ° C, the linear compression simple multistage compressor 3i is connected, and the target is 2-5 times the relative speed existing gas turbine etc. 2 times the compressed air pressure or more is easily set to an ultra-high pressure, compressed air is injected into the theoretical combustion chamber 4Q from the compressed air injection vane 6G of the contra-rotating machine outer box 77C, and from the fuel injection nozzle 6X. The combustion gas 49 is obtained as a quadruple fuel combustion amount of an existing compressed gas turbine or the like by making the superheated steam 50 such as heat recovery 200 MPa or the like into the production theoretical air-fuel ratio combustion by the high-pressure high-temperature water heating pipe 5H. The superheated steam 50 of 3/4 heat quantity or 20 times pressure or the like is rocket-injected, and the inner output blade 8s + outer output blade 8t is driven in combination with the combustion gas 49 so that the same compressed air amount is applied to the existing jet engine. Aiming at 10-times injection propulsion output and 10-times rotation output of gas turbines, the horizontal shaft 1h or the inner shaft device 60A is extended to rotate and drive generators, automobiles, ships and airplanes. In the case of power generation, in the case of power generation, a simple gas engine 88q exhaust gas is recovered by heat exchange heating air 28a, and compressed water injection heat recovery is performed by inner compression blades 8q + outer compression blades 8r. The high-temperature water 52b is injected into the high-pressure high-temperature water heating pipe 5H, the air 28a is generated by repeating fuel injection combustion in the theoretical combustion chamber 4Q, and further, the amount of power generation is increased by the combined high-temperature air 28a heating of the solar heater 21 in FIG. Similarly, the exhaust heat and geothermal heat are also converted into the temperature of the air 28a and compressed by suction compressed water injection, and similarly, the simple gas engine 88q with an increased power generation amount is obtained.

図7の簡単空気噴射機関88rは、両側中心支持軸受荷重合体0接近+内側圧縮翼8q外側圧縮翼8r内側出力翼8s外側出力翼8t+横軸軸受荷重0接近とし、超高速二重反転直線圧縮翼や直線膨張出力翼の回転速度や周速度や回転半径に合せた、回転半径角度や曲線とした圧縮翼や出力翼にする、長大高速二重反転容易とした簡単空気噴射機関88rは、、横軸1h二重反転にすることで圧縮翼や出力翼を簡単環状部品の嵌合組立部9M組立として、全自動大量製造容易や全自動加工容易や組立容易や部品数1/100狙い、簡単多段圧縮機3i連結狙いとし、横型全動翼水重力タービン8B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、安価電気製造物駆動の理論燃焼室4Q等に液体酸素+電気+高温水を受給して、液体酸素を圧縮することで、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+液体燃料+高温水を24〜200MPa等超高圧に圧縮、高圧高温水加熱管5H等で加熱して、複数入口出口の開閉弁1Qを閉止2種類としたロケット燃焼理論燃焼室4Q内の、酸素噴射ノズル6L+燃料噴射ノズル6Xより最適温度に加熱した酸素+燃料噴射燃焼し、理論燃焼室4Q内壁で燃料+酸素+高温水〜過熱蒸気50を最適温度に加熱理論空燃比燃焼にして、既存ジェット機燃焼の40倍圧力40倍燃焼量狙いにし、理論燃焼室4Q外周空気28a吸引流の過熱蒸気ロケット噴口6A+燃焼ガス噴射ノズル6Yより、200MPaに近付けた過熱蒸気50や高圧高温燃焼室5M燃焼ガス49を噴射して、空気28aを吸引噴射して水を吸引噴射し、既存技術改良理論燃焼室4Qでは既存技術の4倍燃料の理論空燃比燃焼量として、増大熱量で200MPa狙い過熱蒸気50を製造、ロケット外箱77B過熱蒸気ロケット噴口6A噴射し、高圧高温燃焼室5M燃焼ガス49で回転出力発生して、外周空気28a吸引流前方の空気28aを吸引噴射して水52aを吸引噴射し、既存ジェットエンジンを大改良した簡単空気噴射機関88rとして、圧縮仕事率を空気圧縮の21/60000容積圧縮仕事率追加の、液体酸素駆動理論燃焼室4Q複数の合体とし、液体酸素0でも使用する簡単空気噴射機関88rとする。 The simple air injection engine 88r shown in FIG. 7 has a double-sided center support bearing load combined 0 approach + inner compression blade 8q outer compression blade 8r inner output blade 8s outer output blade 8t + horizontal bearing load 0 approach, A simple air injection engine 88r that is easy to make a long, high speed, double reversal, which is a compression blade or output blade with a rotation radius angle or curve that matches the rotation speed, peripheral speed, or rotation radius of the blade or linear expansion output blade, By making the horizontal axis 1h double-reversing, the compression blade and output blade can be easily assembled as a 9M assembly of an annular part, making it easy to manufacture fully automatically, fully automated, easy to assemble, and aim for 1/100 parts. Multi-stage compressor 3i connection aim, horizontal full-blade water gravity turbine 8B fuel cost 0 power generation extremely cheap electricity production from electricity + liquid air cold heat + hot water to superheated steam temperature supply equipment 3D, cheap electric product drive For the theoretical combustion chamber 4Q, etc. By receiving body oxygen + electricity + hot water and compressing liquid oxygen, the compression volume work rate is 21/60000 volume compression work rate of air compression, and liquid oxygen + liquid fuel + hot water is 24 to 200 MPa, etc. Optimum temperature from oxygen injection nozzle 6L + fuel injection nozzle 6X in rocket combustion theoretical combustion chamber 4Q, which is compressed to ultra-high pressure and heated by high-pressure high-temperature water heating pipe 5H etc. The heated oxygen + fuel is injected and burned, the fuel + oxygen + hot water to superheated steam 50 is heated to the optimal temperature on the inner wall of the theoretical combustion chamber 4Q, and the combustion is aimed at the theoretical air-fuel ratio combustion. From the superheated steam rocket nozzle 6A of the theoretical combustion chamber 4Q peripheral air 28a suction flow and the combustion gas injection nozzle 6Y, the superheated steam 50 and the high pressure high temperature combustion chamber 5M 49, the air 28a is sucked and jetted, and water is sucked and jetted. In the existing technology improved theoretical combustion chamber 4Q, the superheated steam 50 aiming at 200 MPa is increased as the theoretical air-fuel ratio combustion amount of four times the fuel of the existing technology. Manufacturing, rocket outer box 77B superheated steam rocket injection hole 6A is injected, high pressure high temperature combustion chamber 5M combustion gas 49 rotation output is generated, outer air 28a suction flow forward air 28a suction injection and water 52a suction injection, As a simple air injection engine 88r that is a greatly improved existing jet engine, the compression work rate is 21/60000 volumetric compression work rate addition, combined with multiple liquid oxygen driven theoretical combustion chambers 4Q, easy to use even with zero liquid oxygen The air injection engine 88r is assumed.

液体酸素0既存技術改良理論燃焼室4Qで簡単空気噴射機関88r駆動の場合を説明すると、既存ジェットエンジンやガスタービンの静翼を略全廃して、二重反転磁気装置85〜二重反転歯車装置85Yにより、両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近の内側軸装置60A+外側軸装置60Bを二重反転駆動し、内側圧縮翼8q+外側圧縮翼8rで入口静翼6Gから吸入した空気28aを直線圧縮して、燃料噴射燃焼する二重反転直線超高速膨張大出力で簡単多段圧縮機3i連結や、相対速度既存ガスタービン等の2〜5倍の2倍圧縮空気圧力以上等を容易超高圧とし、二重反転機外箱77Cの圧縮空気噴射用静翼6Gより、理論燃焼室4Qに圧縮空気28aを噴射して、燃料噴射ノズル6Xより燃料噴射燃焼し、高圧高温水加熱管5Hで熱回収過熱蒸気50を製造理論空燃比燃焼にすることで、同一圧縮空気量既存ガスタービン等の4倍燃料燃焼量や外周をロケット噴射部として、燃焼ガス49の3/4熱量以上や20倍圧力等の過熱蒸気50をロケット外箱77B内に噴射し、燃焼ガス49で内側出力翼8s+外側出力翼8tを二重反転駆動して、同一圧縮空気量既存ジェットエンジンやガスタービンの15倍噴射推進出力+5倍回転出力狙いとし、空気吸引噴射部筒を後方のみ具備等水抵抗増大0で空気吸引噴射量増大にして、水中噴射する船舶類の噴射推進駆動等にする、簡単空気噴射機関88rにする。 The case where the simple air injection engine 88r is driven in the liquid oxygen 0 existing technology improved theoretical combustion chamber 4Q will be described. The existing jet engine and the stationary vanes of the gas turbine are almost completely abolished, and the counter rotating magnetic device 85 to the counter rotating gear device. With 85Y, the inner shaft device 60A + the outer shaft device 60B approaching both sides of the center support bearing load combined 0 approaching + horizontal bearing load 0 approaching is reversed and sucked from the inlet stationary blade 6G by the inner compression blade 8q + the outer compression blade 8r. The air 28a is linearly compressed and the fuel is injected and burned. The output is a double reversal linear ultra-high-speed expansion, high output, simple multi-stage compressor 3i connection, relative speed 2-5 times that of existing gas turbines, etc. High pressure and high temperature water is obtained by injecting compressed air 28a into the theoretical combustion chamber 4Q from the compressed air injection stationary vane 6G of the counter-rotating machine outer box 77C and fuel injection combustion from the fuel injection nozzle 6X. By making the heat recovery superheated steam 50 into the stoichiometric air-fuel ratio combustion with the heat pipe 5H, the same compressed air amount is 4 times the fuel combustion amount of the existing gas turbine or the like, and the outer periphery is the rocket injection part or more than 3/4 heat amount of the combustion gas 49 The superheated steam 50 of 20 times pressure or the like is injected into the rocket outer box 77B, and the combustion gas 49 is used to reversely drive the inner output blade 8s + the outer output blade 8t, so that the same compressed air amount of the existing jet engine or gas turbine Simple air that aims at 15 times injection propulsion output + 5 times rotation output, has an air suction injection part cylinder only at the rear, etc. Increases air suction injection amount with 0 water resistance increase, and makes it an injection propulsion drive etc. for ships that inject underwater The injection engine 88r is used.

図8の簡単噴射機関88sは、両側中心支持軸受荷重合体0接近+内側圧縮翼8q外側圧縮翼8r内側出力翼8s外側出力翼8t+横軸軸受荷重0接近とし、超高速二重反転直線圧縮翼や直線膨張出力翼の回転速度や周速度や回転半径に合せた、回転半径角度や曲線とした圧縮翼や出力翼にする、長大高速二重反転容易とした簡単噴射機関88sは、、横軸1h二重反転にすることで圧縮翼や出力翼を簡単環状部品の嵌合組立部9M組立として、全自動大量製造容易や全自動加工容易や組立容易や部品数1/100狙い、簡単多段圧縮機3i連結狙いとし、横型全動翼水重力タービン8B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、安価電気製造物駆動の理論燃焼室4Q等に液体酸素+電気+高温水を受給して、液体酸素を圧縮することで、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+液体燃料+高温水を24〜200MPa等超高圧に圧縮加熱して、複数入口出口の開閉弁1Qを閉止2種類としたロケット燃焼理論燃焼室4Q内の、酸素噴射ノズル6L+燃料噴射ノズル6Xより最適温度に加熱した酸素+燃料噴射燃焼し、理論燃焼室4Q内壁で燃料+酸素+高温水〜過熱蒸気50を最適温度に加熱理論空燃比燃焼にして、既存ジェット機燃焼の40倍圧力40倍燃焼量狙いにし、ロケット外箱77B内過熱蒸気ロケット噴口6A+燃焼ガス噴射ノズル6Yより、200MPaに近付けた過熱蒸気50や高圧高温燃焼室5M燃焼ガス49を噴射して、開閉弁1Q閉では大出力ロケット燃焼宇宙利用全盛等とし、開閉弁1Q開では前方の空気28aを吸引噴射して、理論燃焼室4Q複数を液体酸素駆動のロケット燃焼室兼ジェット燃焼室とし、既存技術改良ジェット燃焼理論燃焼室4Qでは既存技術の4倍燃料の理論空燃比燃焼量として、増大熱量で200MPa狙い過熱蒸気50を製造、ロケット外箱77B過熱蒸気ロケット噴口6Aより噴射し、高圧高温燃焼室5M燃焼ガス49で回転出力発生して、前方の空気28aを吸引噴射し、既存ジェットエンジンを大改良した簡単噴射機関88sとして、液体酸素駆動理論燃焼室4Q複数の合体とし、液体酸素0でも使用する簡単噴射機関88sとする。 The simple injection engine 88s shown in FIG. 8 has a double-sided center support bearing load combined 0 approach + inner compression blade 8q outer compression blade 8r inner output blade 8s outer output blade 8t + horizontal bearing load 0 approach, The simple injection engine 88s, which is a long, high speed, double reversible, easy-to-return compression blade or output blade with a rotation radius angle or curve that matches the rotation speed, circumferential speed, and rotation radius of the linear expansion output blade, 1h Double reversal makes the compression blade and output blade a simple annular part fitting assembly part 9M assembly, fully automated mass production, fully automated processing, easy assembly, aiming at 1/100 parts count, simple multistage compression The aim is to connect machine 3i, horizontal full-blade water gravity turbine 8B fuel cost 0 power generation extremely cheap electricity production, electricity + liquid air cold heat + hot water to superheated steam temperature supply facility 3D, theoretical combustion driven by cheap electricity products Liquid oxygen in chamber 4Q etc. By receiving electricity + high temperature water and compressing liquid oxygen, the compression volume work rate is 21/60000 volume compression work rate of air compression, and liquid oxygen + liquid fuel + high temperature water is set to ultra high pressure such as 24-200 MPa. Oxygen + fuel injection combustion heated to the optimum temperature from the oxygen injection nozzle 6L + fuel injection nozzle 6X in the rocket combustion theoretical combustion chamber 4Q with two types of shut-off valves 1Q closed at multiple inlets and outlets by compression heating, theoretical combustion Fuel + oxygen + hot water to superheated steam 50 is heated to the optimum temperature on the inner wall of the chamber 4Q, and the target air / fuel ratio combustion is set to 40 times the pressure 40 times that of the existing jet combustion. The superheated steam 50 and the high pressure / high temperature combustion chamber 5M combustion gas 49 approaching 200 MPa are injected from the combustion gas injection nozzle 6Y. When the on-off valve 1Q is opened, the front air 28a is sucked and injected, and a plurality of theoretical combustion chambers 4Q are used as rocket combustion chambers and jet combustion chambers driven by liquid oxygen. As the theoretical air-fuel ratio combustion amount of the quadruple fuel of the existing technology, the superheated steam 50 is manufactured aiming at 200 MPa with an increased heat quantity, injected from the rocket outer box 77B superheated steam rocket nozzle 6A, and rotational output is generated in the high-pressure high-temperature combustion chamber 5M combustion gas 49 As a simple injection engine 88s that sucks and injects the air 28a ahead and greatly improves the existing jet engine, a combination of a plurality of liquid oxygen drive theoretical combustion chambers 4Q is used, and a simple injection engine 88s that uses even liquid oxygen 0 is used.

液体酸素0既存技術改良理論燃焼室4Qで簡単噴射機関88s駆動の場合を説明すると、既存ジェットエンジンやガスタービンの静翼を略全廃して、二重反転磁気装置85〜二重反転歯車装置85Yにより、両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近の内側軸装置60A+外側軸装置60Bを二重反転駆動し、内側圧縮翼8q+外側圧縮翼8rで入口静翼6Gから吸入した空気28aを直線圧縮して、燃料噴射燃焼二重反転直線超高速膨張大出力で簡単多段圧縮機3i連結や、相対速度既存ガスタービン等の2〜5倍の2倍圧縮空気圧力以上等を容易超高圧とし、二重反転機外箱77Cの圧縮空気噴射用静翼6Gより、ジェット燃焼理論燃焼室4Qに圧縮空気28aを噴射して、燃料噴射ノズル6Xより燃料噴射燃焼し、高圧高温水加熱管5Hで熱回収過熱蒸気50を製造理論空燃比燃焼にすることで、同一圧縮空気量既存ガスタービン等の4倍燃料燃焼量や外周をロケット噴射部として、燃焼ガス49の3/4熱量以上や20倍圧力等の過熱蒸気50をロケット外箱77B内に噴射し、燃焼ガス49で内側出力翼8s+外側出力翼8tを二重反転駆動して、同一圧縮空気量既存ジェットエンジンやガスタービンの15倍噴射推進出力+5倍回転出力狙いとし、水中噴射する船舶類や飛行機類を噴射推進駆動等にする、簡単噴射機関88sにする。 The case of driving the simple injection engine 88s in the liquid oxygen 0 existing technology improved theoretical combustion chamber 4Q will be described. The existing jet engine and the stationary vanes of the gas turbine are almost completely abolished, and the counter rotating magnetic device 85 to the counter rotating gear device 85Y. As a result, the inner shaft device 60A + the outer shaft device 60B approaching both sides of the center support bearing load combined 0 approaching + horizontal shaft bearing load approaching the double inversion drive, and the air sucked from the inlet stationary blade 6G by the inner compression blade 8q + outer compression blade 8r 28a is linearly compressed, fuel injection combustion counter-rotating linear ultra-high-speed expansion, high output, easy multistage compressor 3i connection, relative speed 2-5 times that of existing gas turbine etc. The compressed air 28a is injected into the jet combustion theoretical combustion chamber 4Q from the compressed air injection stationary blade 6G of the contra-rotating outer casing 77C, and the fuel is injected and burned from the fuel injection nozzle 6X. By making the heat recovery superheated steam 50 into the production theoretical air-fuel ratio combustion with the water heating pipe 5H, the same compressed air amount is 4 times the fuel combustion amount of the existing gas turbine or the like, and the outer periphery is 3/4 of the combustion gas 49. Overheated steam 50 having a heat amount or 20 times pressure or the like is injected into the rocket outer box 77B, and the inner output blade 8s + outer output blade 8t is double-reversed and driven by the combustion gas 49, so that an existing jet engine or gas with the same compressed air amount is used. A simple injection engine 88s is used which aims at 15 times injection propulsion output +5 times rotation output of the turbine, and makes the water-injected vessels and airplanes use injection propulsion drive.

図9の簡単ガス機関自動車7Iは、既存マイクロガスタービン自動車の改良発明簡単ガス機関88qを、圧縮空気駆動+燃料費0発電電気製造物選択駆動を選択可能としたもので、横型全動翼水重力タービン8B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、安価電気製造物駆動の理論燃焼室4Q等に液体酸素+電気+高温水を受給して、液体酸素を圧縮することで、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+液体燃料+高温水を24〜200MPa等超高圧に圧縮加熱して、複数入口の開閉弁1Qを閉止したロケット燃焼理論燃焼室4Q内の、酸素噴射ノズル6L+燃料噴射ノズル6Xより最適温度に加熱した酸素+燃料噴射燃焼し、理論燃焼室4Q内壁で燃料+酸素+高温水〜過熱蒸気50を最適温度に加熱理論空燃比燃焼にして、既存ジェット機燃焼の40倍圧力40倍燃焼量狙いにし、既存技術改良ジェット燃焼理論燃焼室4Qでは既存技術の4倍燃料4倍燃焼量の理論空燃比燃焼量として、増大熱量で200MPa等の過熱蒸気50を製造過熱蒸気ロケット噴口6Aより噴射して、ロケット噴射により4倍燃焼や40倍燃焼狙い高圧高温燃焼室5M燃焼ガス49を吸引噴射し、既存マイクロガスタービンを大改良した簡単ガス機関88qとして、発電機1を駆動して蓄電池1Aに蓄電蓄電池駆動車輪4J駆動し、圧縮空気駆動の発電所や蓄電所としても使用する、液体酸素駆動理論燃焼室4Q複数の合体として、液体酸素0でも使用する、超高速回転出力+超高圧噴射推進出力重量増大に対応する、簡単ガス機関自動車7Iとする。 A simple gas engine vehicle 7I in FIG. 9 is an improved invention of an existing micro gas turbine vehicle. The simple gas engine 88q can select a compressed air drive + a fuel cost zero power generation electric product selection drive. Gravity turbine 8B Fuel cost 0 Power generation Extremely cheap electricity production from electricity + liquid air cold heat + hot water to superheated steam temperature heat supply equipment 3D, to the theoretical combustion chamber 4Q driven by cheap electricity products etc. Liquid oxygen + electricity + hot water And compressing liquid oxygen, the compression volume work rate is 21/60000 volume compression work rate of air compression, and liquid oxygen + liquid fuel + high-temperature water is compressed and heated to an ultrahigh pressure such as 24-200 MPa. In the rocket combustion theoretical combustion chamber 4Q with the multiple inlet on-off valves 1Q closed, oxygen + fuel injection heated to an optimum temperature from the oxygen injection nozzle 6L + fuel injection nozzle 6X, the theoretical combustion chamber Fuel + oxygen + hot water to superheated steam 50 is heated to the optimum temperature on the Q inner wall, and the target air-fuel ratio combustion is aimed at 40 times pressure 40 times the combustion amount of existing jet combustion, and existing technology improved jet combustion theoretical combustion chamber 4Q As the theoretical air-fuel ratio combustion amount of 4 times fuel and 4 times combustion amount of technology, superheated steam 50 such as 200 MPa with increased heat quantity is injected from the production superheated steam rocket nozzle 6A, and high pressure aiming at 4 times combustion or 40 times combustion by rocket injection As a simple gas engine 88q that sucks and injects the high-temperature combustion chamber 5M combustion gas 49 and greatly improves the existing micro gas turbine, the generator 1 is driven to drive the storage battery drive wheels 4J to the storage battery 1A, and the compressed air drive power plant Liquid oxygen drive theoretical combustion chamber 4Q also used as a power storage station, combined with multiple Q4, even with liquid oxygen 0, ultra high speed rotation output + ultra high pressure injection propulsion output It corresponds to the amount increases, and simple gas engine automobile 7I.

図10の簡単ガス機関船舶7Jは、既存ガスタービン船舶の改良発明簡単ガス機関88qを、圧縮空気駆動+燃料費0発電電気製造物選択駆動を選択可能としたもので、横型全動翼水重力タービン8B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、安価電気製造物駆動の理論燃焼室4Q等に液体酸素+電気+高温水を受給して、液体酸素を圧縮することで、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+液体燃料+高温水を24〜200MPa等超高圧に圧縮加熱して、複数入口の開閉弁1Qを閉止したロケット燃焼理論燃焼室4Q内の、酸素噴射ノズル6L+燃料噴射ノズル6Xより最適温度に加熱した酸素+燃料噴射燃焼し、理論燃焼室4Q内壁で燃料+酸素+高温水〜過熱蒸気50を最適温度に加熱理論空燃比燃焼にして、既存ジェット機燃焼の40倍圧力40倍燃焼量狙いにし、既存技術改良理論燃焼室4Qでは既存技術の4倍燃料4倍燃焼量の理論空燃比燃焼量として、増大熱量で200MPa等の過熱蒸気50を製造過熱蒸気ロケット噴口6Aより噴射して、ロケット噴射により4倍燃焼量や40倍燃焼狙い高圧高温燃焼室5M燃焼ガス49を吸引噴射し、既存ガスタービン船舶を大改良した簡単ガス機関船舶7Jとして、簡単ガス機関88qの回転出力でスクリュウ7C駆動排気を先頭部船底に噴射することで、摩擦損失最低として10倍出力等が可能なロケット燃焼で急速浮上滑空接近にし、摩擦損失を極端に低減して燃料酸素を節約する、液体酸素節約駆動理論燃焼室4Q複数の合体として、液体酸素0でも使用する、超高速回転出力+超高圧噴射推進出力重量増大に対応する、簡単ガス機関船舶7Jとする。 The simple gas engine ship 7J in FIG. 10 is an improved invention of the existing gas turbine ship. The simple gas engine 88q can be selected from compressed air drive + fuel cost 0 power generation electrical product selection drive. Turbine 8B Fuel cost 0 Power generation Extremely inexpensive electricity production Electricity + liquid air cold heat + high temperature water-superheated steam temperature heat supply equipment 3D from liquid oxygen + electricity + high temperature water to the theoretical combustion chamber 4Q, etc. driven by cheap electric products By receiving and compressing liquid oxygen, the compression volume work rate is set to 21/60000 volume compression work rate of air compression, and liquid oxygen + liquid fuel + high temperature water is compressed and heated to an ultrahigh pressure such as 24-200 MPa, In the rocket combustion theoretical combustion chamber 4Q with the multiple inlet on-off valve 1Q closed, the oxygen + fuel injection heated to the optimum temperature from the oxygen injection nozzle 6L + fuel injection nozzle 6X is combusted, and the theoretical combustion chamber 4Q inner wall Gas + oxygen + hot water to superheated steam 50 is heated to the optimum temperature and the theoretical air-fuel ratio combustion is performed, aiming for 40 times the pressure 40 times the combustion amount of the existing jet combustion, and the existing technology improved theoretical combustion chamber 4Q is 4 times the fuel of the existing technology As the stoichiometric air-fuel ratio combustion amount with a quadruple combustion amount, superheated steam 50 of 200 MPa or the like with an increased heat amount is injected from the production superheated steam rocket nozzle 6A, and the high pressure and high temperature combustion chamber 5M aiming at the quadruple combustion amount or 40 times combustion by rocket injection As a simple gas engine ship 7J in which the combustion gas 49 is sucked and injected, and the existing gas turbine ship is greatly improved, the screw 7C drive exhaust is injected to the bottom of the ship at the rotational output of the simple gas engine 88q, so that the minimum friction loss is 10 Liquid oxygen conserving drive theoretical combustion chamber 4Q that saves fuel oxygen by drastically reducing glide loss with rocket combustion capable of double output, etc. As the number of combined use any liquid oxygen 0, it corresponds to ultra high speed output + ultra high-pressure jet propulsion output increase in weight, and simple gas engine vessels 7J.

図11の簡単ガス機関飛行機7Kは、既存ジェット機の改良発明簡単ガス機関88qを圧縮空気駆動+燃料費0発電電気製造物選択駆動を選択可能としたもので、横型全動翼水重力タービン8B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、安価電気製造物駆動の理論燃焼室4Q等に液体酸素+電気+高温水を受給して、液体酸素を圧縮することで、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+液体燃料+高温水を24〜200MPa等超高圧に圧縮加熱して、複数入口の開閉弁1Qを閉止したロケット燃焼理論燃焼室4Q内の、酸素噴射ノズル6L+燃料噴射ノズル6Xより最適温度に加熱した酸素+燃料噴射燃焼し、理論燃焼室4Q内壁で燃料+酸素+高温水〜過熱蒸気50を最適温度に加熱理論空燃比燃焼にして、既存ジェット機燃焼の40倍圧力40倍燃焼量狙いにし、既存技術改良理論燃焼室4Qでは既存技術の4倍燃料4倍燃焼量の理論空燃比燃焼量として、増大熱量で200MPa等の過熱蒸気50を製造過熱蒸気ロケット噴口6Aより噴射して、排気噴射やロケット噴射により、4倍燃焼量や40倍燃焼狙い高圧高温燃焼室5M燃焼ガス49を吸引噴射し、既存ジェット機を大改良した簡単ガス機関飛行機7Kとして、簡単ガス機関88qの回転出力でプロペラ7A駆動排気を後方に噴射し、、短時間40倍出力狙いロケット燃焼+4倍出力狙いジェット燃焼等にする、液体酸素駆動理論燃焼室4Q複数の合体として、宇宙到達費用1/50万狙いや大気圏帰還速度マッハ3以下や、大気中は液体酸素0でも飛行する、超高速回転出力+超高圧噴射推進出力重量増大に対応する、大型簡単ガス機関飛行機7Kとする。 The simple gas engine airplane 7K of FIG. 11 is an improved invention of an existing jet aircraft. The simple gas engine 88q can select a compressed air drive + a fuel cost zero power generation electric product selection drive. Cost 0 Power generation Extremely cheap electricity production, electricity + liquid air cold heat + high temperature water to superheated steam temperature heat supply equipment 3D receives liquid oxygen + electricity + high temperature water to the theoretical combustion chamber 4Q etc. driven by cheap electricity products By compressing liquid oxygen, the compression volume work rate is set to 21/60000 volume compression work rate of air compression, and liquid oxygen + liquid fuel + high temperature water is compressed and heated to an ultra-high pressure such as 24-200 MPa. In the rocket combustion theoretical combustion chamber 4Q in which the on-off valve 1Q is closed, oxygen + fuel injection heated to an optimum temperature from the oxygen injection nozzle 6L + fuel injection nozzle 6X is combusted, and the fuel + on the inner wall of the theoretical combustion chamber 4Q + Elementary high-temperature water to superheated steam 50 are heated to the optimal temperature, and the theoretical air-fuel ratio combustion is performed, aiming at 40 times the pressure 40 times the combustion amount of the existing jet combustion, and the existing technology improved theoretical combustion chamber 4Q is 4 times the fuel 4 times the existing technology As the theoretical air-fuel ratio combustion amount of combustion amount, superheated steam 50 with an increased heat amount of 200 MPa or the like is injected from the production superheated steam rocket nozzle 6A, and high-pressure high-temperature combustion aiming at 4 times combustion amount or 40 times combustion by exhaust injection or rocket injection 5M combustion gas 49 is sucked and injected, and as a simple gas engine airplane 7K, which is a greatly improved existing jet aircraft, propeller 7A driving exhaust is injected backward with the rotation output of the simple gas engine 88q, aiming for 40 times output rocket combustion for a short time As a combination of multiple liquid oxygen drive theoretical combustion chambers 4Q, aiming at +4 times target jet combustion, etc., space arrival cost 1 / 500,000 target and atmospheric return speed Mach Hereinafter and in the air it flies even LOX 0 corresponds to ultra high speed output + ultra high-pressure jet propulsion output increase in weight, and large simple gas engine airplane 7K.

図12の簡単空気噴射機関船舶7Lは、既存ガスタービン船舶の改良発明簡単噴射機関88eを圧縮空気駆動+燃料費0発電電気製造物選択駆動を選択可能としたもので、横型全動翼水重力タービン8B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、安価電気製造物駆動の理論燃焼室4Q等に液体酸素+電気+高温水を受給して、液体酸素を圧縮することで、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+液体燃料+高温水を24〜200MPa等超高圧に圧縮加熱して、複数入口出口の開閉弁1Qを閉止したロケット燃焼理論燃焼室4Q内の、酸素噴射ノズル6L+燃料噴射ノズル6Xより最適温度に加熱した酸素+燃料噴射燃焼し、理論燃焼室4Q内壁で燃料+酸素+高温水〜過熱蒸気50を最適温度に加熱理論空燃比燃焼にして、既存ジェット機燃焼の40倍圧力40倍燃焼量狙いにし、理論燃焼室4Q外周の過熱蒸気ロケット噴口6A+燃焼ガス噴射ノズル6Yより、200MPaに近付けた過熱蒸気50や高圧高温燃焼室5M燃焼ガス49を噴射して、開閉弁1Q閉では大出力ロケット燃焼とし、開閉弁1Q開では前方の空気28aを吸引噴射ジェット燃焼として、理論燃焼室4Q複数を液体酸素駆動のロケット燃焼室兼ジェット燃焼室とし、既存技術改良ジェット燃焼理論燃焼室4Qでは既存技術の4倍燃料の理論空燃比燃焼として、増大熱量で200MPa狙い過熱蒸気50を製造、ロケット外箱77B過熱蒸気ロケット噴口6Aより噴射し、高圧高温燃焼室5M燃焼ガス49で回転出力発生して、前方の空気28aを吸引噴射して水を吸引噴射し、既存ジェットエンジンを大改良した簡単空気噴射機関88r駆動として、液体酸素駆動理論燃焼室4Q複数の合体で急浮上飛行速度とし、液体酸素0近傍でも飛行速度維持狙う、超高速回転出力+超高圧噴射推進出力重量増大に対応する、簡単空気噴射機関船舶7Lとする。 A simple air injection engine ship 7L in FIG. 12 is an improved invention of an existing gas turbine ship. The simple injection engine 88e can select a compressed air drive + a fuel cost 0 generation electric product selection drive. Turbine 8B Fuel cost 0 Power generation Extremely inexpensive electricity production Electricity + liquid air cold heat + high temperature water-superheated steam temperature heat supply equipment 3D from liquid oxygen + electricity + high temperature water to the theoretical combustion chamber 4Q, etc. driven by cheap electric products By receiving and compressing liquid oxygen, the compression volume work rate is set to 21/60000 volume compression work rate of air compression, and liquid oxygen + liquid fuel + high temperature water is compressed and heated to an ultrahigh pressure such as 24-200 MPa, In the rocket combustion theoretical combustion chamber 4Q with the multiple inlet / outlet opening / closing valve 1Q closed, the oxygen + fuel injection combustion heated to the optimum temperature from the oxygen injection nozzle 6L + fuel injection nozzle 6X, the theoretical combustion chamber 4Q Fuel + oxygen + high-temperature water to superheated steam 50 heated to the optimum temperature on the wall, aiming at the theoretical air-fuel ratio combustion, aiming for 40 times the pressure and 40 times the combustion amount of existing jet combustion, superheated steam rocket nozzle 6A + combustion around the theoretical combustion chamber 4Q From the gas injection nozzle 6Y, the superheated steam 50 and the high-pressure high-temperature combustion chamber 5M combustion gas 49 approaching 200 MPa are injected, and when the on-off valve 1Q is closed, high-power rocket combustion is performed, and when the on-off valve 1Q is open, the front air 28a is sucked and injected. As jet combustion, a plurality of theoretical combustion chambers 4Q are used as rocket combustion chambers and jet combustion chambers driven by liquid oxygen, and in the existing technology improved jet combustion theoretical combustion chamber 4Q, the theoretical air-fuel ratio combustion of four times the fuel of the existing technology is increased by 200 MPa with an increased amount of heat. The target superheated steam 50 is manufactured, injected from the rocket outer box 77B superheated steam rocket nozzle 6A, and the high pressure high temperature combustion chamber 5M combustion gas 49 Rotation output is generated, the air 28a in front is sucked and jetted, and water is sucked and jetted. As a simple air jet engine 88r driven by a greatly improved existing jet engine, the liquid oxygen drive theoretical combustion chamber 4Q is united with a plurality of coalesced flight. It is a simple air injection engine ship 7L corresponding to an increase in the super high speed rotation output + ultra high pressure injection propulsion output weight, aiming at maintaining the flight speed even in the vicinity of zero liquid oxygen.

図13の簡単噴射機関飛行機7Mは、既存ジェット機の改良発明簡単噴射機関88eを圧縮空気駆動+燃料費0発電電気製造物選択駆動を選択可能としたもので、横型全動翼水重力タービン8B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、安価電気製造物駆動の理論燃焼室4Q等に液体酸素+電気+高温水を受給して、液体酸素を圧縮することで、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+液体燃料+高温水を24〜200MPa等超高圧に圧縮加熱して、複数入口出口の開閉弁1Qを閉止したロケット燃焼理論燃焼室4Q内の、酸素噴射ノズル6L+燃料噴射ノズル6Xより最適温度に加熱した酸素+燃料噴射燃焼し、理論燃焼室4Q内壁で燃料+酸素+高温水〜過熱蒸気50を最適温度に加熱理論空燃比燃焼にして、既存ジェット機燃焼の40倍圧力40倍燃焼量狙いにし、理論燃焼室4Q外周の過熱蒸気ロケット噴口6A+燃焼ガス噴射ノズル6Yより、200MPaに近付けた過熱蒸気50や高圧高温燃焼室5M燃焼ガス49を噴射して、開閉弁1Q閉では大出力ロケット燃焼宇宙利用全盛等とし、開閉弁1Q開では前方の空気28aを吸引噴射して、理論燃焼室4Q複数を液体酸素駆動のロケット燃焼室兼ジェット燃焼室とし、既存技術改良理論燃焼室4Qでは既存技術の4倍燃料の理論空燃比燃焼として、増大熱量で200MPa狙い過熱蒸気50を製造、ロケット外箱77B過熱蒸気ロケット噴口6Aより噴射し、高圧高温燃焼室5M燃焼ガス49で回転出力発生して、前方の空気28aを吸引噴射し、既存ジェットエンジンを大改良した簡単噴射機関88s駆動として、液体酸素駆動理論燃焼室4Q複数の合体で宇宙到達費用既存技術の1/50万狙いとし、大気圏帰還速度マッハ3以下や大気中は液体酸素0で高速飛行や、用途により内側軸装置60A延長してプロペラ7A駆動する、超高速回転出力+超高圧噴射推進出力重量増大に対応する、大型簡単噴射機関飛行機7Mとする。 The simple injection engine airplane 7M in FIG. 13 is an improved invention of the existing jet aircraft. The simple injection engine 88e can select the compressed air drive + the fuel cost 0 generation electric product selection drive. Cost 0 Power generation Extremely cheap electricity production, electricity + liquid air cold heat + high temperature water to superheated steam temperature heat supply equipment 3D receives liquid oxygen + electricity + high temperature water to the theoretical combustion chamber 4Q etc. driven by cheap electricity products By compressing liquid oxygen, the compression volume work rate is made to be 21/60000 volume compression work rate of air compression, and liquid oxygen + liquid fuel + high temperature water is compressed and heated to ultrahigh pressure such as 24 to 200 MPa, multiple inlets and outlets In the rocket combustion theoretical combustion chamber 4Q with the open / close valve 1Q closed, oxygen + fuel injection heated to an optimum temperature from the oxygen injection nozzle 6L + fuel injection nozzle 6X is combusted and burned on the inner wall of the theoretical combustion chamber 4Q + Oxygen + Hot water to superheated steam 50 heated to the optimum temperature Theoretical air-fuel ratio combustion, 40 times the pressure of existing jet combustion, 40 times the combustion amount, superheated steam rocket nozzle 6A around the combustion chamber 4Q + combustion gas injection nozzle From 6Y, superheated steam 50 and high-pressure high-temperature combustion chamber 5M combustion gas 49 approaching 200 MPa are injected, and when the on-off valve 1Q is closed, the high-power rocket combustion space utilization is primed. The theoretical combustion chamber 4Q is made into a liquid oxygen-driven rocket combustion chamber and jet combustion chamber, and the existing technology improved theoretical combustion chamber 4Q is a theoretical air-fuel ratio combustion of four times the fuel of the existing technology. Steam 50 is manufactured, injected from the rocket outer box 77B superheated steam rocket nozzle 6A, and rotational output is generated in the high-pressure high-temperature combustion chamber 5M combustion gas 49, As a simple injection engine 88s drive that sucks and injects the air 28a, and the existing jet engine is greatly improved, the combined space of the liquid oxygen drive theoretical combustion chamber 4Q is 15,000,000 to reach the space cost of the existing technology. Large, simple injection engine airplane with Mach 3 or lower and high-speed flight with zero liquid oxygen in the atmosphere, and extended propeller 7A by extending the inner shaft device 60A depending on the application. 7M.

図14の回転翼飛行機7Nは、既存回転翼機の改良発明簡単ガス機関88qを圧縮空気駆動+燃料費0発電電気製造物選択駆動を選択可能としたもので、横型全動翼水重力タービン8B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、安価電気製造物駆動の理論燃焼室4Q等に液体酸素+電気+高温水を受給して、液体酸素を圧縮することで、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+液体燃料+高温水を24〜200MPa等超高圧に圧縮加熱して、複数入口の開閉弁1Qを閉止したロケット燃焼理論燃焼室4Q内の、酸素噴射ノズル6L+燃料噴射ノズル6Xより最適温度に加熱した酸素+燃料噴射燃焼し、理論燃焼室4Q内壁で燃料+酸素+高温水〜過熱蒸気50を最適温度に加熱理論空燃比燃焼にして、既存ジェット機燃焼の40倍圧力40倍燃焼量狙いにし、ジェット燃焼理論燃焼室4Qでは既存技術の4倍燃料燃焼の理論空燃比燃焼として、増大3倍熱量で200MPa等の過熱蒸気50を製造し、過熱蒸気ロケット噴口6Aより噴射して、排気噴射やロケット噴射により4倍燃焼量や40倍燃焼狙い高圧高温燃焼室5M噴射し、既存回転翼機を大改良した回転翼飛行機7Nとして、簡単ガス機関88qの回転出力で回転翼7B駆動排気噴射で回転力+噴射推進にし、内側軸装置60A延長回転翼7B駆動して、10倍出力等が可能なロケット燃焼+ジェット燃焼+回転出力+噴射推進出力にする、圧縮空気+液体酸素駆動理論燃焼室4Q複数の合体として、宇宙到達費用既存技術の1/50万狙いや、大気圏帰還速度マッハ3以下や液体酸素0でも飛行する、超高速回転出力+超高圧噴射推進出力重量増大に対応する、大型回転翼飛行機7Nとする。 The rotary wing airplane 7N of FIG. 14 is an improved invention of an existing rotary wing aircraft. The simple gas engine 88q can select a compressed air drive + a fuel cost 0 power generation electric product selection drive. Fuel cost 0 power generation Electricity + liquid air cold heat + high temperature water to superheated steam temperature heat supply equipment 3D, which is extremely inexpensive electricity production, receives liquid oxygen + electricity + high temperature water to the theoretical combustion chamber 4Q, etc. driven by low cost electric products By compressing liquid oxygen, the compression volume work rate is made to be 21/60000 volume compression work rate of air compression, and liquid oxygen + liquid fuel + high temperature water is compressed and heated to an ultrahigh pressure such as 24-200 MPa, and a plurality of inlets In the rocket combustion theoretical combustion chamber 4Q with the open / close valve 1Q closed, oxygen + fuel injection combustion heated to an optimum temperature from the oxygen injection nozzle 6L + fuel injection nozzle 6X, fuel + oxygen + high on the inner wall of the theoretical combustion chamber 4Q Water to superheated steam 50 is heated to the optimum temperature and the theoretical air-fuel ratio combustion is performed, aiming at 40 times the pressure and 40 times the combustion amount of the existing jet combustion, and in the jet combustion theoretical combustion chamber 4Q, the theoretical air-fuel ratio combustion of the existing technology 4 times fuel combustion As an example, the superheated steam 50 of 200 MPa or the like is manufactured with a triple heat quantity, injected from the superheated steam rocket nozzle 6A, and injected into the high-pressure and high-temperature combustion chamber 5M aiming at a 4-fold combustion amount or 40-fold combustion by exhaust injection or rocket injection, As a rotary wing airplane 7N, which is a greatly improved existing rotary wing aircraft, the rotary output of the simple gas engine 88q is used to drive the rotary blade 7B, and the rotational force is added to the propulsion, and the inner shaft device 60A is driven by the extended rotary blade 7B. Rocket combustion + jet combustion + rotation output + injection propulsion output capable of output etc. Compressed air + liquid oxygen driven theoretical combustion chamber 4Q Combined with multiple combustion chambers 4Q 1/50 ten thousand aim and the operator, to fly even atmospheric feedback speed Mach 3 or less and liquid oxygen 0, corresponds to ultra high speed output + ultra high-pressure jet propulsion output weight increase, the large rotating blades airplane 7N.

図15の回転翼噴射飛行機7Oは、既存回転翼機の改良発明簡単噴射機関88eを圧縮空気駆動+燃料費0発電電気製造物選択駆動を選択可能としたもので、横型全動翼水重力タービン8B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、安価電気製造物駆動の理論燃焼室4Q等に液体酸素+電気+高温水を受給して、液体酸素を圧縮することで、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+液体燃料+高温水を24〜200MPa等超高圧に圧縮加熱して、複数入口出口の開閉弁1Qを閉止したロケット燃焼理論燃焼室4Q内の、酸素噴射ノズル6L+燃料噴射ノズル6Xより最適温度に加熱した酸素+燃料噴射燃焼し、理論燃焼室4Q内壁で燃料+酸素+高温水〜過熱蒸気50を最適温度に加熱理論空燃比燃焼にして、既存ジェット機燃焼の40倍圧力40倍燃焼量狙いにし、理論燃焼室4Q外周の過熱蒸気ロケット噴口6A+燃焼ガス噴射ノズル6Yより、200MPaに近付けた過熱蒸気50や高圧高温燃焼室5M燃焼ガス49を噴射にして、開閉弁1Q閉では大出力ロケット燃焼宇宙利用全盛等とし、開閉弁1Q開では圧縮空気28a燃焼を理論空燃比燃焼等で噴射して、理論燃焼室4Q複数を液体酸素駆動のロケット燃焼室兼ジェット燃焼室とし、圧縮空気燃焼ジェット燃焼理論燃焼室4Qでは既存技術の4倍燃料の理論空燃比燃焼として、増大3倍熱量で200MPa狙い過熱蒸気50を製造、高圧高温燃焼室5M燃焼ガス49噴射で回転出力発生し、外周空気28a吸引流の過熱蒸気ロケット噴口6Aより過熱蒸気50を噴射して、前方の空気28aを吸引噴射し、既存ジェットエンジンに近付けた簡単噴射機関88s駆動として、液体酸素駆動理論燃焼室4Q複数の合体で宇宙到達費用既存技術の1/50万狙いとし、大気圏帰還速度マッハ3以下や大気中は液体酸素0で飛行や、内側軸装置60A延長回転翼7B駆動して、超高速回転出力+超高圧噴射推進出力重量増大に対応する、大型回転翼噴射飛行機7Oとする。 A rotary wing jet airplane 70 in FIG. 15 is an improved invention of an existing rotary wing aircraft. The simple injection engine 88e can select a compressed air drive + a fuel cost zero power generation electric product selection drive. 8B Fuel cost 0 Power generation Extremely inexpensive electricity production Electricity + Liquid air cold heat + High temperature water-Superheated steam temperature supply facility 3D Receives liquid oxygen + electricity + high temperature water to the theoretical combustion chamber 4Q, etc. driven by cheap electricity products Then, by compressing liquid oxygen, the compression volume work rate is set to 21/60000 volume compression work rate of air compression, and liquid oxygen + liquid fuel + high temperature water is compressed and heated to an ultrahigh pressure such as 24-200 MPa. In the rocket combustion theoretical combustion chamber 4Q with the opening / closing valve 1Q at the inlet / outlet closed, oxygen + fuel injection heated to an optimum temperature from the oxygen injection nozzle 6L + fuel injection nozzle 6X is combusted, and fuel is added to the inner wall of the theoretical combustion chamber 4Q + Elementary high-temperature water to superheated steam 50 are heated to the optimum temperature, theoretical air-fuel ratio combustion is performed, the target is 40 times the pressure of the existing jet combustion, and the combustion amount is 40 times the combustion amount. Therefore, the superheated steam 50 and the high-pressure high-temperature combustion chamber 5M combustion gas 49 approaching 200 MPa are injected, and when the on-off valve 1Q is closed, the high-power rocket combustion space is primed. Injecting by fuel ratio combustion or the like, the plurality of theoretical combustion chambers 4Q are liquid oxygen driven rocket combustion chambers and jet combustion chambers, and the compressed air combustion jet combustion theoretical combustion chamber 4Q is a theoretical air fuel ratio combustion of four times the fuel of the existing technology, The superheated steam 50 is produced with an increase of 3 times the amount of heat and is aimed at 200 MPa. The high pressure and high temperature combustion chamber 5M combustion gas 49 is injected to generate rotational output. The superheated steam 50 is injected from the thermal steam rocket nozzle 6A, the air 28a in front is sucked and injected, and as a simple injection engine 88s driven close to the existing jet engine, the liquid oxygen drive theoretical combustion chamber 4Q is combined with a plurality of space arrival costs. The target of 1 / 500,000 of the existing technology is that the atmospheric return speed is Mach 3 or less, and the atmosphere is flying with liquid oxygen 0, or the inner shaft device 60A extension rotor blade 7B is driven, ultra high speed rotation output + ultra high pressure injection propulsion output weight A large rotary wing jet airplane 70 corresponding to the increase is assumed.

図16の特大オスプレイ7Pは、既存回転翼機兼プロペラ機の改良発明簡単噴射機関88sを、圧縮空気駆動+燃料費0発電電気製造物選択駆動を選択可能としたもので、横型全動翼水重力タービン8B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、安価電気製造物駆動の理論燃焼室4Q等に液体酸素+電気+高温水を受給して、液体酸素を圧縮することで、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+液体燃料+高温水を24〜200MPa等超高圧に圧縮加熱して、複数入口出口の開閉弁1Qを閉止したロケット燃焼理論燃焼室4Q内の、酸素噴射ノズル6L+燃料噴射ノズル6Xより最適温度に加熱した酸素+燃料噴射燃焼し、理論燃焼室4Q内壁で燃料+酸素+高温水〜過熱蒸気50を最適温度に加熱理論空燃比燃焼にして、既存ジェット機燃焼の40倍圧力40倍燃焼量狙いにし、理論燃焼室4Q外周の過熱蒸気ロケット噴口6A+燃焼ガス噴射ノズル6Yより、200MPaに近付けた過熱蒸気50や高圧高温燃焼室5M燃焼ガス49を噴射にして、入口出口の開閉弁1Q閉では大出力ロケット燃焼宇宙利用全盛狙いとし、開閉弁1Q開では圧縮空気28a燃焼を理論空燃比燃焼等で噴射して、理論燃焼室4Q複数を液体酸素駆動のロケット燃焼室兼ジェット燃焼室とし、圧縮空気燃焼ジェット燃焼理論燃焼室4Qでは既存技術の4倍燃料の理論空燃比燃焼として、増大3倍熱量で200MPa狙い過熱蒸気50を製造、高圧高温燃焼室5M燃焼ガス49噴射で回転出力発生し、外周空気28a吸引流の過熱蒸気ロケット噴口6Aより過熱蒸気50を噴射して、前方の空気28a叉は真空を吸引噴射し、既存ジェットエンジンを超大出力とした簡単噴射機関88s駆動として、液体酸素駆動理論燃焼室4Q複数の合体で宇宙到達費用既存技術の1/50万月着陸帰還狙いとし、大気圏帰還速度マッハ3以下や大気中は液体酸素0で飛行や、内側軸装置60A延長回転翼兼プロペラ7A複数を駆動垂直上昇水平飛行して、超高速回転出力+超高圧噴射推進出力重量増大に対応する、超大型の特大オスプレイ7Pとする。 The extra large Osprey 7P shown in FIG. 16 is an improved invention simple injection engine 88s of an existing rotor blade / propeller aircraft, which can select a compressed air drive + a fuel cost 0 power generation electric product selection drive. Gravity turbine 8B Fuel cost 0 Power generation Extremely cheap electricity production from electricity + liquid air cold heat + hot water to superheated steam temperature heat supply equipment 3D, to the theoretical combustion chamber 4Q driven by cheap electricity products etc. Liquid oxygen + electricity + hot water And compressing liquid oxygen, the compression volume work rate is 21/60000 volume compression work rate of air compression, and liquid oxygen + liquid fuel + high-temperature water is compressed and heated to an ultrahigh pressure such as 24-200 MPa. In the rocket combustion theoretical combustion chamber 4Q in which the on-off valve 1Q at the plurality of inlets and outlets is closed, the oxygen + fuel injection combustion heated to the optimum temperature from the oxygen injection nozzle 6L + fuel injection nozzle 6X is performed, and the theoretical combustion chamber 4Q Fuel + oxygen + high-temperature water to superheated steam 50 heated to the optimum temperature on the wall, aiming at the theoretical air-fuel ratio combustion, aiming for 40 times the pressure and 40 times the combustion amount of existing jet combustion, superheated steam rocket nozzle 6A + combustion around the theoretical combustion chamber 4Q From the gas injection nozzle 6Y, the superheated steam 50 or the high-pressure high-temperature combustion chamber 5M combustion gas 49 approaching 200 MPa is injected. Compressed air 28a combustion is injected by theoretical air-fuel ratio combustion or the like, and a plurality of theoretical combustion chambers 4Q are used as liquid oxygen-driven rocket combustion chambers and jet combustion chambers. As the theoretical air-fuel ratio combustion, the superheated steam 50 is produced with a target of 200 MPa with an increased heat quantity of 3 times, and the rotation output is generated by the high-pressure high-temperature combustion chamber 5M combustion gas 49 injection. The superheated steam 50 is jetted from the superheated steam rocket nozzle 6A of the suction flow of the peripheral air 28a, the front air 28a or the vacuum is sucked and jetted, and the existing jet engine is driven as a simple injection engine 88s with a super-high output. Combining multiple theoretical combustion chambers 4Q, space arrival costs 1 / 500,000 months landing return target of existing technology, air return speed of Mach 3 or less, flight in atmosphere with liquid oxygen 0, inner shaft device 60A extension rotor and propeller A plurality of 7A drive vertical ascending horizontal flights, and an ultra-large extra-large Osprey 7P that responds to the increase in weight of ultra-high-speed rotation output + ultra-high-pressure injection propulsion output.

図17の大型オスプレイ7Qは、既存回転翼機兼プロペラ機の改良発明簡単ガス機関88qを、圧縮空気駆動+燃料費0発電電気製造物選択駆動を選択可能としたもので、横型全動翼水重力タービン8B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、安価電気製造物駆動の理論燃焼室4Q等に液体酸素+電気+高温水を受給して、液体酸素を圧縮することで、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+液体燃料+高温水を24〜200MPa等超高圧に圧縮加熱して、複数入口の開閉弁1Qを閉止したロケット燃焼理論燃焼室4Q内の、酸素噴射ノズル6L+燃料噴射ノズル6Xより最適温度に加熱した酸素+燃料噴射燃焼し、理論燃焼室4Q内壁で燃料+酸素+高温水〜過熱蒸気50を最適温度に加熱理論空燃比燃焼にして、既存ジェット機燃焼の40倍圧力40倍燃焼量狙いにし、ジェット燃焼理論燃焼室4Qでは既存技術の4倍燃料燃焼の理論空燃比燃焼として、増大3倍熱量で200MPa等の過熱蒸気50を製造し、過熱蒸気ロケット噴口6Aより噴射して、排気噴射やロケット噴射により4倍燃焼量や40倍圧力噴射狙い高圧高温燃焼室5M噴射し、既存回転翼機兼プロペラ機を大改良した大型オスプレイ7Qとして、簡単ガス機関88qの回転出力で回転翼兼プロペラ7A複数駆動垂直上昇水平飛行する、排気噴射+ロケット噴射で回転出力+噴射推進出力にし、内側軸装置60A延長回転翼兼プロペラ7A駆動して、40倍圧力噴射が可能なロケット噴射+ジェット燃焼+回転出力+噴射推進出力にする、圧縮空気+液体酸素駆動理論燃焼室4Q複数の合体として、宇宙到達費用既存技術の1/50万月着陸帰還狙いとし、大気圏帰還速度マッハ3以下や大気中は液体酸素0で飛行や、内側軸装置60A延長回転翼兼プロペラ7A複数を駆動垂直上昇水平飛行して、超高速回転出力+超高圧噴射推進出力重量増大に対応する、大型の大型オスプレイ7Qとする。 The large Osprey 7Q shown in FIG. 17 is an improved invention of the existing rotor blade / propeller aircraft. The simple gas engine 88q can be selected from compressed air drive + zero fuel cost electric product selection drive. Gravity turbine 8B Fuel cost 0 Power generation Extremely cheap electricity production from electricity + liquid air cold heat + hot water to superheated steam temperature heat supply equipment 3D, to the theoretical combustion chamber 4Q driven by cheap electricity products etc. Liquid oxygen + electricity + hot water And compressing liquid oxygen, the compression volume work rate is 21/60000 volume compression work rate of air compression, and liquid oxygen + liquid fuel + high-temperature water is compressed and heated to an ultrahigh pressure such as 24-200 MPa. In the rocket combustion theoretical combustion chamber 4Q in which the on-off valve 1Q at the plurality of inlets is closed, the oxygen + fuel injection combustion heated to the optimum temperature from the oxygen injection nozzle 6L + fuel injection nozzle 6X and the inner wall of the theoretical combustion chamber 4Q Fuel + oxygen + hot water to superheated steam 50 is heated to the optimum temperature, and the theoretical air-fuel ratio combustion is performed, aiming for 40 times the pressure and 40 times the combustion amount of the existing jet combustion, and the jet combustion theoretical combustion chamber 4Q is four times the fuel combustion of the existing technology As the stoichiometric air-fuel ratio combustion, superheated steam 50 of 200 MPa or the like is manufactured with a triple heat quantity, injected from superheated steam rocket nozzle 6A, and targeted for quadruple combustion quantity or 40 times pressure injection by high pressure and high temperature by exhaust injection or rocket injection As a large Osprey 7Q with 5M injection in the combustion chamber and a greatly improved existing rotor blade / propeller aircraft, the rotor / propeller 7A is driven in multiple vertical ascending horizontal flight with the rotational output of the simple gas engine 88q, and rotated by exhaust injection + rocket injection. Rocket injection + jet combustion capable of 40 times pressure injection by driving output + injection propulsion output and driving inner shaft device 60A extension rotor blade and propeller 7A Compressed air + liquid oxygen drive theoretical combustion chamber 4Q combined with rotation output + injection propulsion output As a combination of multiple combustion chambers 4Q, the space arrival cost is aimed at 1 / 500,000 months landing return, atmospheric return speed Mach 3 or less and in the atmosphere Flying with liquid oxygen 0, driving the inner shaft device 60A extension rotor blades and propellers 7A vertically flying horizontally, and making a large large osprey 7Q that supports ultra-high-speed rotation output + ultra-high-pressure jet propulsion output weight increase .

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、横型全動翼水重力タービン8B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等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、水噴射速度マッハ3等+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量200倍発電量等の横型全動翼水重力タービン8B発電で、極端に安価発電にする可能性がある。 Compared with the existing pumped-storage power generation, the horizontal full-blade water gravity turbine 8B power generation aiming at a resource price of 0 fuel cost of 0 power generation less than 1/2 of the nuclear power generation will be explained. Gravity acceleration in vacuum is added to injection speed Mach 3 etc., and work rate is proportional to speed + proportional to height, so water injection speed Mach 3 etc. + gravity acceleration in vacuum = Mach 30 etc. , 100 times vertical speed 1/100 mass vertical water drive + 1 h double axis reversal drive, maximum power of 9.8 m / s in gravity acceleration in vacuum, 200 sets vertical to world's highest building height of 828 m There is a possibility of extremely low-priced power generation with a horizontal full-blade water gravity turbine 8B power generation with the same power generation amount 200 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、横型全動翼水重力タービン8B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、円筒タービン翼群8A駆動で同発電量となり、1/215容積水駆動で200倍発電量100組連結の1台で20000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。 In the process of comparing the horizontal full-blade water gravity turbine 8B power generation with the existing thermal power nuclear steam turbine power generation, aiming for the cost of resource 0 fuel cost 0 power generation less than 1/2 of the nuclear power generation, the atmospheric pressure 100 ° C according to Boyle's law Steam of 1,700 times the volume of water at 760 mmHg becomes 43,000 times the volume of water at an exhaust temperature of 29 ° C. and a vacuum pressure of 30 mmHg. Since the speed is less than 1 / 100th of the speed of sound 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 / 433,000 volume 29 ° C water drive of the steam 29 ° C volume, the same amount of power is generated by driving the cylindrical turbine blade group 8A, and 100 units of 200 times the amount of generated power are connected by 1/215 volume water drive. If it is calculated by elementary school science, such as a power generation amount of 20000 times, there is a possibility that extremely low-priced power generation becomes an astronomical large power generation amount.

横型全動翼水重力タービン8B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。 Horizontal full-blade hydrogravity turbine 8B power generation Extremely inexpensive power generation as an electric product prime, electricity + liquid air cold heat + superheated steam temperature supply equipment 3D receives superheated steam to methane hydrate under the seabed or permafrost land Injecting enclosures provide methane recovery, pasture grazing conversion in permafrost areas, superheated steam injection in oil sands, oil shale, and aging oil collection areas, and vaporization, recovery, liquefaction storage, etc. There is a possibility of receiving cheap steam for mass production of cheap foods and using it for agricultural, industrial, industrial and mining industries to make full use of thermal energy.

横型全動翼水重力タービン8B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、液体酸素駆動と通常駆動を合体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、簡単ガス機関88qや簡単空気噴射機関88rや簡単噴射機関88s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。 Horizontal full-blade hydrogravity turbine 8B 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, liquid oxygen drive and normal drive combined drive To make the simple gas engine 88q, the simple air injection engine 88r, and the simple injection engine 88s by compressing the liquid oxygen 5K to 21/50000 volume compression work rate. Driving, there is a possibility that CO2 exhaust and fuel costs will be close to 1/10 in a car, a ship may be close to 10 times the speed with the same fuel cost, and an airplane will have a space arrival cost of 1 / 500,000, etc. There is a possibility of making a major revolution in the use of cold energy, such as making day trips anywhere on the planet 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で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の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、 1Q:開閉弁、 1Y:複数段燃焼室、 1b:燃料(液体燃料+液化可能気体燃料) 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) 1J:燃料制御弁、 1K:液体燃料制御弁、 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(船底に空気や燃焼ガスや過熱蒸気等を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熱交換器で複数回熱回収して残りを温熱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、 2X:空気熱交換器 2Y:圧縮空気熱交換器(液体空気冷熱+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、 3f:簡単多段圧縮機、 3i:簡単多段圧縮機、 3s:簡単圧縮機、 3t:簡単多段圧縮機、 3u:空気タービン、 3A:撥水コーティング、 3B:水圧力往復機関、 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 3G:理論燃焼歯車機関、 3H:往復ピストン、 3J:理論燃焼往復機関、 3K:外接歯車、 3L:複数段燃焼室、 3M:水蒸気圧力往復機関、 3N:水蒸気圧力歯車機関、 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、 3a:撥水鍍金、 3b:撥水コーティング、 4C:対向同期歯車、 4D:直列同回転歯車、 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、 4Q:理論燃焼室(過熱蒸気製造で理論空燃比燃焼既存の4倍燃焼量等や20倍圧力過熱蒸気噴射狙う燃焼室)、 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、 5h:精留塔排ガス管、 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、 5G:高圧高温水加熱管、 5H:高圧高温水加熱管、 5H:高圧高温過熱蒸気管、 5K:液体酸素、 5K:液体酸素室、 5L:液体窒素、 5L:液体窒素室、 5M:高圧高温燃焼室、 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:過熱蒸気ロケット噴口、 6B:圧縮空気噴射ノズル、 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、 7D:簡単ガス機関自動車、 7E:簡単ガス機関船舶、 7F:簡単ガス機関飛行機、 7G:簡単水噴射機関船舶、 7H:簡単噴射機関飛行機、 7I:簡単ガス機関自動車、 7J:簡単ガス機関船舶、 7K:簡単ガス機関飛行機、 7L:簡単空気噴射機関船舶、 7M:簡単噴射機関飛行機、 7N:回転翼飛行機、 7O:回転翼噴射飛行機、 7P:特大オスプレイ、 7Q:大型オスプレイ、 7d:簡単ガス機関自動車、 7e:簡単ガス機関船舶、 7f:簡単ガス機関飛行機、 7g:簡単水噴射機関船舶、 7h:簡単噴射機関飛行機、 7i:回転翼飛行機、 7j:回転翼噴射飛行機、 7k:簡単ガス機関自動車、 7l:簡単ガス機関船舶、 7m:簡単ガス機関飛行機、 7n:簡単水噴射機関船舶、 7o:簡単噴射機関飛行機、 7p:回転翼飛行機、 7q:回転翼噴射飛行機、 7r:簡単ガス機関自動車、 7s:簡単ガス機関船舶、 7t:簡単ガス機関飛行機、 7u:簡単水噴射機関船舶、 7v:簡単噴射機関飛行機、 7w:回転翼飛行機、 7x:回転翼噴射飛行機、 7y:特大オスプレイ、 7z:大型オスプレイ、 8b:タービン翼(サイクル数や比重大物質性質仕事速度や周速度に合せた角度や曲線や回転半径直列同回転歯車4Dとしたタービン翼) 8c:タービン翼(円筒外面に直線長大タービン翼を設けて内周や外周の全自動加工や軽量化を狙う) 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、 8k:内側圧縮翼、 8m:外側圧縮翼、 8n:内側出力翼、 8p:外側出力翼、 8q:内側圧縮翼(回転速度や周速度に合せた角度や曲線や回転半径二重反転とした圧縮翼) 8r:外側圧縮翼(回転速度や周速度に合せた角度や曲線や回転半径二重反転とした圧縮翼) 8s:内側出力翼(回転速度や周速度に合せた角度や曲線や回転半径二重反転とした出力翼) 8t:外側出力翼(回転速度や周速度に合せた角度や曲線や回転半径二重反転とした出力翼) 8A:円筒タービン翼群(横型円筒タービン翼群として全自動加工や精密組立可能にする) 8B:横型全動翼水重力タービン(磁気利用同期歯車+磁気利用軸受荷重0接近にする) 8C:横型全動翼比重大物質重力タービン(磁気利用同期歯車+磁気利用軸受荷重0接近にする) 8R:横型全動翼タービン(対向全動翼弾み車タービン直列全動翼弾み車タービン食込全動翼弾み車タービン) 8R:横型全動翼タービン(円筒外面に直線長大タービン翼を設けて内周や外周の全自動加工や軽量化を狙う) 8R:横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水の真空度上昇中の重力加速度使用必須とする) 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) 8V:竪型全動翼水重力タービン、 8W:竪型全動翼比重大物質重力タービン、 8X:竪型全動翼水重力タービン(9B9Cで軸受荷重0接近+横軸軸受荷重0接近とした) 8Y:竪型全動翼比重大物質重力タービン(9B9Cで軸受荷重0接近+横軸軸受荷重0接近とした) 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にする) 9b:上吸引下反発磁石、 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、 9M:嵌合組立部、 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、 16:水平軸板(精密組立を容易にする円盤) 16A:水平軸、 11D:気体専用冷却室、 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、 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) 38H:理論スクリュウ船舶、 38J:理論噴射船舶、 38T:理論噴射飛行機、 38U:理論プロペラ飛行機、 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) 60c:内側動翼、 60d:外側動翼、 60e:外入口翼、 60f:内入口翼、 60g:外中間翼、 60h:内中間翼、 60j:内出口翼、 60k:外出口翼、 76:歯車装置(磁気摩擦動力伝達装置を含む) 77B:ロケット外箱、 77C:二重反転機外箱、 77F:噴射部外箱、 77G:円筒回転部、 77a:タービン外箱、 77b:圧縮機外箱、 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(高圧高温燃焼室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(高圧高温燃焼室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(既存技術で同様にする) 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:簡単ガス機関、 88b:簡単噴射機関、 88c:簡単水噴射機関、 88d:簡単ガス機関、 88f:簡単噴射機関、 88e:簡単水噴射機関、 88g:液体酸素製造機88p:液体酸素製造機、 88i:簡単ガス機関、 88j:簡単水噴射機関、 88k:簡単噴射機関、 88l:液体酸素製造機、 88m:簡単ガス機関、 88n:簡単水噴射機関、 88o:簡単噴射機関、 88p:液体酸素製造機、 88q:簡単ガス機関、 88r:簡単空気噴射機関、 88s:簡単噴射機関、 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) 88C:理論空気噴射部、 88M:理論水噴射部、 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 and divided into liquid air cold heat + superheated steam heat) Gravity energy rises storage spray accelerates gravitational acceleration in vacuum 0: Various energy storage cycle coalescing engine and coalescence method (various heat energy is heated by solar heat or geothermal heat, etc., and is recovered by compressing heat with a heat pump as liquid temperature, liquid air cooling + Divided and stored in superheated steam temperature ・ Used with a heat retaining device when using liquid metal under 500 ℃ ・ Shock energy is used to extend the working time by providing silicon blade coating or fluorine resin coating on turbine blades and small metal balls・ Gravity energy is increased by a lifting device Preservation of jets Gravity acceleration in vacuum Accelerated gravitational acceleration and conversion of generated energy Engine and various energy merging 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 multi-stage heat pump (heat energy is air temperature, heat pump (various air compressors) multiple times 1K: Liquid fuel control valve, 1L: Fuel heating pipe, 1Q: On-off valve, 1Y: Multistage combustion chamber, 1b: Fuel (Liquid fuel + liquefaction) 1b: Fuel (liquid fuel + liquefiable gas fuel) 1b: Fuel pipe (provided so that the fuel injection temperature becomes the optimum temperature) 1c: Liquid fuel, 1d: Mercury, 1g: Force accelerating unit, 1h: Horizontal axis (axis that alternates rotation direction of outer shaft device and inner shaft device) 1J: Fuel control valve, 1K: Liquid fuel control valve, 2: Solar heater (Solar light with long lens) 2a: Acceleration of natural phenomena (When the leftover food, which has almost zero change in the air, moves to a nearby river, the amount of microorganisms that approach zero will increase overnight.) 2a: Acceleration of natural phenomena (In power generation, cold water 28a is mixed with seawater. The natural phenomenon is accelerated. The seawater is supplied to the sea. Nutrients such as nitrogen, oxygen and CO2 are supplied. Microorganisms increase and foods such as fish and kombu increase. (Equipment) 2a: Acceleration of natural phenomena (ships supply nutrients such as nitrogen, oxygen and CO2 into the sea, aiming for the digestive ability of microorganisms tens of thousands of times in the forest, phytoplankton, seaweed, etc. by breeding food chains, etc. Increasing human food) b: Slight water resistance (low-speed injection of air, combustion gas, superheated steam, etc. to the bottom of the ship to reduce water resistance) 2c: Insulating material, 2d: Long lens (Convex lens cross-section is linearly extended rectangle, multiple use 2e: water surface, 2g: specific material acceleration direction, 2A: heat-resistant material, 2B: heat absorbing material, 2C: 1 to multi-stage compression heat recovery device (heat pump with heat energy as air temperature) 2): Specific critical substances (including alloys, platinum spheres, gold spheres, tungsten alloy powder sintered spheres, silver spheres, copper) Spheres, tin spheres, lead spheres, zinc spheres, aluminum spheres, indium, cadmium, gallium, thallium, bismuth, etc. 2E: Specific material (coated platinum alloy ball, coated gold alloy ball, coated tungsten alloy powder sintered ball with silicon resin coating or silicon resin coating)・ Coated silver alloy balls ・ Coated bismuth alloy balls ・ Coated copper alloy balls ・ Coated tin alloy balls ・ Coated lead alloy balls ・ Coated zinc alloy balls ・ Coated aluminum alloy balls 2H: Cold and hot seawater mixer, 2X: Air heat exchanger 2Y: Compressed air heat exchanger (liquid air cold heat + heat production) 2Z: Specific critical material heat exchanger (used for temperature control of liquid metal below 500 degrees) 3a: water repellent plating, 3f: simple multistage compressor, 3i: simple multistage compressor, 3s: simple compressor, 3t: simple multistage compressor, 3u: air turbine, 3A: water repellent coating, 3B: water pressure reciprocating Seki, 3D: Electricity + liquid air cooling + superheated steam temperature supply equipment (cooling + heat production by gravity power generation and supplying liquid oxygen and liquid nitrogen Supplying automobiles, ships and airplanes and supplying with superheated steam Methane injected into methane hydrate 3E: Specific critical substances (specific critical substances that are liquid at normal temperatures such as mercury and water) 3E: Specific critical substances (low-melting-point alloys that are liquids of less than 500 degrees C and high-temperature liquid alloys) 3F: Oxygen pressure reciprocating engine 3G: Theoretical combustion gear engine, 3H: Reciprocating piston, 3J: Theoretical combustion reciprocating engine, 3K: External gear, 3L: Multistage combustion chamber, 3M: Steam pressure reciprocating engine, 3N: Steam pressure gear Engine, 3P: Theoretical expansion engine (the gas volume is inversely proportional to the pressure, the best engine + oxygen hydrogen increase combustion aim) 3Q: Theoretical expansion engine (The best engine in Boyle's law + the highest in vacuum 3R: theoretical gas turbine (theoretical best gas turbine whose gas volume is inversely proportional to pressure) 3S: theoretical steam turbine (theoretical best steam turbine whose gas volume is inversely proportional to pressure) 3T: theoretical gas compressor (Theoretical best gas compressor whose gas volume is inversely proportional to pressure) 3U: Theoretical turbine, 3V: Pump engine (uses various existing pumps in the engine) 3X: Compressor engine (uses existing various compressors in the engine) 3Y : Counter rotating engine (engine whose gas volume is inversely proportional to pressure) 3Z: Oxygen pressure gear engine, 3a: Water repellent plating, 3b: Water repellent coating, 4C: Opposite synchronous gear, 4D: In-line rotating gear, 4F : Combustion gas reciprocating engine, 4H: Heat absorption tube (The long lens 2d collects sunlight into the heat absorption tube in a straight line, and the air temperature inside the tube is heated to the maximum to increase the outside air temperature. 4J: Storage battery drive wheel, 4K: Theoretical expansion engine vehicle, 4Q: Theoretical combustion chamber (combustion chamber aiming at 20 times pressure superheated steam injection, etc.) Theoretical compression chamber, 4Y: Theoretical combustion chamber (combustion chamber for high-temperature pyrolysis, electrolysis and combustion of water in water vapor, aiming at compound 0) 4Z: Combustion gas gear engine, 4X: Turbine blade cross section (cross-sectional area enlarged surface area) 4a: Liquid oxygen pump, 4c: Water pump, 4d: Gear device, 4e: Roller, 4f: Rotation support, 5: Air injection nozzle, 5a: High-pressure high-temperature combustion gas control valve, 5b : Compression intake air path, 5d: Combustion flow inner wall, 5e: Ultra high pressure oxygen, 5h: Rectification tower exhaust pipe, 5A: Supply valve, 5B: Cooling fin, 5C: Exhaust chamber 5D: Exhaust valve 5E: Supply chamber 5F: Oxygen heating Tube, 5G: Steam heating tube, 5G: High pressure high temperature water heating tube, 5H: High pressure high temperature water heating tube, 5H: High pressure high temperature superheated steam tube, 5K: Liquid oxygen, 5K: Liquid oxygen chamber, 5L: Liquid nitrogen, 5L: Liquid nitrogen chamber, 5M: high pressure high temperature combustion chamber, 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 rocket nozzle, 6B: compressed air injection nozzle, 6E: specific material injection nozzle, 6F: water injection nozzle, 6G : Static blade, 6H: Drain pipe, 6L: Oxygen injection nozzle, 6W: Specific critical material accelerator (liquid specific critical material 3E pressure and specific gravity difference, specific critical material 3E and 2E mixed injection) 6X: Fuel injection nozzle, 6X: Afterburner (combustion combined with the fuel injection cold heat 28a combustion flow 6Y in the intake air flow and the space rises due to a large increase in the amount of fuel combustion) 6Y: combustion gas injection nozzle (cooling 28a combustion flow) 6Z: steam injection nozzle, 7A: propeller, 7B : Rotor, 7C: Screw, 7D: Simple gas engine car, 7E: Simple gas engine ship, 7F: Simple gas engine airplane, 7G: Simple water injection engine ship, 7H: Simple injection engine airplane, 7I: Simple gas engine automobile 7J: simple gas engine ship, 7K: simple gas engine airplane, 7L: simple air injection engine ship, 7M: simple injection engine airplane, 7N: rotary wing airplane, 7O: rotary wing injection airplane, 7P: extra large Osprey, 7Q: Large Osprey, 7d: Simple gas engine vehicle, 7e: Simple gas engine ship, 7f: Simple gas engine airplane, 7g: Simple water 7h: Simple gas engine car, 7l: Simple gas engine airplane, 7n: Simple gas engine airplane, 7n: Simple injection engine airplane, 7i: Rotary wing airplane, 7j: Rotary wing injection airplane, 7k: Simple gas engine automobile, 7l: Simple gas engine airplane Engine ship, 7o: Simple injection engine airplane, 7p: Rotary wing airplane, 7q: Rotary wing injection airplane, 7r: Simple gas engine automobile, 7s: Simple gas engine ship, 7t: Simple gas engine airplane, 7u: Simple water injection engine Ship, 7v: simple injection engine plane, 7w: rotary wing plane, 7x: rotary wing injection plane, 7y: extra large osprey, 7z: large osprey, 8b: turbine wing (cycle number and specific material properties work speed and peripheral speed Turbine blades with the same angle, curve, and rotation radius in series with the same rotation gear 4D) 8c: Turbine blades (inner circumference with linear long turbine blades on the outer surface of the cylinder) 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, 8k: Inner compression blade, 8m: Outer compression blade, 8n: Inner output blade, 8p: Outer output blade, 8q: Inner compression blade (angle, curve and rotation radius according to the rotational speed and peripheral speed) 8r: Outer compression blade (angle, curve and rotation radius according to rotation speed and circumferential speed, compression blade with rotation radius double reversal) 8s: Inner output blade (according to rotation speed and circumferential speed) 8t: Outer output blade (output blade with angle, curve and rotation radius double reversed according to rotation speed and peripheral speed) 8A: Cylindrical turbine blade group (horizontal type) Fully automatic machining and precision assembly are possible as a cylindrical turbine blade group) 8B: Horizontal Type full blade hydrogravity turbine (magnetization synchronous gear + magnetic utilization bearing load approach 0) 8C: horizontal full blade ratio critical material gravity turbine (magnetization synchronization gear + magnetic bearing load approach 0) 8R: Horizontal type all-blade turbine (opposite all blade impeller turbine series full blade impeller turbine bite all rotor blade impeller turbine) 8R: Horizontal all blade turbine (all the inner and outer circumferences are provided with a linear long turbine blade on the outer surface of the cylinder) 8R: Horizontal type full-blade water gravity turbine (existing steam turbine is a stationary blade and the damming output approaches 0 because all blades are indispensable and the work rate is 1 / 3.6 that of platinum balls) 8M: Vertical all-blade water-gravity turbine (6 types of cylindrical turbine blade group fitting assembly + magnetic utilization bearing load close to 0) 8N: Specific gravity of vertical type moving blade Mass Gravity Turbine (6 types of cylindrical turbine blade group fitting assembly + magnetic utilization bearing load approach 0) 8R: Horizontal all blade hydrogravity turbine (cylindrical turbine blade group series opposed synchronous rotation + magnetic utilization bearing load approach 0) 8S: Gravity turbine with horizontal total blade ratio critical material (cylindrical turbine blade group in series opposed synchronous rotation + close to magnetic bearing load 0) 8P: Vertical type full blade hydrogravity turbine (six types of cylindrical turbine motion) Blade group fitting assembly + Magnetic bearing load 0 approach + Super high speed peripheral speed) 8Q: Vertical type moving blade ratio critical material gravity turbine (6 types of cylindrical turbine blade group fitting assembly + magnetic bearing load 0) 8T: Horizontal full blade hydrogravity turbine (cylindrical turbine blade group serially opposed synchronous rotation + magnetic utilization bearing load 0 approach + super high speed peripheral speed) 8U: Horizontal full blade ratio is significant Material weight Turbine (cylindrical turbine blade group series counter synchronous rotation + magnetized bearing load 0 approach + super high speed peripheral speed) 8V: vertical all-blade water gravity turbine, 8W: vertical all-blade ratio critical material gravity turbine, 8X : Vertical type blade dynamic gravity turbine (with 9B9C approaching bearing load 0 + horizontal axis bearing load 0 approach) 8Y: Vertical type full blade ratio material gravity turbine (9B9C approaching zero bearing load + horizontal axis bearing load) 9: Wear-resistant annular assembly (A fitting assembly method in which only the critical material flow path including 8c is made of a cemented carbide to reduce the weight of the annular material is produced.) 9b: Upper attractive lower repulsion magnet, 9A: Cylindrical annular assembly (Abrasion-resistant cylindrical annular assembly blade group is made into 6 types to make the structure simple, the number of parts is small, fully automatic processing is easy, assembly is easy, and weight reduction is easy.) 9A: Cylindrical annular assembly (fixed inlet outer blade 60E + outer annular) Wing 60G + Outlet fixed outer wing Cylindrical outer rotor blade group 60D is configured by 0J fitting, and cylindrical fixed rotor blade 60H + inner annular blade 60H + outlet fixed inner blade 60K is fitted to form cylindrical inner rotor blade group 60C) 9B: Repulsive permanent magnet, 9C : Suction permanent magnet, 9D: compressed air part, 9E: vacuum part, 9M: fitting assembly part, 9Q: vertical parallel plate (vertical parallel plate for guiding the blast air to the storage stern) 10: hull, 10A: cabin 10b: Cockpit, 10c: Control room, 10d: Guest room, 10e: Cargo compartment, 16: Horizontal shaft (disc for facilitating precision assembly) 16A: Horizontal shaft, 11D: Gas cooling room, 21: Solar heating 24 (combustion gas control valve, 24A: compressed air control valve, 25: superheated steam control valve, 25b: fuel control valve, 25c: fuel pipe) 28a: Air 28 a: Cold energy (compressed air 28a is compressed by a heat pump and stored in the form of 50 heated superheated steam of compressed air heat + compressed air 28a cold heat containing liquid oxygen or liquid nitrogen) 28b: Compressed air heat amount, 28A: Intake air path, 28B : Airway entrance, 38: Rotating guide, 38a: Flight trunk, 38b: Flying wing, 38c: Flying wing, 38d: Vertical wing, 38e: Wing front edge, 38g: Water wing, 38h: Surfing boat, 38B: Air suction jet ship (with 79S79T79Y79Z) 38C: Water suction jet ship (with 79U79X) 38H: Theoretical screw ship, 38J: Theoretical jet ship, 38T: Theoretical jet airplane, 38U: Theoretical propeller airplane, 39A: Solar thermal gravity airplane, 39B: Solar thermal gravity rotating plane, 39C: Solar thermal gravity helicopter, 39D: Screw ship, 39G: Solar thermal gravity Aircraft, 39H: Oxygen coalescence screw ship, 39J: Oxygen coalescence injection ship, 39K: Oxygen coalescence screw injection ship, 39L: Oxygen coalescence jet airplane, 39M: Oxygen coalescence propeller airplane, 39N: Oxygen coalescence propeller airplane, 39P: Oxygen Combined rotary wing airplane, 39Q: Oxygen combined screw ship, 39R: Oxygen combined injection ship, 39S: Oxygen combined screw injected ship, 39T: Oxygen combined injection airplane, 39U: Oxygen combined propeller airplane, 40A: Rudder, 49: Combustion gas, 50: Superheated steam, 50: Superheated steam chamber, 50: Warmth (compressed air 28a is compressed with a heat pump and stored in the form of 50 heat of compressed air heat + compressed air 28a cold) 50A: Steam, 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 (change from 28a) 55B: Transmission, 60A: Inner shaft device (turbine blade) 60B: Outer shaft device (turbine blade equipped device) 60C: Cylindrical inner rotor blade group (Wear resistant cylindrical annular assembly fixed rotor blade group including fully automatic processing easy assembly) 60D: Cylindrical outer rotor blade group (Ease of easy wear and assembly including wear-resistant cylindrical annular assembly fixed rotor blade group) 60E: Outer fixed outer blade (inlet blade for annular assembly fixing outer rotor blade group) 60F: Inlet fixed inner blade (inner motion) 60G: Outer annular blade (intermediate blade for annular assembly of outer blade group) 60H: Inner annular blade (intermediate blade for annular assembly of inner blade group) 60J: Outlet fixed outer blade (Outer blade 60K: Outlet fixed inner blade (exit blade for annular assembly fixing of inner rotor blade group) 60c: Inner rotor blade, 60d: Outer rotor blade, 60e: Outer inlet blade, 60f: Inner inlet blade 60g: outer intermediate blade, 60h: inner intermediate blade, 60j: inner outlet blade, 60k: outer outlet blade, 76: gear device (including magnetic friction power transmission device) 77B: rocket outer box, 77C: counter rotating machine Outer box, 77F: Injection unit outer box, 77G: Cylindrical rotating unit, 77a: Turbine outer box, 77b: Compressor outer box, 80: Bearing (including magnetic bearing + air bearing) 80a: Thrust bearing (magnetic bearing + air bearing) 80A: Joint, 80B: Fastener, 80Y: Liquid air suction water jet (High pressure high temperature combustion chamber 5M High pressure high temperature steam chamber 5N is received and fuel injected and burned to 5M multiple times, 5N is inner and inner circumference Multiple times from the outer circumference 80Z: Liquid air suction water jet (receives high pressure high temperature combustion chamber 5M high pressure high temperature steam chamber 5N, and injects fuel into 5M multiple times and burns 5N inside) 84: Counter-rotating magnetic friction device (fixed) 84: Counter-rotating magnetic friction device (fixed) 84Y: Counter-rotating gear device (same for existing technology) 85: Counter-rotating magnetic device (magnet gear height is small) 85Y: Counter-rotating gear device (reciprocal reverse rotation using the existing horizontal shaft 1h gear) 88a: simple gas engine, 88b: simple injection engine, 88c: simple Water injection engine, 88d Simple gas engine, 88f: Simple injection engine, 88e: Simple water injection engine, 88g: Liquid oxygen production machine 88p: Liquid oxygen production machine, 88i: Simple gas engine, 88j: Simple water injection engine, 88k: Simple injection engine, 88l : Liquid oxygen production machine, 88m: simple gas engine, 88n: simple water injection engine, 88o: simple injection engine, 88p: liquid oxygen production machine, 88q: simple gas engine, 88r: simple air injection engine, 88s: simple injection engine 88A: oxygen combined air injection section (rocket combustion + jet combustion + steam injection and combined injection) 88B: oxygen combined air injection section (ultra-high pressure rocket combustion + jet combustion + superheated steam injection suction) 88C: theoretical air injection section, 88M: Theoretical water injection unit, 88K: Oxygen combined water injection unit (rocket combustion + jet combustion + water vapor injection and combined injection) 88L: Oxygen combined water injection unit (ultra-high pressure rocket combustion + jet combustion + superheated steam injection suction) 95a: combustion gas reservoir, 95b: compressed air reservoir, 95c: superheated steam reservoir, 103: cold energy recovery device,

Claims (457)

タービン翼(8b)タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)1〜20組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体にする各種エネルギ保存サイクル合体機関及び合体方法。   Turbine blade (8b) Turbine blade (8b) Cylindrical turbine blade group (8A) A horizontal shaft (16A) is fixed to both sides by a horizontal shaft plate (16), and the horizontal shaft (16A) is equipped with an opposing synchronous gear (4C). Thus, a pair of counter-synchronized rotations are provided, and a series rotation gear (4D) is provided between the horizontal shafts (16A), and each set is rotated in the same direction in the same vertical direction, so that the magnetic bearing load approaches 0+ ( 4C) (4D) Horizontal full-blade water gravity turbine (8B) 1-20 sets driven by electric gears with magnetic gears and super-high-speed circumferential speed + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8 s) Various energy storage cycle coalescence engines and coalescence methods for coalescence of outer output blade (8t) + horizontal shaft bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)21〜40組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). The counter-synchronized rotation is provided with a series rotation gear (4D) between the horizontal shafts (16A), and each set is rotated in the same direction in the same direction in the vertical direction, so that the magnetic bearing load approaches 0+ (4C) (4D) Horizontal type full-blade water gravity turbine (8B) 21-40 sets driven by electric gears with magnetic gears and super-high speed peripheral drive + inner compressor blade (8q) outer compressor blade (8r) inner output blade (8s) outer output Various energy storage cycle merging engines and merging methods for merging wings (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)41〜60組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). The counter-synchronized rotation is provided with a series rotation gear (4D) between the horizontal shafts (16A), and each set is rotated in the same direction in the same direction in the vertical direction, so that the magnetic bearing load approaches 0+ (4C) (4D) Horizontal full-blade hydrogravity turbine (8B) 41-60 sets driven by electric gears with magnetic gears and super-high-speed circumferential drive + inner compressor blade (8q) outer compressor blade (8r) inner output blade (8s) outer output Various energy storage cycle merging engines and merging methods for merging wings (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)61〜80組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). The counter-synchronized rotation is provided with a series rotation gear (4D) between the horizontal shafts (16A), and each set is rotated in the same direction in the same direction in the vertical direction, so that the magnetic bearing load approaches 0+ (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 61-80 sets driven by electric gears with magnetic gears and ultra-high speed peripheral drive + inner compressor blade (8q) outer compressor blade (8r) inner output blade (8s) outer output Various energy storage cycle coalescence engines and coalescence methods for merging of blade (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)81〜100組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). The counter-synchronized rotation is provided with a series rotation gear (4D) between the horizontal shafts (16A), and each set is rotated in the same direction in the same direction in the vertical direction, so that the magnetic bearing load approaches 0+ (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 81-100 sets driven by electric gears with magnetic gears and super-high-speed circumferential speed + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output Various energy storage cycle merging engines and merging methods for merging wings (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)101〜120発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). The counter-synchronized rotation is provided with a series rotation gear (4D) between the horizontal shafts (16A), and each set is rotated in the same direction in the same direction in the vertical direction, so that the magnetic bearing load approaches 0+ (4C) (4D) Horizontal type full-blade water gravity turbine (8B) 101-120 generator electric product drive with magnetic gears and super high speed circumferential speed + inner compressor blade (8q) outer compressor blade (8r) inner output blade (8s) outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combined engine and various energy storage cycle combining engines and combining methods. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)121〜140組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). The counter-synchronized rotation is provided with a series rotation gear (4D) between the horizontal shafts (16A), and each set is rotated in the same direction in the same direction in the vertical direction, so that the magnetic bearing load approaches 0+ (4C) (4D) Horizontal type full-blade water gravity turbine (8B) 121-140 sets driven by electric gears with magnetic gears and super-high-speed circumferential speed drive + inner compressor blade (8q) outer compressor blade (8r) inner output blade (8s) outer output Various energy storage cycle coalescence engines and coalescence methods for merging of blade (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)141〜160組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). The counter-synchronized rotation is provided with a series rotation gear (4D) between the horizontal shafts (16A), and each set is rotated in the same direction in the same direction in the vertical direction, so that the magnetic bearing load approaches 0+ (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 141-160 set with magnetic gears and super high speed circumferential speed drive Electric product drive + inner compressor blade (8q) outer compressor blade (8r) inner output blade (8s) outer output Various energy storage cycle merging engines and merging methods for merging wings (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)161〜180組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). The counter-synchronized rotation is provided with a series rotation gear (4D) between the horizontal shafts (16A), and each set is rotated in the same direction in the same direction in the vertical direction, so that the magnetic bearing load approaches 0+ (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 161-180 sets driven by electric gears with magnetic gears and super-high speed peripheral drive + inner compressor blade (8q) outer compressor blade (8r) inner output blade (8s) outer output Various energy storage cycle merging engines and merging methods for merging wings (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)181〜200組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). The counter-synchronized rotation is provided with a series rotation gear (4D) between the horizontal shafts (16A), and each set is rotated in the same direction in the same direction in the vertical direction, so that the magnetic bearing load approaches 0+ (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 181 to 200 sets driven by electric gears with magnetic gears and super-high-speed peripheral speed + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output Various energy storage cycle merging engines and merging methods for merging wings (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ1〜30で噴射駆動する磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)1〜20組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). Magnets that are driven synchronously with water (3E) Mach 1 to 30 in the same synchronous rotation in the same axis (4D) between the horizontal axes (16A) and in the same vertical rotation direction in the same direction. Utilization of bearing load 0 approach + (4C) (4D) Horizontal full-blade hydrogravity turbine (8B) 1-20 sets driven by super-high-speed circumferential speed with magnetic gears + Driven electric product drive + Outer compression blade (8q) Outer compression Various energy storage cycle coalescence engines and coalescence methods for merging of blade (8r) inner output wing (8s) outer output wing (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ1〜30で噴射駆動する磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)21〜40組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). Magnets that are driven synchronously with water (3E) Mach 1 to 30 in the same synchronous rotation in the same axis (4D) between the horizontal axes (16A) and in the same vertical rotation direction in the same direction. Utilization of bearing load 0 approach + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 21-40 sets with super high speed circumferential speed with magnetic gears + Driven electric product drive + Outer compression blade (8q) Outer compression Various energy storage cycle coalescence engines and coalescence methods for merging of blade (8r) inner output wing (8s) outer output wing (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ1〜30で噴射駆動する磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)41〜60組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). Magnets that are driven synchronously with water (3E) Mach 1 to 30 in the same synchronous rotation in the same axis (4D) between the horizontal axes (16A) and in the same vertical rotation direction in the same direction. Utilization of bearing load 0 approach + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 41-60 sets driven by magnetic gears and super high speed circumferential speed + Inner compressor blade (8q) Outer compression Various energy storage cycle coalescence engines and coalescence methods for merging of blade (8r) inner output wing (8s) outer output wing (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ1〜30で噴射駆動する磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)61〜80組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). Magnets that are driven synchronously with water (3E) Mach 1 to 30 in the same synchronous rotation in the same axis (4D) between the horizontal axes (16A) and in the same vertical rotation direction in the same direction. Utilization of bearing load 0 approach + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 61-80 sets driven by magnetic gears and super high speed circumferential speed drive + inner compression blade (8q) outer compression Various energy storage cycle coalescence engines and coalescence methods for merging of blade (8r) inner output wing (8s) outer output wing (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ1〜30で噴射駆動する磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)81〜100組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). Magnets that are driven synchronously with water (3E) Mach 1 to 30 in the same synchronous rotation in the same axis (4D) between the horizontal axes (16A) and in the same vertical rotation direction in the same direction. Utilization of bearing load 0 approach + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 81-100 sets driven by magnetic gears and super high speed circumferential speed drive + electric compressor drive + inner compression blade (8q) outer compression Various energy storage cycle coalescence engines and coalescence methods for merging of blade (8r) inner output wing (8s) outer output wing (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ1〜30で噴射駆動する磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)101〜120発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). Magnets that are driven synchronously with water (3E) Mach 1 to 30 in the same synchronous rotation in the same axis (4D) between the horizontal axes (16A) and in the same vertical rotation direction in the same direction. Utilization of bearing load 0 approach + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 101-120 generator electric product drive + inner compression blade (8q) outer compression blade with super high speed circumferential speed with magnetic gear (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combined with various energy storage cycle combined engines and methods. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ1〜30で噴射駆動する磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)121〜140組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). Magnets that are driven synchronously with water (3E) Mach 1 to 30 in the same synchronous rotation in the same axis (4D) between the horizontal axes (16A) and in the same vertical rotation direction in the same direction. Utilization of bearing load 0 approach + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 121-140 sets driven by magnetic gears and super-high speed circumferential speed Driven electric product drive + inner compression blade (8q) outer compression Various energy storage cycle coalescence engines and coalescence methods for merging of blade (8r) inner output wing (8s) outer output wing (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ1〜30で噴射駆動する磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)141〜160組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). Magnets that are driven synchronously with water (3E) Mach 1 to 30 in the same synchronous rotation in the same axis (4D) between the horizontal axes (16A) and in the same vertical rotation direction in the same direction. Utilization of bearing load 0 approach + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 141-160 set with super high speed circumferential speed with magnetic gears Driven electric product drive + inner compression blade (8q) outer compression Various energy conservation cycle coalescence engines and coalescence methods for merging of blade (8r) inner output wing (8s) outer output wing (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ1〜30で噴射駆動する磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)161〜180組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). Magnets that are driven synchronously with water (3E) Mach 1 to 30 in the same synchronous rotation in the same axis (4D) between the horizontal axes (16A) and in the same vertical rotation direction in the same direction. Utilization of bearing load 0 approach + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 161-180 set with super high speed circumferential speed with magnetic gears + Inner compressor blade (8q) Outer compression Various energy storage cycle coalescence engines and coalescence methods for merging of blade (8r) inner output wing (8s) outer output wing (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ1〜30で噴射駆動する磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)181〜200組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). Magnets that are driven synchronously with water (3E) Mach 1 to 30 in the same synchronous rotation in the same axis (4D) between the horizontal axes (16A) and in the same vertical rotation direction in the same direction. Utilization of bearing load 0 approach + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 181 to 200 sets driven by magnetic gears and super high speed circumferential speed drive + inner compression blade (8q) outer compression Various energy storage cycle coalescence engines and coalescence methods for merging of blade (8r) inner output wing (8s) outer output wing (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ20狙いで噴射駆動する磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)1〜20組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). Use of magnetic force to drive counter-synchronous rotation, in-line co-rotating gear (4D) between horizontal shafts (16A), rotate in the same direction in the same vertical direction, and drive to jet water aiming at water (3E) Mach 20 Bearing load 0 approach + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 1-20 sets driven by electric gears with magnetic gears and super high speed circumferential speed + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combined with various energy storage cycle combined engines and methods. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ20狙いで噴射駆動する磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)21〜40組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). Use of magnetic force to drive counter-synchronous rotation, in-line co-rotating gear (4D) between horizontal shafts (16A), rotate in the same direction in the same vertical direction, and drive to jet water aiming at water (3E) Mach 20 Bearing load 0 approach + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 21 to 40 sets driven by magnetic gears and super high speed circumferential speed drive + Electric product drive + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combined with various energy storage cycle combined engines and methods. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ20狙いで噴射駆動する磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)41〜60組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). Use of magnetic force to drive counter-synchronous rotation, in-line co-rotating gear (4D) between horizontal shafts (16A), rotate in the same direction in the same vertical direction, and drive to jet water aiming at water (3E) Mach 20 Bearing load 0 approach + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 41-60 sets driven by magnetic gears and super high speed circumferential speed + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combined with various energy storage cycle combined engines and methods. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ20狙いで噴射駆動する磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)61〜80組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). Use of magnetic force to drive counter-synchronous rotation, in-line co-rotating gear (4D) between horizontal shafts (16A), rotate in the same direction in the same vertical direction, and drive to jet water aiming at water (3E) Mach 20 Bearing load 0 approach + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 61-80 sets driven by magnetic gears and super high speed circumferential speed Driven electric product drive + inner compressor blade (8q) outer compressor blade (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combined with various energy storage cycle combined engines and methods. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ20狙いで噴射駆動する磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)81〜100組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). Use of magnetic force to drive counter-synchronous rotation, in-line co-rotating gear (4D) between horizontal shafts (16A), rotate in the same direction in the same vertical direction, and drive to jet water aiming at water (3E) Mach 20 Bearing load 0 approach + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 81-100 sets driven by electric gears with super high speed circumferential speed with magnetic gears + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combined with various energy storage cycle combined engines and methods. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ20狙いで噴射駆動する磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)101〜120発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). Use of magnetic force to drive counter-synchronous rotation, in-line co-rotating gear (4D) between horizontal shafts (16A), rotate in the same direction in the same vertical direction, and drive to jet water aiming at water (3E) Mach 20 Bearing load 0 approach + (4C) (4D) Horizontal full-blade hydrogravity turbine (8B) 101-120 generator electric product drive with super high speed circumferential speed with magnetic gear + inner compressor blade (8q) outer compressor blade ( 8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combined drive with various energy storage cycle combined engines and methods. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ20狙いで噴射駆動する磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)121〜140組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). Use of magnetic force to drive counter-synchronous rotation, in-line co-rotating gear (4D) between horizontal shafts (16A), rotate in the same direction in the same vertical direction, and drive to jet water aiming at water (3E) Mach 20 Bearing load 0 approach + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 121-140 set driven by magnetic gears and super high speed circumferential speed drive + electric product drive + inner compressor blade (8q) outer compressor blade (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combined with various energy storage cycle combined engines and methods. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ20狙いで噴射駆動する磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)141〜160組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). Use of magnetic force to drive counter-synchronous rotation, in-line co-rotating gear (4D) between horizontal shafts (16A), rotate in the same direction in the same vertical direction, and drive to jet water aiming at water (3E) Mach 20 Bearing load 0 approach + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 141-160 set with super high speed circumferential speed with magnetic gears + Driven electric product drive + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combined with various energy storage cycle combined engines and methods. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ20狙いで噴射駆動する磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)161〜180組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). Use of magnetic force to drive counter-synchronous rotation, in-line co-rotating gear (4D) between horizontal shafts (16A), rotate in the same direction in the same vertical direction, and drive to jet water aiming at water (3E) Mach 20 Bearing load 0 approach + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 161-180 sets driven by magnetic gears and super high speed circumferential speed drive + inner compressor blade (8q) outer compressor blade (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combined with various energy storage cycle combined engines and methods. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ20狙いで噴射駆動する磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)181〜200組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). Use of magnetic force to drive counter-synchronous rotation, in-line co-rotating gear (4D) between horizontal shafts (16A), rotate in the same direction in the same vertical direction, and drive to jet water aiming at water (3E) Mach 20 Bearing load 0 approach + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 181 to 200 sets driven by magnetic gears and super high speed circumferential speed Drive of electric power product + inner compressor blade (8q) outer compressor blade (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combined with various energy storage cycle combined engines and methods. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、内径全面切削可能実験最大径の磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)1〜20組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). The counter-synchronized rotation is provided with a series rotation gear (4D) between the horizontal axes (16A), and each set is rotated in the same direction in the same direction in the vertical direction. Approach + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 1-20 sets driven by electric gear with super high speed circumferential speed with magnetic gears + Inner compressor blade (8q) Outer compressor blade (8r) Various energy storage cycle coalescence engines and coalescence methods for coalescence of inner output wing (8s) outer output wing (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、内径全面切削可能実験最大径の磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)21〜40組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). The counter-synchronized rotation is provided with a series rotation gear (4D) between the horizontal axes (16A), and each set is rotated in the same direction in the same direction in the vertical direction. Approach + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 21-40 sets driven by electrical gears with magnetic gears and super high speed circumferential speed + Inner compressor blade (8q) Outer compressor blade (8r) Various energy storage cycle coalescence engines and coalescence methods for coalescence of inner output wing (8s) outer output wing (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、内径全面切削可能実験最大径の磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)41〜60組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). The counter-synchronized rotation is provided with a series rotation gear (4D) between the horizontal axes (16A), and each set is rotated in the same direction in the same direction in the vertical direction. Approach + (4C) (4D) Horizontal type full-blade water gravity turbine (8B) 41-60 sets driven by electrical gears with magnetic gears and super high speed circumferential speed + Inner compressor blade (8q) Outer compressor blade (8r) Various energy storage cycle coalescence engines and coalescence methods for coalescence of inner output wing (8s) outer output wing (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、内径全面切削可能実験最大径の磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)61〜80組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). The counter-synchronized rotation is provided with a series rotation gear (4D) between the horizontal axes (16A), and each set is rotated in the same direction in the same direction in the vertical direction. Approach + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 61-80 sets driven by electric gear with magnetic gears and super high speed circumferential speed + Inner compressor blade (8q) Outer compressor blade (8r) Various energy storage cycle coalescence engines and coalescence methods for coalescence of inner output wing (8s) outer output wing (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、内径全面切削可能実験最大径の磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)81〜100組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). The counter-synchronized rotation is provided with a series rotation gear (4D) between the horizontal axes (16A), and each set is rotated in the same direction in the same direction in the vertical direction. Approach + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 81-100 sets driven by electric gear with super high speed circumferential speed with magnetic gears + inner compressor blade (8q) outer compressor blade (8r) Various energy storage cycle coalescence engines and coalescence methods for coalescence of inner output wing (8s) outer output wing (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、内径全面切削可能実験最大径の磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)101〜120発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). The counter-synchronized rotation is provided with a series rotation gear (4D) between the horizontal axes (16A), and each set is rotated in the same direction in the same direction in the vertical direction. Approach + (4C) (4D) Horizontal full-blade hydrogravity turbine (8B) 101-120 generator electric product drive with super high speed circumferential speed with magnetic gears + inner compressor blade (8q) outer compressor blade (8r) inside Various energy conservation cycle coalescence engines and coalescence methods for coalescence of output vane (8s) outer output vane (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、内径全面切削可能実験最大径の磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)121〜140組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). The counter-synchronized rotation is provided with a series rotation gear (4D) between the horizontal axes (16A), and each set is rotated in the same direction in the same direction in the vertical direction. Approach + (4C) (4D) Horizontal full-blade hydrogravity turbine (8B) 121-140 sets driven by electric gears with magnetic gears and super-high-speed circumferential speed + Inner compressor blade (8q) Outer compressor blade (8r) Various energy storage cycle coalescence engines and coalescence methods for coalescence of inner output wing (8s) outer output wing (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、内径全面切削可能実験最大径の磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)141〜160組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). The counter-synchronized rotation is provided with a series rotation gear (4D) between the horizontal axes (16A), and each set is rotated in the same direction in the same direction in the vertical direction. Approach + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 141-160 set driven by super-high-speed circumferential speed with magnetic gears + Power generator drive + Inner compressor blade (8q) Outer compressor blade (8r) Various energy storage cycle coalescence engines and coalescence methods for coalescence of inner output wing (8s) outer output wing (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、内径全面切削可能実験最大径の磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)161〜180組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). The counter-synchronized rotation is provided with a series rotation gear (4D) between the horizontal axes (16A), and each set is rotated in the same direction in the same direction in the vertical direction. Approach + (4C) (4D) Horizontal full-blade hydrogravity turbine (8B) 161-180 sets driven by electric gears with magnetic gears and super high speed circumferential speed drive + inner compressor blade (8q) outer compressor blade (8r) Various energy storage cycle coalescence engines and coalescence methods for coalescence of inner output wing (8s) outer output wing (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、内径全面切削可能実験最大径の磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)181〜200組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). The counter-synchronized rotation is provided with a series rotation gear (4D) between the horizontal axes (16A), and each set is rotated in the same direction in the same direction in the vertical direction. Approach + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 181 to 200 sets driven by electric gears with magnetic gears and super high speed peripheral drive + inner compressor blade (8q) outer compressor blade (8r) Various energy storage cycle coalescence engines and coalescence methods for coalescence of inner output wing (8s) outer output wing (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ1〜30で噴射駆動する内径全面切削可能実験最大径の磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)1〜20組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). An inner diameter that is driven by water (3E) Mach 1 to 30 in the same synchronous rotation in the opposite direction and provided in series with the same rotation gear (4D) between the horizontal axes (16A). Full surface cutting possible Experiment using the largest diameter magnetic bearing load 0 approach + (4C) (4D) Horizontal full-blade water gravity turbine (8B) 1-20 sets driven by electric gears with super high speed circumferential speed with magnetic gears + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Organization and coalescence method. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ1〜30で噴射駆動する内径全面切削可能実験最大径の磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)21〜40組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). An inner diameter that is driven by water (3E) Mach 1 to 30 in the same synchronous rotation in the opposite direction and provided in series with the same rotation gear (4D) between the horizontal axes (16A). Full-scale cutting possible experiment using the maximum diameter magnetic bearing load 0 approach + (4C) (4D) Horizontal type full-blade water gravity turbine (8B) 21-40 sets driven by super-high-speed circumferential speed with magnetic gears + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Organization and coalescence method. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ1〜30で噴射駆動する内径全面切削可能実験最大径の磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)41〜60組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). An inner diameter that is driven by water (3E) Mach 1 to 30 in the same synchronous rotation in the opposite direction and provided in series with the same rotation gear (4D) between the horizontal axes (16A). Full surface cutting possible experiment using the maximum diameter magnetic bearing load 0 approach + (4C) (4D) Horizontal type full-blade water gravity turbine (8B) 41-60 sets driven by ultra-high speed circumferential speed with magnetic gears + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Organization and coalescence method. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ1〜30で噴射駆動する内径全面切削可能実験最大径の磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)61〜80組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). An inner diameter that is driven by water (3E) Mach 1 to 30 in the same synchronous rotation in the opposite direction and provided in series with the same rotation gear (4D) between the horizontal axes (16A). Full-surface cutting possible experiment using the maximum diameter magnetic bearing load 0 approach + (4C) (4D) Horizontal type full-blade water gravity turbine (8B) 61-80 sets driven by electric gears with super high speed circumferential speed with magnetic gears + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Organization and coalescence method. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ1〜30で噴射駆動する内径全面切削可能実験最大径の磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)81〜100組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). An inner diameter that is driven by water (3E) Mach 1 to 30 in the same synchronous rotation in the opposite direction and provided in series with the same rotation gear (4D) between the horizontal axes (16A). Full-scale cutting possible experiment using the largest diameter magnetic bearing load 0 approach + (4C) (4D) Horizontal all blade hydrogravity turbine (8B) 81-100 sets driven by electric gears with super high speed circumferential speed with magnetic gears + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Organization and coalescence method. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ1〜30で噴射駆動する内径全面切削可能実験最大径の磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)101〜120発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). An inner diameter that is driven by water (3E) Mach 1 to 30 in the same synchronous rotation in the opposite direction and provided in series with the same rotation gear (4D) between the horizontal axes (16A). Full-scale cutting possible experiment using the maximum diameter magnetic bearing load 0 approach + (4C) (4D) horizontal full-blade hydrogravity turbine (8B) 101-120 power generation electric product drive + inside Compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combined drive of various energy conservation cycle combined engine And coalescing method. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ1〜30で噴射駆動する内径全面切削可能実験最大径の磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)121〜140組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). An inner diameter that is driven by water (3E) Mach 1 to 30 in the same synchronous rotation in the opposite direction and provided in series with the same rotation gear (4D) between the horizontal axes (16A). Full surface cutting possible experiment using the maximum diameter magnetic bearing load 0 approach + (4C) (4D) horizontal all-blade hydrogravity turbine (8B) 121-140 sets driven by super-high-speed circumferential speed with magnetic gears + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Organization and coalescence method. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ1〜30で噴射駆動する内径全面切削可能実験最大径の磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)141〜160組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). An inner diameter that is driven by water (3E) Mach 1 to 30 in the same synchronous rotation in the opposite direction and provided in series with the same rotation gear (4D) between the horizontal axes (16A). Full-scale cutting possible experiment using the largest diameter magnetic bearing load 0 approach + (4C) (4D) Horizontal all blade hydrogravity turbine (8B) 141 to 160 sets driven by magnetic gears and super high speed circumferential drive Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Organization and coalescence method. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ1〜30で噴射駆動する内径全面切削可能実験最大径の磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)161〜180組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). An inner diameter that is driven by water (3E) Mach 1 to 30 in the same synchronous rotation in the opposite direction and provided in series with the same rotation gear (4D) between the horizontal axes (16A). Full-surface cutting possible experiment using maximum diameter magnetic bearing load 0 approach + (4C) (4D) Horizontal all blade hydrogravity turbine (8B) 161-180 sets driven by electric gears with super high speed circumferential speed + 4 Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Organization and coalescence method. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ1〜30で噴射駆動する内径全面切削可能実験最大径の磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)181〜200組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). An inner diameter that is driven by water (3E) Mach 1 to 30 in the same synchronous rotation in the opposite direction and provided in series with the same rotation gear (4D) between the horizontal axes (16A). Full surface cutting possible experiment using the maximum diameter magnetic bearing load 0 approach + (4C) (4D) Horizontal all blade hydrogravity turbine (8B) 181-200 sets driven by electric gears with ultra high speed circumferential speed with magnetic gears + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Organization and coalescence method. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ20狙いで噴射駆動する内径全面切削可能実験最大径の磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)1〜20組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). In the same synchronous rotation, a series of co-rotating gears (4D) are provided between the horizontal axes (16A), and each pair of vertical co-rotating in the same direction is rotated at the same speed, and the entire inner diameter is driven for injection by water (3E) Mach 20 The maximum diameter of magnetically available bearings that can be cut is approached to zero + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) with super high speed circumferential speed with magnetic gears (8B) 1 to 20 sets of power generation electric product drive + inside Compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combined drive of various energy conservation cycle combined engine And coalescing method. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ20狙いで噴射駆動する内径全面切削可能実験最大径の磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)21〜40組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). In the same synchronous rotation, a series of co-rotating gears (4D) are provided between the horizontal axes (16A), and each pair of vertical co-rotating in the same direction is rotated at the same speed, and the entire inner diameter is driven for injection by water (3E) Mach 20 The maximum diameter of magnetically available bearings that can be cut is approaching zero + (4C) (4D) horizontal all-blade hydrogravity turbine (8B) 21-40 sets driven by magnetic gears and ultra-high-speed circumferential drive Compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combined drive of various energy conservation cycle combined engine And coalescing method. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ20狙いで噴射駆動する内径全面切削可能実験最大径の磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)41〜60組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). In the same synchronous rotation, a series of co-rotating gears (4D) are provided between the horizontal axes (16A), and each pair of vertical co-rotating in the same direction is rotated at the same speed, and the entire inner diameter is driven for injection by water (3E) Mach 20 Horizontally-moving blade hydrogravity turbine (8B) 41-60 sets driven by a magnetic gear with super-high-speed circumferential speed with a magnetic gear bearing load 0 approach + (4C) (4D) magnetic gear of the maximum diameter that can be cut + Driven inside electric power product drive + inside Compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combined drive of various energy conservation cycle combined engine And coalescing method. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ20狙いで噴射駆動する内径全面切削可能実験最大径の磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)61〜80組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). In the same synchronous rotation, a series of co-rotating gears (4D) are provided between the horizontal axes (16A), and each pair of vertical co-rotating in the same direction is rotated at the same speed, and the entire inner diameter is driven for injection by water (3E) Mach 20 The maximum diameter of magnetically available bearing load that can be cut is approaching 0 + (4C) (4D) Horizontal all-blade hydrogravity turbine (8B) 61-80 sets driven by magnetic gears and ultra-high speed peripheral drive + inside Compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combined drive of various energy conservation cycle combined engine And coalescing method. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ20狙いで噴射駆動する内径全面切削可能実験最大径の磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)81〜100組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). In the same synchronous rotation, a series of co-rotating gears (4D) are provided between the horizontal axes (16A), and each pair of vertical co-rotating in the same direction is rotated at the same speed, and the entire inner diameter is driven for injection by water (3E) Mach 20 Horizontally-moving blade hydrogravity turbine (8B) 81-100 sets driven by electric gears of the maximum diameter using magnetic gears of the maximum diameter that can be cut + (4C) (4D) magnetic gears and ultra-high speed circumferential drive + inner drive Compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combined drive of various energy conservation cycle combined engine And coalescing method. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ20狙いで噴射駆動する内径全面切削可能実験最大径の磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)101〜120発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). In the same synchronous rotation, a series of co-rotating gears (4D) are provided between the horizontal axes (16A), and each pair of vertical co-rotating in the same direction is rotated at the same speed, and the entire inner diameter is driven for injection by water (3E) Mach 20 Horizontally-moving blade hydrogravity turbine (8B) 101-120 power generation electric product drive + inward compression with super high speed circumferential speed with magnetic gear bearing load 0 approach + (4C) (4D) magnetic gear Various energy conservation cycle coalescing engines that combine driving blades (8q) outer compression blades (8r) inner output blades (8s) outer output blades (8t) + transverse shaft bearing load 0 approaching counter rotating production compressed air (28a) drive, Merge method. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ20狙いで噴射駆動する内径全面切削可能実験最大径の磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)121〜140組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). In the same synchronous rotation, a series of co-rotating gears (4D) are provided between the horizontal axes (16A), and each pair of vertical co-rotating in the same direction is rotated at the same speed, and the entire inner diameter is driven for injection by water (3E) Mach 20 Horizontally-moving blade hydrogravity turbine (8B) 121-140 sets driven by a magnetic gear bearing with a maximum diameter of approx. Compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combined drive of various energy conservation cycle combined engine And coalescing method. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ20狙いで噴射駆動する内径全面切削可能実験最大径の磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)141〜160組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). In the same synchronous rotation, a series of co-rotating gears (4D) are provided between the horizontal axes (16A), and each pair of vertical co-rotating in the same direction is rotated at the same speed, and the entire inner diameter is driven for injection by water (3E) Mach 20 The maximum diameter of magnetically available bearing load that can be cut is approaching 0 + (4C) (4D) Horizontal all-blade hydrogravity turbine (8B) 141-160 sets driven by magnetic gears and ultra-high speed circumferential drive Compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combined drive of various energy conservation cycle combined engine And coalescing method. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ20狙いで噴射駆動する内径全面切削可能実験最大径の磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)161〜180組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). In the same synchronous rotation, a series of co-rotating gears (4D) are provided between the horizontal axes (16A), and each pair of vertical co-rotating in the same direction is rotated at the same speed, and the entire inner diameter is driven for injection by water (3E) Mach 20 Horizontally-moving blade hydrogravity turbine (8B) 161-180 sets driven by a magnetic gear with an ultra-high-speed circumferential speed with magnetic gear bearings approaching 0 with the maximum magnetically available bearing load of the maximum diameter that can be cut. Compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combined drive of various energy conservation cycle combined engine And coalescing method. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定1組とし、水平軸(16A)に対向同期歯車(4C)具備して1組の対向同期回転にして、水平軸(16A)の間に直列同回転歯車(4D)具備し、1組夫々の垂直同方向同速度回転にして、水(3E)マッハ20狙いで噴射駆動する内径全面切削可能実験最大径の磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)181〜200組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体に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 set of horizontal shafts (16A) fixed on both sides of the turbine blade (8b) cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) are provided on the horizontal shaft (16A). In the same synchronous rotation, a series of co-rotating gears (4D) are provided between the horizontal axes (16A), and each pair of vertical co-rotating in the same direction is rotated at the same speed, and the entire inner diameter is driven for injection by water (3E) Mach 20 Horizontally-moving blade hydrogravity turbine (8B) 181 to 200 sets driven by a magnetic gear with an ultra-high-speed circumferential speed with magnetic gear bearing load 0 approaching maximum (4C) (4D) magnetic gear + drive inside power generation Compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combined drive of various energy conservation cycle combined engine And coalescing method. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定2個1組とし、対向直列全動翼弾み車タービンとした磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)1〜20組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体にする各種エネルギ保存サイクル合体機関及び合体方法。   Turbine blades (8b) Cylindrical turbine blade group (8A) The horizontal shaft (16A) is fixed to each side by a horizontal shaft plate (16) on one side, and a pair of two is used, and a magnetically utilized bearing load of 0 is approached. (4C) (4D) Horizontal full-blade hydrogravity turbine (8B) 1-20 sets driven by electric gears with magnetic gears and super-high speed circumferential drive + inner compressor blade (8q) outer compressor blade (8r) inner output Various energy storage cycle coalescence engines and coalescence methods for merging of blade (8s) outer output wing (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定2個1組とし、対向直列全動翼弾み車タービンとした磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)21〜40組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体にする各種エネルギ保存サイクル合体機関及び合体方法。   Turbine blades (8b) Cylindrical turbine blade group (8A) The horizontal shaft (16A) is fixed to both sides by a horizontal shaft plate (16), and one set of two is used as an opposed series full blade impeller turbine. (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 21 to 40 sets driven by electric gears with magnetic gears and super high speed peripheral drive + inner compressor blade (8q) outer compressor blade (8r) inner output Various energy storage cycle coalescence engines and coalescence methods for merging of blade (8s) outer output wing (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定2個1組とし、対向直列全動翼弾み車タービンとした磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)41〜60組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体にする各種エネルギ保存サイクル合体機関及び合体方法。   Turbine blades (8b) Cylindrical turbine blade group (8A) The horizontal shaft (16A) is fixed to each side by a horizontal shaft plate (16) on one side, and a pair of two is used, and a magnetically utilized bearing load of 0 is approached. (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 41-60 sets driven by electric gears with magnetic gears and super high speed circumferential speed + Inner compressor blade (8q) Outer compressor blade (8r) Inner output Various energy storage cycle coalescence engines and coalescence methods for merging of blade (8s) outer output wing (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定2個1組とし、対向直列全動翼弾み車タービンとした磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)61〜80組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体にする各種エネルギ保存サイクル合体機関及び合体方法。   Turbine blades (8b) Cylindrical turbine blade group (8A) The horizontal shaft (16A) is fixed to each side by a horizontal shaft plate (16) on one side, and a pair of two is used, and a magnetically utilized bearing load of 0 is approached. (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 61-80 sets driven by electric gears with magnetic gears and super-high speed peripheral drive + inner compressor blade (8q) outer compressor blade (8r) inner output Various energy storage cycle coalescence engines and coalescence methods for merging of blade (8s) outer output wing (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定2個1組とし、対向直列全動翼弾み車タービンとした磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)81〜100組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体にする各種エネルギ保存サイクル合体機関及び合体方法。   Turbine blades (8b) Cylindrical turbine blade group (8A) The horizontal shaft (16A) is fixed to each side by a horizontal shaft plate (16) on one side, and a pair of two is used, and a magnetically utilized bearing load of 0 is approached. (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 81-100 sets driven by electric gears with magnetic gears and super high speed circumferential speed + Inner compressor blade (8q) Outer compressor blade (8r) Inner output Various energy storage cycle coalescence engines and coalescence methods for merging of blade (8s) outer output wing (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定2個1組とし、対向直列全動翼弾み車タービンとした磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)100〜120組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体にする各種エネルギ保存サイクル合体機関及び合体方法。   Turbine blades (8b) Cylindrical turbine blade group (8A) The horizontal shaft (16A) is fixed to each side by a horizontal shaft plate (16) on one side, and a pair of two is used, and a magnetically utilized bearing load of 0 is approached. (4C) (4D) Horizontal full-blade hydrogravity turbine (8B) 100-120 sets driven by magnetic gears and super-high speed circumferential drive Power generation electric product drive + inner compressor blade (8q) outer compressor blade (8r) inner output Various energy storage cycle coalescence engines and coalescence methods for merging of blade (8s) outer output wing (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定2個1組とし、対向直列全動翼弾み車タービンとした磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)121〜140組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体にする各種エネルギ保存サイクル合体機関及び合体方法。   Turbine blades (8b) Cylindrical turbine blade group (8A) The horizontal shaft (16A) is fixed to each side by a horizontal shaft plate (16) on one side, and a pair of two is used, and a magnetically utilized bearing load of 0 is approached. (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 121-140 sets driven by magnetic gears and super-high speed circumferential drive (power generation electric product drive + inner compression blade (8q) outer compression blade (8r) inner output Various energy storage cycle coalescence engines and coalescence methods for merging of blade (8s) outer output wing (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定2個1組とし、対向直列全動翼弾み車タービンとした磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)141〜160組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体にする各種エネルギ保存サイクル合体機関及び合体方法。   Turbine blades (8b) Cylindrical turbine blade group (8A) The horizontal shaft (16A) is fixed to each side by a horizontal shaft plate (16) on one side, and a pair of two is used, and a magnetically utilized bearing load of 0 is approached. (4C) (4D) Horizontal full-blade hydrogravity turbine (8B) 141-160 set driven by magnetic gears and super-high speed circumferential drive Power generation electric product drive + inner compressor blade (8q) outer compressor blade (8r) inner output Various energy storage cycle coalescence engines and coalescence methods for merging of blade (8s) outer output wing (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定2個1組とし、対向直列全動翼弾み車タービンとした磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)161〜180組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体にする各種エネルギ保存サイクル合体機関及び合体方法。   Turbine blades (8b) Cylindrical turbine blade group (8A) The horizontal shaft (16A) is fixed to both sides by a horizontal shaft plate (16), and one set of two is used as an opposed series full blade impeller turbine. (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 161-180 sets driven by magnetic gears and super-high speed circumferential drive Power generation electric product drive + inner compressor blade (8q) outer compressor blade (8r) inner output Various energy storage cycle coalescence engines and coalescence methods for merging of blade (8s) outer output wing (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定2個1組とし、対向直列全動翼弾み車タービンとした磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)181〜200組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体にする各種エネルギ保存サイクル合体機関及び合体方法。   Turbine blades (8b) Cylindrical turbine blade group (8A) The horizontal shaft (16A) is fixed to each side by a horizontal shaft plate (16) on one side, and a pair of two is used, and a magnetically utilized bearing load of 0 is approached. (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 181 to 200 sets driven by magnetic gears and super-high-speed circumferential speed + drive of power generation electric product + inner compressor blade (8q) outer compressor blade (8r) inner output Various energy storage cycle coalescence engines and coalescence methods for merging of blade (8s) outer output wing (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定2個1組とし、直列全動翼弾み車タービンとした磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)1〜20組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体にする各種エネルギ保存サイクル合体機関及び合体方法。   Turbine blades (8b) Cylindrical turbine blade group (8A) The horizontal shaft (16A) is fixed to the both sides by a horizontal shaft plate (16) as one set, and a magnetic bearing load of 0 approach + ( 4C) (4D) Horizontal full-blade water gravity turbine (8B) 1-20 sets driven by electric gears with magnetic gears and super-high-speed circumferential speed + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8 s) Various energy storage cycle coalescence engines and coalescence methods for coalescence of outer output blade (8t) + horizontal shaft bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定2個1組とし、直列全動翼弾み車タービンとした磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)21〜40組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体にする各種エネルギ保存サイクル合体機関及び合体方法。   Turbine blades (8b) Cylindrical turbine blade group (8A) The horizontal shaft (16A) is fixed to the both sides by a horizontal shaft plate (16) as one set, and a magnetic bearing load of 0 approach + ( 4C) (4D) Horizontal full-blade hydrogravity turbine (8B) 21 to 40 sets driven by electric gear with super high speed circumferential speed with magnetic gears + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8 s) Various energy storage cycle coalescence engines and coalescence methods for coalescence of outer output blade (8t) + horizontal shaft bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定2個1組とし、直列全動翼弾み車タービンとした磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)41〜60組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体にする各種エネルギ保存サイクル合体機関及び合体方法。   Turbine blades (8b) Cylindrical turbine blade group (8A) The horizontal shaft (16A) is fixed to the both sides by a horizontal shaft plate (16) as one set, and a magnetic bearing load of 0 approach + ( 4C) (4D) Horizontal full-blade hydrogravity turbine (8B) 41-60 sets driven by electric gear with super high speed circumferential speed with magnetic gears + inner compressor blade (8q) outer compressor blade (8r) inner output blade (8 s) Various energy storage cycle coalescence engines and coalescence methods for coalescence of outer output blade (8t) + horizontal shaft bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定2個1組とし、直列全動翼弾み車タービンとした磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)61〜80組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体にする各種エネルギ保存サイクル合体機関及び合体方法。   Turbine blades (8b) Cylindrical turbine blade group (8A) The horizontal shaft (16A) is fixed to the both sides by a horizontal shaft plate (16) as one set, and a magnetic bearing load of 0 approach + ( 4C) (4D) Horizontal full-blade hydrogravity turbine (8B) 61-80 sets driven by electric gears with magnetic gears and super high speed circumferential speed drive + inner compressor blade (8q) outer compressor blade (8r) inner output blade (8 s) Various energy storage cycle coalescence engines and coalescence methods for coalescence of outer output blade (8t) + horizontal shaft bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定2個1組とし、直列全動翼弾み車タービンとした磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)81〜100組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体にする各種エネルギ保存サイクル合体機関及び合体方法。   Turbine blades (8b) Cylindrical turbine blade group (8A) The horizontal shaft (16A) is fixed to the both sides by a horizontal shaft plate (16) as one set, and a magnetic bearing load of 0 approach + ( 4C) (4D) Horizontal full-blade hydrogravity turbine (8B) 81 to 100 sets driven by electric gears with magnetic gears and super-high-speed circumferential speed + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8 s) Various energy storage cycle coalescence engines and coalescence methods for coalescence of outer output blade (8t) + horizontal shaft bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定2個1組とし、直列全動翼弾み車タービンとした磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)100〜120組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体にする各種エネルギ保存サイクル合体機関及び合体方法。   Turbine blades (8b) Cylindrical turbine blade group (8A) The horizontal shaft (16A) is fixed to the both sides by a horizontal shaft plate (16) as one set, and a magnetic bearing load of 0 approach + ( 4C) (4D) Horizontal full-blade hydrogravity turbine (8B) 100-120 sets driven by electric gears with magnetic gears and super-high-speed circumferential speed + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8 s) Various energy storage cycle coalescence engines and coalescence methods for coalescence of outer output blade (8t) + horizontal shaft bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定2個1組とし、直列全動翼弾み車タービンとした磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)121〜140組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体にする各種エネルギ保存サイクル合体機関及び合体方法。   Turbine blades (8b) Cylindrical turbine blade group (8A) The horizontal shaft (16A) is fixed to the both sides by a horizontal shaft plate (16) as one set, and a magnetic bearing load of 0 approach + ( 4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 121-140 sets driven by electric gears with magnetic gears and super high speed circumferential speed drive + inner compressor blade (8q) outer compressor blade (8r) inner output blade (8 s) Various energy storage cycle coalescence engines and coalescence methods for coalescence of outer output blade (8t) + horizontal shaft bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定2個1組とし、直列全動翼弾み車タービンとした磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)141〜160組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体にする各種エネルギ保存サイクル合体機関及び合体方法。   Turbine blades (8b) Cylindrical turbine blade group (8A) The horizontal shaft (16A) is fixed to the both sides by a horizontal shaft plate (16) as one set, and a magnetic bearing load of 0 approach + ( 4C) (4D) Horizontal full-blade hydrogravity turbine (8B) 141-160 sets driven by magnetic gears and super-high speed circumferential speed power generation electric product drive + inner compression blade (8q) outer compression blade (8r) inner output blade (8 s) Various energy storage cycle coalescence engines and coalescence methods for coalescence of outer output blade (8t) + horizontal shaft bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定2個1組とし、直列全動翼弾み車タービンとした磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)161〜180組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体にする各種エネルギ保存サイクル合体機関及び合体方法。   Turbine blades (8b) Cylindrical turbine blade group (8A) The horizontal shaft (16A) is fixed to the both sides by a horizontal shaft plate (16) as one set, and a magnetic bearing load of 0 approach + ( 4C) (4D) Horizontal full-blade hydrogravity turbine (8B) 161-180 sets driven by electric gears with magnetic gears and super-high-speed circumferential speed + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8 s) Various energy storage cycle coalescence engines and coalescence methods for coalescence of outer output blade (8t) + horizontal shaft bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定2個1組とし、直列全動翼弾み車タービンとした磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)181〜200組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体にする各種エネルギ保存サイクル合体機関及び合体方法。   Turbine blades (8b) Cylindrical turbine blade group (8A) The horizontal shaft (16A) is fixed to the both sides by a horizontal shaft plate (16) as one set, and a magnetic bearing load of 0 approach + ( 4C) (4D) Horizontal full-blade hydrogravity turbine (8B) 181 to 200 sets driven by magnetic gears and super-high-speed circumferential speed Drive power generation product + inner compressor blade (8q) outer compressor blade (8r) inner output blade (8 s) Various energy storage cycle coalescence engines and coalescence methods for coalescence of outer output blade (8t) + horizontal shaft bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定2個1組とし、食込直列全動翼弾み車タービンとした磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)1〜20組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体にする各種エネルギ保存サイクル合体機関及び合体方法。   Turbine blade (8b) Cylindrical turbine blade group (8A) The horizontal shaft (16A) is fixed to the both sides by a horizontal shaft plate (16), and one set of two blades is used as a bite series full blade impeller turbine. + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 1-20 sets driven by electric gears with super high speed circumferential speed with magnetic gears + Inner compressor blade (8q) Outer compressor blade (8r) inside Various energy conservation cycle coalescence engines and coalescence methods for coalescence of output vane (8s) outer output vane (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定2個1組とし、食込直列全動翼弾み車タービンとした磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)21〜40組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体にする各種エネルギ保存サイクル合体機関及び合体方法。   Turbine blade (8b) Cylindrical turbine blade group (8A) The horizontal shaft (16A) is fixed to the both sides by a horizontal shaft plate (16), and one set of two blades is used as a bite series full blade impeller turbine. + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 21-40 sets driven by electric gear with super high speed circumferential speed with magnetic gears + Inner compressor blade (8q) Outer compressor blade (8r) inside Various energy conservation cycle coalescence engines and coalescence methods for coalescence of output vane (8s) outer output vane (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定2個1組とし、食込直列全動翼弾み車タービンとした磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)41〜60組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体にする各種エネルギ保存サイクル合体機関及び合体方法。   Turbine blade (8b) Cylindrical turbine blade group (8A) The horizontal shaft (16A) is fixed to the both sides by a horizontal shaft plate (16), and one set of two blades is used as a bite series full blade impeller turbine. + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 41-60 sets driven by electric gear with super high speed circumferential speed with magnetic gears + Inner compressor blade (8q) Outer compressor blade (8r) inside Various energy conservation cycle coalescence engines and coalescence methods for coalescence of output vane (8s) outer output vane (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定2個1組とし、食込直列全動翼弾み車タービンとした磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)61〜80組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体にする各種エネルギ保存サイクル合体機関及び合体方法。   Turbine blade (8b) Cylindrical turbine blade group (8A) The horizontal shaft (16A) is fixed to the both sides by a horizontal shaft plate (16), and one set of two blades is used as a bite series full blade impeller turbine. + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 61-80 sets driven by electric gears with magnetic gears and super high speed circumferential speed + Inner compressor blade (8q) Outer compressor blade (8r) inside Various energy conservation cycle coalescence engines and coalescence methods for coalescence of output vane (8s) outer output vane (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定2個1組とし、食込直列全動翼弾み車タービンとした磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)81〜100組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体にする各種エネルギ保存サイクル合体機関及び合体方法。   Turbine blades (8b) Cylindrical turbine blade group (8A) The horizontal shaft (16A) is fixed to each side by a horizontal shaft plate (16) on one side of the turbine blade (8A). + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 81-100 sets driven by electric gear with super high speed circumferential speed with magnetic gears + Inner compressor blade (8q) Outer compressor blade (8r) inside Various energy conservation cycle coalescence engines and coalescence methods for coalescence of output vane (8s) outer output vane (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定2個1組とし、食込直列全動翼弾み車タービンとした磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)100〜120組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体にする各種エネルギ保存サイクル合体機関及び合体方法。   Turbine blade (8b) Cylindrical turbine blade group (8A) The horizontal shaft (16A) is fixed to the both sides by a horizontal shaft plate (16), and one set of two blades is used as a bite series full blade impeller turbine. + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 100-120 sets driven by electric gears with magnetic gears and super high speed circumferential speed + Inner compressor blade (8q) Outer compressor blade (8r) inside Various energy conservation cycle coalescence engines and coalescence methods for coalescence of output vane (8s) outer output vane (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定2個1組とし、食込直列全動翼弾み車タービンとした磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)121〜140組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体にする各種エネルギ保存サイクル合体機関及び合体方法。   Turbine blade (8b) Cylindrical turbine blade group (8A) The horizontal shaft (16A) is fixed to the both sides by a horizontal shaft plate (16), and one set of two blades is used as a bite series full blade impeller turbine. + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 121-140 sets driven by electric gears with super high speed circumferential speed with magnetic gears + Inner compressor blade (8q) Outer compressor blade (8r) inside Various energy conservation cycle coalescence engines and coalescence methods for coalescence of output vane (8s) outer output vane (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定2個1組とし、食込直列全動翼弾み車タービンとした磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)141〜160組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体にする各種エネルギ保存サイクル合体機関及び合体方法。   Turbine blade (8b) Cylindrical turbine blade group (8A) The horizontal shaft (16A) is fixed to the both sides by a horizontal shaft plate (16), and one set of two blades is used as a bite series full blade impeller turbine. + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 141-160 sets driven by electric gears with magnetic gears and super high speed circumferential speed + Inner compressor blade (8q) Outer compressor blade (8r) inside Various energy conservation cycle coalescence engines and coalescence methods for coalescence of output vane (8s) outer output vane (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定2個1組とし、食込直列全動翼弾み車タービンとした磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)161〜180組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体にする各種エネルギ保存サイクル合体機関及び合体方法。   Turbine blade (8b) Cylindrical turbine blade group (8A) The horizontal shaft (16A) is fixed to the both sides by a horizontal shaft plate (16), and one set of two blades is used as a bite series full blade impeller turbine. + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 161-180 sets driven by electric gears with magnetic gears and super-high-speed circumferential speed + Inner compressor blade (8q) Outer compressor blade (8r) inside Various energy conservation cycle coalescence engines and coalescence methods for coalescence of output vane (8s) outer output vane (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. タービン翼(8b)円筒タービン翼群(8A)両側に水平軸(16A)を水平軸板(16)で固定2個1組とし、食込直列全動翼弾み車タービンとした磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)181〜200組発電電気製造物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動の合体にする各種エネルギ保存サイクル合体機関及び合体方法。   Turbine blade (8b) Cylindrical turbine blade group (8A) The horizontal shaft (16A) is fixed to the both sides by a horizontal shaft plate (16), and one set of two blades is used as a bite series full blade impeller turbine. + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) 181 to 200 sets driven by a magnetic gear and super-high-speed circumferential speed + Inner compressor blade (8q) Outer compressor blade (8r) inside Various energy conservation cycle coalescence engines and coalescence methods for coalescence of output vane (8s) outer output vane (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a) drive. 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+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)極端に安価発電電気駆動の、簡単圧縮機(3s)〜簡単多段圧縮(3i)で1〜複数回圧縮し、圧縮毎に高圧高温水加熱管(5H)で熱回収液体酸素製造機(88p)熱製造して、、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)供給物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動合体に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 full blade having a solar heater (21) provided with buoyancy on the water surface and the solar heated air having a magnetic bearing load of 0 approach + (4C) (4D) magnetic gears and a super high speed circumferential speed Water gravity turbine (8B) Turbine blade (8b) Extremely inexpensive power generation electric drive, simple compressor (3s) to simple multi-stage compression (3i), compressed one or more times, each time high pressure high temperature water heating pipe (5H ) Heat recovery liquid oxygen production machine (88p) heat production, electricity + liquid air cold heat + hot water to superheated steam temperature supply equipment (3D) feed drive + inner compression blade (8q) outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Drive coalescence and various 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、太陽光加熱空気を磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)極端に安価発電電気駆動の、簡単圧縮機(3s)〜簡単多段圧縮(3i)で1〜複数回圧縮し、圧縮毎に高圧高温水加熱管(5H)で熱回収液体酸素製造機(88p)熱製造して、、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)供給物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動合体に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. 0 approach + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with ultra high speed circumferential speed with magnetic gears Extremely inexpensive power generation electric drive, simple compressor (3s)-simple Compressed one or more times with multi-stage compression (3i), heat-recovered liquid oxygen production machine (88p) with high-pressure high-temperature water heating pipe (5H) for each compression, electricity + liquid air cold + high-temperature water to superheat Steam temperature heat supply equipment (3D) feed drive + inner compressor blade (8q) outer compressor blade (8r) inner output blade (8s) outer output blade (8t) + horizontal bearing load 0 approaching counter-rotating manufactured compressed air (28a) ) Various energy storage cycle coalescence engine and coalescence method for driving coalescence 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+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)極端に安価発電電気駆動の、簡単圧縮機(3s)〜簡単多段圧縮(3i)で1〜複数回圧縮し、圧縮毎に高圧高温水加熱管(5H)で熱回収液体酸素製造機(88p)熱製造して、、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)供給物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動合体に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), and a device for controlling the rotation of sunlight at a right angle in the vertical direction, and using a magnetic gear bearing load approaching zero + (4C) (4D) magnetic gears Compressed horizontal full-blade water gravity turbine (8B) Turbine blade (8b) Extremely inexpensive power generation electric drive, simple compressor (3s) to simple multistage compression (3i), compressed one to several times, high pressure and high temperature for each compression Heat recovery liquid oxygen production machine (88p) heat production with water heating pipe (5H), electricity + liquid air cold heat + hot water to superheated steam temperature heat supply equipment (3D) feed drive + inner compression blade (8q) outside Compression blade (8r) Inner output blade (8s) Outer output blade ( t) + horizontal axis bearing load 0 close counterrotating producing compressed air (28a) various energy conservation cycle combined engine and coalescence process for the driving coalesce. 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+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)極端に安価発電電気駆動の、簡単圧縮機(3s)〜簡単多段圧縮(3i)で1〜複数回圧縮し、圧縮毎に高圧高温水加熱管(5H)で熱回収液体酸素製造機(88p)熱製造して、、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)供給物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動合体に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 the rotation of 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. Horizontal full-blade hydrogravity turbine (8B) turbine blade (8b) extremely inexpensive, with the highest air (28a) temperature and the use of magnetic bearing load 0 approach + (4C) (4D) super high speed circumferential speed with magnetic gear Compressed one or more times with a simple compressor (3s) to simple multi-stage compression (3i), which is driven by power generation. Electricity + liquid air cold + high temperature -Superheated steam temperature supply facility (3D) feed drive + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + horizontal axis bearing load 0 approaching counter-rotating manufactured compressed air (28a) Various energy storage cycle coalescence engines and coalescence methods for driving coalescence. 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+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)極端に安価発電電気駆動の、簡単圧縮機(3s)〜簡単多段圧縮(3i)で1〜複数回圧縮し、圧縮毎に高圧高温水加熱管(5H)で熱回収液体酸素製造機(88p)熱製造して、、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)供給物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動合体に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 the rotation of 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 air (28a) temperature is maximized, the external air (28a) is also heated, and each air passage (28A) is used as a high-temperature selective suction. The horizontal full-blade hydrogravity turbine (8B) and the turbine blade (8b) were compressed one or more times with a simple compressor (3s) to simple multistage compression (3i) of extremely inexpensive power generation and electric drive. With high temperature water heating pipe (5H) Recovered liquid oxygen production machine (88p) heat production, electricity + liquid air cold heat + hot water to superheated steam temperature heat supply equipment (3D) feed drive + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) Outer output blade (8t) + horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Various energy storage cycle coalescing engine and coalescence method for driving coalescence. 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+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)極端に安価発電電気駆動の、簡単圧縮機(3s)〜簡単多段圧縮(3i)で1〜複数回圧縮し、圧縮毎に高圧高温水加熱管(5H)で熱回収液体酸素製造機(88p)熱製造して、、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)供給物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動合体にする各種エネルギ保存サイクル合体機関及び合体方法。   Horizontal type full motion with solar heater (21) provided with circular railway on flat ground, and solar heated air with magnetic bearing load approaching 0 + (4C) (4D) magnetic gears with super high speed circumferential speed Blade water gravity turbine (8B) Turbine blade (8b) Extremely inexpensive power generation electric drive, simple compressor (3s) to simple multistage compression (3i), compressed one to several times, high pressure high temperature water heating tube ( 5H) heat recovery liquid oxygen production machine (88p) heat production, electricity + liquid air cooling + hot water to superheated steam temperature supply equipment (3D) feed drive + inner compression blade (8q) outer compression blade (8r) ) Inner output wing (8s) Outer output wing (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combined engine and method for combining various energy storage cycles. 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+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)極端に安価発電電気駆動の、簡単圧縮機(3s)〜簡単多段圧縮(3i)で1〜複数回圧縮し、圧縮毎に高圧高温水加熱管(5H)で熱回収液体酸素製造機(88p)熱製造して、、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)供給物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動合体に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. Load approach 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with ultra-high speed circumferential speed with magnetic gears Simple multi-stage compression (3i) is compressed one or more times, and at each compression, a heat recovery liquid oxygen production machine (88p) is heated with a high-pressure high-temperature water heating pipe (5H), and electricity + liquid air cold heat + high-temperature water Superheated steam temperature supply equipment (3D) feed drive + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + horizontal axis bearing load 0 approaching counter-rotating manufactured compressed air ( 28a) Various energy storage cycle coalescence engines and coalescence to drive coalescence Law. 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+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)極端に安価発電電気駆動の、簡単圧縮機(3s)〜簡単多段圧縮(3i)で1〜複数回圧縮し、圧縮毎に高圧高温水加熱管(5H)で熱回収液体酸素製造機(88p)熱製造して、、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)供給物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動合体に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. The horizontal full-blade hydrogravity turbine (8B) and the turbine blade (8b) were compressed one or more times with a simple compressor (3s) to simple multistage compression (3i) of extremely inexpensive power generation and electric drive. Heat recovery liquid oxygen production machine (88p) heat production with high temperature water heating pipe (5H), electricity + liquid air cold heat + high temperature water to superheated steam temperature supply equipment (3D) feed drive + inner compressor blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output (8t) + horizontal axis bearing load 0 close counterrotating producing compressed air (28a) various energy conservation cycle combined engine and coalescence process for the driving coalesce. 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+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)極端に安価発電電気駆動の、簡単圧縮機(3s)〜簡単多段圧縮(3i)で1〜複数回圧縮し、圧縮毎に高圧高温水加熱管(5H)で熱回収液体酸素製造機(88p)熱製造して、、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)供給物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動合体に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). Horizontal full blade hydrogravity turbine (8B) turbine blade (8b) Compressed one or more times with a simple compressor (3 s) to simple multistage compression (3i), which is driven by low-cost electric power generation, and heat recovery liquid oxygen production machine (88p) heat with a high-pressure high-temperature water heating pipe (5H) for each compression Manufacture, electricity + liquid air cooling + High temperature water to superheated steam temperature supply equipment (3D) feed drive + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approach double reversal Various energy storage cycle coalescence engines and coalescence methods for producing compressed air (28a) drive coalescence. 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+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)極端に安価発電電気駆動の、簡単圧縮機(3s)〜簡単多段圧縮(3i)で1〜複数回圧縮し、圧縮毎に高圧高温水加熱管(5H)で熱回収液体酸素製造機(88p)熱製造して、、電気+液体空気冷熱+高温水〜過熱蒸気温熱供給設備(3D)供給物駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)駆動合体に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). Irradiation internal air (28a) temperature is maximized, external air (28a) is also heated, each air passage (28A) as high-temperature selective suction, magnetic utilization bearing load 0 approach + (4C) (4D) magnetic gears, super high speed circle Horizontal type full-scale blade hydrogravity turbine (8B) turbine blade (8b) with peripheral speed Extremely inexpensive power generation electric drive, simple compressor (3s) to simple multistage compression (3i), compressed one or more times, each compression High pressure high temperature water heating pipe ( H) heat recovery liquid oxygen production machine (88p) heat production, electricity + liquid air cold heat + hot water to superheated steam temperature supply equipment (3D) feed drive + inner compressor blade (8q) outer compressor blade (8r) ) Inner output wing (8s) Outer output wing (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combined engine and method for combining various energy storage cycles. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)より液体酸素(5K)受給駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Liquid oxygen (5K) receiving drive from cold heat + high temperature water to superheated steam heat supply equipment (3D) + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + horizontal shaft bearing Various energy storage cycle coalescing engine and coalescence method for driving zero-load approaching counter-rotating manufactured compressed air (28a). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)より液体酸素(5K)過熱蒸気(50)受給駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Liquid oxygen (5K) superheated steam (50) receiving drive from cold heat + high temperature water to superheated steam temperature supply facility (3D) + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) ) + Axial bearing load 0 approaching counter-rotating manufactured compressed air (28a) Various energy storage cycle merging engines and merging methods driven. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)より液体酸素(5K)過熱蒸気(50)を理論燃焼室(4Q)複数に受給駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cool oxygen + high temperature water to superheated steam temperature supply facility (3D), liquid oxygen (5K) superheated steam (50) is supplied to multiple theoretical combustion chambers (4Q) + inner compression blade (8q) outer compression blade (8r) inner output Blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) driven various energy storage cycle coalescing engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)より液体酸素(5K)過熱蒸気(50)を理論燃焼室(4Q)複数に受給合体駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cooling + hot water to superheated steam hot water supply equipment (3D) Liquid oxygen (5K) superheated steam (50) is supplied to multiple theoretical combustion chambers (4Q) combined drive + inner compressor blade (8q) outer compressor blade (8r) inside Various energy storage cycle coalescence engine and coalescence method for driving output blade (8s) outer output blade (8t) + horizontal bearing load 0 approaching counter-rotating production compressed air (28a). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)より液体酸素(5K)過熱蒸気(50)を理論燃焼室(4Q)複数に受給合体ロケット燃焼駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold oxygen + high temperature water to superheated steam temperature supply facility (3D) liquid oxygen (5K) superheated steam (50) is supplied to multiple theoretical combustion chambers (4Q) combined rocket combustion drive + inner compressor blade (8q) outer compressor blade (8r) ) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) driven various energy storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)より液体酸素(5K)過熱蒸気(50)を理論燃焼室(4Q)複数に受給合体ロケット燃焼追加駆動+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold oxygen + high temperature water to superheated steam temperature supply facility (3D) Liquid oxygen (5K) superheated steam (50) is supplied to multiple theoretical combustion chambers (4Q) combined rocket combustion additional drive + inner compressor blade (8q) outer compressor blade ( 8r) Inner output vane (8s) Outer output vane (8t) + horizontal shaft bearing load 0 approaching counter-rotating production compressed air (28a) driven various energy storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)より液体酸素(5K)過熱蒸気(50)を理論燃焼室(4Q)複数に受給合体ロケット燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold oxygen + hot water to superheated steam supply system (3D) Liquid oxygen (5K) superheated steam (50) is received in multiple theoretical combustion chambers (4Q) Combined rocket combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output wing (8s) Outer output wing (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Various energy storage cycle merging engines and merging methods. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)より液体酸素(5K)過熱蒸気(50)を理論燃焼室(4Q)複数に受給ロケット燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold oxygen + high temperature water to superheated steam temperature supply facility (3D) liquid oxygen (5K) superheated steam (50) is received in multiple theoretical combustion chambers (4Q) rocket combustion + inner compressor blade (8q) outer compressor blade (8r) inside Output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Various energy storage cycle coalescing engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)より液体酸素(5K)過熱蒸気(50)を理論燃焼室(4Q)複数に受給ロケット燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold oxygen + high temperature water to superheated steam temperature supply facility (3D) liquid oxygen (5K) superheated steam (50) is received in multiple theoretical combustion chambers (4Q) rocket combustion + inner compressor blade (8q) outer compressor blade (8r) inside Output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Various energy storage cycle coalescing engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)より液体酸素(5K)過熱蒸気(50)を理論燃焼室(4Q)複数に受給ロケット燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold oxygen + high temperature water to superheated steam temperature supply facility (3D) liquid oxygen (5K) superheated steam (50) is received in multiple theoretical combustion chambers (4Q) rocket combustion + inner compressor blade (8q) outer compressor blade (8r) inside Output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Various energy storage cycle coalescing engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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2種類理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Two types of theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner side receiving cold liquid oxygen (5K) from cold water + hot water to superheated steam temperature heat supply equipment (3D) and making the compression volume 21/60000 of air compression Compressor blades (8q) Outer compressor blades (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) As a combustion, drive a simple gas engine (88q) Various energy storage cycle coalescence engine and coalescence method for driving an automobile. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receive cold liquid oxygen (5K) + electricity from cold water + hot water to superheated steam hot water supply facility (3D), theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output vane (8s) Outer output vane (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion engine and various energy storage cycle coalescence engine and coalescence driven by simple gas engine (88q) Method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold liquid + high temperature water to superheated steam temperature supply facility (3D) receives cheap liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output vane (8s) Outer output vane (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion of various energy conservation cycles driven by a simple gas engine (88q) driving an automobile Organization and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)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)回転簡単ガス機関自動車(7I)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Theoretical combustion chamber (4Q) that receives low-priced liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply equipment (3D) and sets the compression volume to 21/60000 of air compression (4Q) Ultra high pressure fuel combustion + inner compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production compressed air (28a) Combustion as simple gas engine (88q) drive generator (1 ) Various energy storage cycle coalescence engines and coalescence methods that store electricity in the drive accumulator (1A) and drive the accumulator drive wheels (4J) rotating simple gas engine vehicle (7I). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)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)回転簡単ガス機関自動車(7I)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost power generation electricity production Receive cold liquid oxygen (5K) + electricity from cold water + hot water to superheated steam hot water supply facility (3D), theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output wing (8s) Outer output wing (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion is stored in simple gas engine (88q) drive generator (1) drive storage battery (1A) Battery storage wheel (4J) rotating simple gas engine automobile (7I) various energy storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)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)回転簡単ガス機関自動車(7I)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold liquid + high temperature water to superheated steam temperature supply facility (3D) receives cheap liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output vane (8s) Outer output vane (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion as simple gas engine (88q) Drive generator (1) Drive battery (1A) Various energy storage cycle coalescing engine and coalescence method for storing the battery and driving the battery drive wheel (4J) rotating simple gas engine automobile (7I). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)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簡単ガス機関自動車(7I)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Theoretical combustion chamber (4Q) that receives low-priced liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply equipment (3D) and sets the compression volume to 21/60000 of air compression (4Q) Ultra high pressure fuel combustion + inner compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production compressed air (28a) Combustion as simple gas engine (88q) drive generator (1 ) Various energy storage cycle coalescence engine and coalescence method for driving a simple gas engine vehicle (7I) capable of rotating the storage battery drive wheel (4J) and normal wheel by accumulating in the drive storage battery (1A). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)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簡単ガス機関自動車(7I)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receive cold liquid oxygen (5K) + electricity from cold water + hot water to superheated steam hot water supply facility (3D), theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output wing (8s) Outer output wing (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion is stored in simple gas engine (88q) drive generator (1) drive storage battery (1A) Various energy storage cycle coalescence engine and coalescence method for driving a simple gas engine vehicle (7I) 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+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)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簡単ガス機関自動車(7I)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold liquid + high temperature water to superheated steam temperature supply facility (3D) receives cheap liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output vane (8s) Outer output vane (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion as simple gas engine (88q) Drive generator (1) Drive accumulator (1A) Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine vehicle (7I) that can be stored in a battery and driven by a storage battery drive wheel (4J) and a normal wheel. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)駆動して簡単ガス機関自動車(7I)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Theoretical combustion chamber (4Q) that receives low-priced liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply equipment (3D) and sets the compression volume to 21/60000 of air compression (4Q) Ultra high pressure fuel combustion + inner compression blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion as simple gas engine (88q) driven as simple gas Various energy storage cycle coalescence engine and coalescence method for driving a locomotive (7I). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Theoretical combustion chamber (4Q) that receives low-priced liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply equipment (3D) and sets the compression volume to 21/60000 of air compression (4Q) Ultra high pressure fuel combustion + inner compression blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion as simple gas engine (88q) driven screw ( 7C) Various energy storage cycle coalescence engines and coalescence methods for driving a rotating ship. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receive cold liquid oxygen (5K) + electricity from cold water + hot water to superheated steam hot water supply facility (3D), theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output wing (8s) Outer output wing (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion as simple gas engine (88q) drive and screw (7C) rotating ship to save various energy Cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold liquid + high temperature water to superheated steam temperature supply facility (3D) receives cheap liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output wing (8s) Outer output wing (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) As a combustion, a simple gas engine (88q) is driven and a screw (7C) is rotated to drive Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Theoretical combustion chamber (4Q) that receives low-priced liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply equipment (3D) and sets the compression volume to 21/60000 of air compression (4Q) Ultra high pressure fuel combustion + inner compression blade (8q) Outer compression blades (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) As a combustion, simple gas engine (88q) 1 to multiple drives Various energy storage cycle coalescing engine and coalescence method for driving a screw (7C) multiple rotation ship. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receive cold liquid oxygen (5K) + electricity from cold water + hot water to superheated steam hot water supply facility (3D), theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output wing (8s) Outer output wing (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion with simple gas engine (88q) 1 to multiple drive and screw (7C) multiple rotation ship drive Various energy storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold liquid + high temperature water to superheated steam temperature supply facility (3D) receives cheap liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) As a combustion, simple gas engine (88q) 1 to multiple drives and screws (7C) multiple Various energy storage cycle coalescence engines and coalescence methods for driving a rotating ship. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動してスクリュー(7C)複数回転簡単ガス機関船舶(7J)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Theoretical combustion chamber (4Q) that receives low-priced liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply equipment (3D) and sets the compression volume to 21/60000 of air compression (4Q) Ultra high pressure fuel combustion + inner compression blade (8q) Outer compression blades (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) As a combustion, simple gas engine (88q) 1 to multiple drives Various energy storage cycle coalescing engine and coalescence method for driving a screw (7C) multi-turn simple gas engine ship (7J). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動してスクリュー(7C)複数回転簡単ガス機関船舶(7J)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receive cold liquid oxygen (5K) + electricity from cold water + hot water to superheated steam hot water supply facility (3D), theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output vane (8s) Outer output vane (8t) + horizontal axis bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion as simple gas engine (88q) 1 to multiple drive screw (7C) multiple rotation simple gas Various energy storage cycle coalescence engines and coalescence methods for driving engine ships (7J). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動してスクリュー(7C)複数回転簡単ガス機関船舶(7J)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold liquid + high temperature water to superheated steam temperature supply facility (3D) receives cheap liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) As a combustion, simple gas engine (88q) 1 to multiple drives and screws (7C) multiple Various energy storage cycle coalescence engine and coalescence method for driving a simple rotating gas engine ship (7J). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)駆動して簡単ガス機関船舶(7J)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Theoretical combustion chamber (4Q) that receives low-priced liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply equipment (3D) and sets the compression volume to 21/60000 of air compression (4Q) Ultra high pressure fuel combustion + inner compression blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion as simple gas engine (88q) driven as simple gas Various energy storage cycle coalescence engines and coalescence methods for driving engine ships (7J). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)駆動してスクリュー(7C)回転簡単空気噴射機関(88r)等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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Theoretical combustion chamber (4Q) that receives low-priced liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply equipment (3D) and sets the compression volume to 21/60000 of air compression (4Q) Ultra high pressure fuel combustion + inner compression blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion as simple gas engine (88q) driven screw ( 7C) Various energy storage cycle coalescing engines and coalescence methods for driving an injection propulsion ship such as a simple rotating air injection engine (88r). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)駆動してスクリュー(7C)回転簡単空気噴射機関(88r)等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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receive cold liquid oxygen (5K) + electricity from cold water + hot water to superheated steam hot water supply facility (3D), theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output wing (8s) Outer output wing (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) As a combustion, a simple gas engine (88q) is driven and a screw (7C) rotation simple air injection engine (88r ) Various energy conservation cycle coalescence engines and coalescence methods for driving equal injection propulsion vessels. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)駆動してスクリュー(7C)回転簡単空気噴射機関(88r)等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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold liquid + high temperature water to superheated steam temperature supply facility (3D) receives cheap liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) As a combustion, a simple gas engine (88q) is driven and a screw (7C) rotation simple air injection Various energy storage cycle coalescence engine and coalescence method for driving an injection propulsion ship such as an engine (88r). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動してスクリュー(7C)複数回転簡単空気噴射機関(88r)等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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Theoretical combustion chamber (4Q) that receives low-priced liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply equipment (3D) and sets the compression volume to 21/60000 of air compression (4Q) Ultra high pressure fuel combustion + inner compression blade (8q) Outer compression blades (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) As a combustion, simple gas engine (88q) 1 to multiple drives Various energy storage cycle coalescence engine and coalescence method for driving a propulsion vessel such as a screw (7C) multiple rotation simple air injection engine (88r). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動してスクリュー(7C)複数回転簡単空気噴射機関(88r)等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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receive cold liquid oxygen (5K) + electricity from cold water + hot water to superheated steam hot water supply facility (3D), theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output vane (8s) Outer output vane (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion as simple gas engine (88q) 1 to multiple drive screw (7C) multiple rotation simple air Various energy storage cycle coalescence engine and coalescence method for driving an injection propulsion ship such as an injection engine (88r). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動してスクリュー(7C)複数回転簡単空気噴射機関(88r)等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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold liquid + high temperature water to superheated steam temperature supply facility (3D) receives cheap liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) As a combustion, simple gas engine (88q) 1 to multiple drives and screws (7C) multiple Various energy storage cycle coalescence engine and coalescence method for driving an injection propulsion ship such as a rotary simple air injection engine (88r). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動してスクリュー(7C)複数回転簡単空気噴射機関(88r)等噴射推進スクリュー噴射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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost power generation electricity production Theoretical combustion chamber (4Q) that receives low-priced liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply equipment (3D) and sets the compression volume to 21/60000 of air compression (4Q) Ultra high pressure fuel combustion + inner compression blade (8q) Outer compression blades (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) As a combustion, simple gas engine (88q) 1 to multiple drives Screw (7C) multi-turn simple air injection engine (88r), etc. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動してスクリュー(7C)複数回転簡単空気噴射機関(88r)等噴射推進スクリュー噴射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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost power generation electricity production Receive cold liquid oxygen (5K) + electricity from cold water + hot water to superheated steam hot water supply facility (3D), theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output vane (8s) Outer output vane (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion as simple gas engine (88q) 1 to multiple drive screw (7C) multiple rotation simple air Various energy storage cycle coalescence engine and coalescence method for driving an injection propulsion screw injection vessel such as an injection engine (88r). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動してスクリュー(7C)複数回転簡単空気噴射機関(88r)等噴射推進スクリュー噴射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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold liquid + high temperature water to superheated steam temperature supply facility (3D) receives cheap liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) As a combustion, simple gas engine (88q) 1 to multiple drives and screws (7C) multiple Various energy storage cycle coalescence engine and coalescence method for driving a propulsion screw injection ship such as a rotary simple air injection engine (88r). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)駆動して簡単空気噴射機関(88r)等噴射推進スクリュー噴射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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Theoretical combustion chamber (4Q) that receives low-priced liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply equipment (3D) and sets the compression volume to 21/60000 of air compression (4Q) Ultra high pressure fuel combustion + inner compression blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion as simple gas engine (88q) driven as simple air Various energy storage cycle coalescence engine and coalescence method for driving an injection propulsion screw injection vessel such as an injection engine (88r). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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にするの理論燃焼室(4Q)複数超高圧燃料燃焼噴射推進+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単空気噴射機関(88r)等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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Theoretical combustion chamber (4Q) with multiple ultra-high pressure fuel combustion propulsion to receive cheap liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply equipment (3D) and make the compression volume 21/60000 of air compression + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion simple air injection engine (88r) ) Various energy conservation cycle coalescence engine and coalescence method for driving an equal injection propulsion ship. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)複数超高圧燃料燃焼噴射推進+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単空気噴射機関(88r)等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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) + electricity is received from cold heat + hot water to superheated steam heat supply equipment (3D), theoretical combustion chamber (4Q) multiple ultra high pressure fuel combustion injection propulsion + inner compression blade (8q) outer compression blade (8r) Inner output wing (8s) Outer output wing (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion simple air injection engine (88r), etc. Cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)複数超高圧燃料燃焼噴射推進+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単空気噴射機関(88r)等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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receiving cold liquid + hot water to superheated steam hot water supply equipment (3D), cheap liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) multiple ultra high pressure fuel combustion injection propulsion + inner compression blades (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion, etc. Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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にするの理論燃焼室(4Q)空気吸引流路具備含む複数超高圧燃料燃焼噴射推進+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単空気噴射機関(88r)等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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production A plurality of theoretical combustion chambers (4Q) including an air suction passage for receiving cheap liquid oxygen (5K) from cold heat + high temperature water to superheated steam temperature heat supply equipment (3D) to make the compression volume 21/60000 of air compression Super high-pressure fuel combustion injection propulsion + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + horizontal shaft bearing load 0 approaching counter-rotating production compressed air (28a) combustion Various energy storage cycle coalescence engine and coalescence method for driving an injection propulsion ship such as a simple air injection engine (88r). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、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+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単空気噴射機関(88r)等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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cooling + high temperature water to superheated steam heating and heat supply equipment (3D) receiving low-priced liquid oxygen (5K) + electricity and equipped with a theoretical combustion chamber (4Q) air suction channel multiple ultra high pressure fuel combustion injection propulsion + inner compression blades (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion of simple air injection engine (88r), etc. Various energy storage cycle coalescence engines and coalescence methods for driving a ship. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、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+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単空気噴射機関(88r)等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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) + electricity + high temperature water is received from cold heat + high temperature water to superheated steam heat supply equipment (3D), and a super combustion fuel combustion injection propulsion including a theoretical combustion chamber (4Q) air suction channel + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion simple air injection engine (88r) Various energy storage cycle coalescence engine and coalescence method for driving an equal injection propulsion ship. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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にするの理論燃焼室(4Q)空気吸引流路具備含む複数超高圧燃料燃焼噴射推進+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単空気噴射機関(88r)等噴射推進簡単空気噴射機関船舶(7L)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production A plurality of theoretical combustion chambers (4Q) including an air suction passage for receiving cheap liquid oxygen (5K) from cold heat + high temperature water to superheated steam temperature heat supply equipment (3D) to make the compression volume 21/60000 of air compression Super high-pressure fuel combustion injection propulsion + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + horizontal shaft bearing load 0 approaching counter-rotating production compressed air (28a) combustion Various energy storage cycle coalescing engines and coalescence methods for driving a simple air injection engine (88r), etc., an injection propulsion simple air injection engine ship (7L). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、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+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単空気噴射機関(88r)等噴射推進簡単空気噴射機関船舶(7L)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cooling + high temperature water to superheated steam heating and heat supply equipment (3D) receiving low-priced liquid oxygen (5K) + electricity and equipped with a theoretical combustion chamber (4Q) air suction channel multiple ultra high pressure fuel combustion injection propulsion + inner compression blades (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion of simple air injection engine (88r), etc. Various energy storage cycle coalescence engine and coalescence method for driving a simple air injection engine ship (7L). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、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+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単空気噴射機関(88r)等噴射推進簡単空気噴射機関船舶(7L)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) + electricity + high temperature water is received from cold heat + high temperature water to superheated steam heat supply equipment (3D), and a super combustion fuel combustion injection propulsion including a theoretical combustion chamber (4Q) air suction channel + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion simple air injection engine (88r) Equi-injection propulsion simple air injection engine ship (7L) various energy storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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にする理論燃焼室(4Q)複数+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単空気噴射機関(88r)等噴射推進簡単空気噴射機関船舶(7L)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Theoretical combustion chamber (4Q) + inner compression blades (8q) that receive cold liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply equipment (3D) and make the compression volume 21/60000 of air compression Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion simple air injection engine (88r), etc. Various energy storage cycle coalescence engine and coalescence method for driving an engine ship (7L). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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にする理論燃焼室(4Q)複数超高圧燃料燃焼噴射推進+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単噴射機関(88s)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Theoretical combustion chamber (4Q) that receives cheap liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply equipment (3D) and makes the compression volume 21/60000 of the air compression. Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion simple injection engine (88s) injection Various energy conservation cycle coalescence engines and coalescence methods for propulsion airplanes. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)複数超高圧燃料燃焼噴射推進+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単噴射機関(88s)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) + electricity is received from cold heat + hot water to superheated steam heat supply equipment (3D), theoretical combustion chamber (4Q) multiple ultra high pressure fuel combustion injection propulsion + inner compression blade (8q) outer compression blade (8r) Inner output wing (8s) Outer output wing (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion simple injection engine (88s) Injection propulsion airplane Combined with various energy conservation cycles Organization and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)複数超高圧燃料燃焼噴射推進+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単噴射機関(88s)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receiving cold liquid + hot water to superheated steam hot water supply equipment (3D), cheap liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) multiple ultra high pressure fuel combustion injection propulsion + inner compression blades (8q) Outer compression blades (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion simple injection engine (88s) Various energy to make an injection propulsion airplane Storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単噴射機関(88s)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature + high temperature water to superheated steam temperature heat supply equipment (3D) receiving cheap liquid oxygen (5K) and having a theoretical combustion chamber (4Q) air suction flow path with a compression volume of 21/60000 of air compression High pressure fuel combustion injection propulsion + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + horizontal axis bearing load 0 approaching counter-rotating production compressed air (28a) combustion Various energy storage cycle coalescence engine and coalescence method for making an injection engine (88s) jet propulsion airplane. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、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+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単噴射機関(88s)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cooling + high temperature water to superheated steam heating and heat supply equipment (3D) receiving low-priced liquid oxygen (5K) + electricity and equipped with a theoretical combustion chamber (4Q) air suction channel multiple ultra high pressure fuel combustion injection propulsion + inner compression blades (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion simple injection engine (88s) Various energy storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、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+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単噴射機関(88s)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) + electricity + high temperature water is received from cold heat + high temperature water to superheated steam heat supply equipment (3D), and a super combustion fuel combustion injection propulsion including a theoretical combustion chamber (4Q) air suction channel + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion simple injection engine (88s) injection Various energy conservation cycle coalescence engines and coalescence methods for propulsion airplanes. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単噴射機関(88s)噴射推進簡単噴射機関飛行機(7M)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature + high temperature water to superheated steam temperature heat supply equipment (3D) receiving cheap liquid oxygen (5K) and having a theoretical combustion chamber (4Q) air suction flow path with a compression volume of 21/60000 of air compression High pressure fuel combustion injection propulsion + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + horizontal axis bearing load 0 approaching counter-rotating production compressed air (28a) combustion Injection engine (88s) injection propulsion simple injection engine airplane (7M) various energy storage cycle combination engine and combination method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、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+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単噴射機関(88s)噴射推進簡単噴射機関飛行機(7M)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cooling + high temperature water to superheated steam heating and heat supply equipment (3D) receiving low-priced liquid oxygen (5K) + electricity and equipped with a theoretical combustion chamber (4Q) air suction channel multiple ultra high pressure fuel combustion injection propulsion + inner compression blades (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion simple injection engine (88s) Injection propulsion simple injection Various energy storage cycle coalescing engines and coalescence methods driven by an engine airplane (7M). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、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+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単噴射機関(88s)噴射推進簡単噴射機関飛行機(7M)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) + electricity + high temperature water is received from cold heat + high temperature water to superheated steam heat supply equipment (3D), and a super combustion fuel combustion injection propulsion including a theoretical combustion chamber (4Q) air suction channel + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion simple injection engine (88s) injection Various energy storage cycle coalescence engine and coalescence method for driving propulsion simple injection engine airplane (7M). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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にする理論燃焼室(4Q)複数とした簡単噴射機関(88s)噴射推進簡単噴射機関飛行機(7M)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Simple injection engine (88s) with multiple theoretical combustion chambers (4Q) that receive cheap liquid oxygen (5K) from cold heat + hot water to superheated steam temperature heat supply equipment (3D) and make the compression volume 21/60000 of air compression ) Injection propulsion simple injection engine airplane (7M) various energy storage cycle coalescence engine and coalescence method to drive. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Theoretical combustion chamber (4Q) that receives low-priced liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply equipment (3D) and sets the compression volume to 21/60000 of air compression (4Q) Ultra high pressure fuel combustion + inner compression blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) As a combustion, a simple gas engine (88q) is driven to 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+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receive cold liquid oxygen (5K) + electricity from cold water + hot water to superheated steam hot water supply facility (3D), theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output wing (8s) Outer output wing (8t) + Horizontal axis bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion with simple gas engine (88q) and propeller (7A) rotating airplane to save various energy Cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold liquid + high temperature water to superheated steam temperature supply facility (3D) receives cheap liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output wing (8s) Outer output wing (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) As a combustion, a simple gas engine (88q) is driven and a propeller (7A) is driven by a rotating airplane Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Theoretical combustion chamber (4Q) that receives low-priced liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply equipment (3D) and sets the compression volume to 21/60000 of air compression (4Q) Ultra high pressure fuel combustion + inner compression blade (8q) Outer compression blades (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) As a combustion, simple gas engine (88q) 1 to multiple drives Propeller (7A) Various energy storage cycle coalescence engine and coalescence method for driving a multi-turn airplane. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receive cold liquid oxygen (5K) + electricity from cold water + hot water to superheated steam hot water supply facility (3D), theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output wing (8s) Outer output wing (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) As a combustion, simple gas engine (88q) 1 to multiple drive, propeller (7A) multiple rotation airplane drive Various energy storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold liquid + high temperature water to superheated steam temperature supply facility (3D) receives cheap liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion with simple gas engine (88q) 1 to multiple propellers (7A) Various energy storage cycle coalescence engine and coalescence method for driving a rotating airplane. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動してプロペラ(7A)複数回転簡単ガス機関飛行機(7K)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Theoretical combustion chamber (4Q) that receives low-priced liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply equipment (3D) and sets the compression volume to 21/60000 of air compression (4Q) Ultra high pressure fuel combustion + inner compression blade (8q) Outer compression blades (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) As a combustion, simple gas engine (88q) 1 to multiple drives Various energy storage cycle coalescing engine and coalescence method for driving a propeller (7A) multi-turn simple gas engine airplane (7K). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動してプロペラ(7A)複数回転簡単ガス機関飛行機(7K)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receive cold liquid oxygen (5K) + electricity from cold water + hot water to superheated steam hot water supply facility (3D), theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output wing (8s) Outer output wing (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion as simple gas engine (88q) 1 to multiple drive propeller (7A) multiple rotation simple gas Various energy storage cycle coalescence engine and coalescence method driven by an engine airplane (7K). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動してプロペラ(7A)複数回転簡単ガス機関飛行機(7K)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold liquid + high temperature water to superheated steam temperature supply facility (3D) receives cheap liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion with simple gas engine (88q) 1 to multiple propellers (7A) Various energy storage cycle coalescence engine and coalescence method driven by a rotary simple gas engine airplane (7K). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)駆動してプロペラ(7A)回転簡単ガス機関飛行機(7K)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Theoretical combustion chamber (4Q) that receives low-priced liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply equipment (3D) and sets the compression volume to 21/60000 of air compression (4Q) Ultra high pressure fuel combustion + inner compression blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) As a combustion, a simple gas engine (88q) is driven to propeller ( 7A) Rotating simple gas engine airplane (7K) driving various energy storage cycle merging engine and merging method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(R)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にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade water gravity turbine (R) with super high speed circumferential speed with magnetic gears (R) Extremely inexpensive power generation electric production, electricity + liquid air cold heat + hot water ~ Theoretical combustion chamber (4Q) super high pressure fuel combustion + inner compression blade (8q) outer compression receiving cheap liquid oxygen (5K) from superheated steam temperature supply facility (3D) and making the compression volume 21/60000 of air compression Wing (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion as simple gas engine (88q) Drive rotor (7B) Various energy storage cycle coalescence engines and coalescence methods to be driven. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receive cold liquid oxygen (5K) + electricity from cold water + hot water to superheated steam hot water supply facility (3D), theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output wing (8s) Outer output wing (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion simple gas engine (88q) Drive rotor (7B) Storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold liquid + high temperature water to superheated steam temperature supply facility (3D) receives cheap liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output wing (8s) Outer output wing (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion as simple gas engine (88q) driving rotor (7B) rotating to drive airplane Various energy storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Theoretical combustion chamber (4Q) that receives low-priced liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply equipment (3D) and sets the compression volume to 21/60000 of air compression (4Q) Ultra high pressure fuel combustion + inner compression blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion as simple gas engine (88q) 1 to multiple drive rotation Wings (7B) Various energy storage cycle coalescing engines and coalescence methods for driving a plurality of wings to drive an airplane. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receive cold liquid oxygen (5K) + electricity from cold water + hot water to superheated steam hot water supply facility (3D), theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output wing (8s) Outer output wing (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion as simple gas engine (88q) 1-multiple drive rotor (7B) Various energy storage cycle coalescence engines and coalescence methods to be driven. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold liquid + high temperature water to superheated steam temperature supply facility (3D) receives cheap liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion as simple gas engine (88q) 1 to multiple drive rotor blades (7B) multiple rotations Various energy storage cycle coalescence engine and coalescence method for driving by airplane. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動回転翼(7B)複数回転して回転翼飛行機(7N)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Theoretical combustion chamber (4Q) that receives low-priced liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply equipment (3D) and sets the compression volume to 21/60000 of air compression (4Q) Ultra high pressure fuel combustion + inner compression blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion as simple gas engine (88q) 1 to multiple drive rotation Various energy storage cycle coalescing engine and coalescence method for driving the wing (7B) and rotating the wing airplane (7N). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動回転翼(7B)複数回転して回転翼飛行機(7N)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receive cold liquid oxygen (5K) + electricity from cold water + hot water to superheated steam hot water supply facility (3D), theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion as simple gas engine (88q) 1 to multiple drive rotor (7B) Various energy storage cycle coalescence engine and coalescence method for driving a wing airplane (7N). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動回転翼(7B)複数回転して回転翼飛行機(7N)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold liquid + high temperature water to superheated steam temperature supply facility (3D) receives cheap liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion as simple gas engine (88q) 1 to multiple drive rotor blades (7B) multiple rotations Various energy storage cycle coalescence engines and coalescence methods for driving a rotary wing airplane (7N). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)駆動回転翼(7B)回転して回転翼飛行機(7N)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Theoretical combustion chamber (4Q) that receives low-priced liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply equipment (3D) and sets the compression volume to 21/60000 of air compression (4Q) Ultra high pressure fuel combustion + inner compression blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion as simple gas engine (88q) driven rotor blade (7B ) Various energy conservation cycle coalescing engines and coalescence methods that rotate and drive a rotorcraft (7N). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)駆動プロペラ(7A)回転し簡単噴射機関(88s)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Theoretical combustion chamber (4Q) that receives low-priced liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply equipment (3D) and sets the compression volume to 21/60000 of air compression (4Q) Ultra high pressure fuel combustion + inner compression blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion as simple gas engine (88q) drive propeller (7A) Various energy storage cycle coalescence engine and coalescence method for rotating and driving simple injection engine (88s) jet propulsion airplane. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)駆動プロペラ(7A)回転し簡単噴射機関(88s)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receive cold liquid oxygen (5K) + electricity from cold water + hot water to superheated steam hot water supply facility (3D), theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output wing (8s) Outer output wing (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion as simple gas engine (88q) drive propeller (7A) and simple injection engine (88s) injection Various energy storage cycle coalescence engines and coalescence methods for driving propulsion airplanes. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)駆動プロペラ(7A)回転し簡単噴射機関(88s)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold liquid + high temperature water to superheated steam temperature supply facility (3D) receives cheap liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion as simple gas engine (88q) drive propeller (7A) and simple injection engine ( 88s) 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+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動プロペラ(7A)複数回転し簡単噴射機関(88s)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Theoretical combustion chamber (4Q) that receives low-priced liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply equipment (3D) and sets the compression volume to 21/60000 of air compression (4Q) Ultra high pressure fuel combustion + inner compression blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion as simple gas engine (88q) 1 to multiple drive propeller (7A) Various energy storage cycle coalescing engine and coalescing method for driving multiple injection and simple injection engine (88s) injection propulsion airplane. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動プロペラ(7A)複数回転し簡単噴射機関(88s)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receive cold liquid oxygen (5K) + electricity from cold water + hot water to superheated steam hot water supply facility (3D), theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output wing (8s) Outer output wing (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion as simple gas engine (88q) 1 to multiple drive propeller (7A) Multiple rotation and simple injection engine (88s) Various energy storage cycle coalescence engine and coalescence method for driving an injection propulsion airplane. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動プロペラ(7A)複数回転し簡単噴射機関(88s)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold liquid + high temperature water to superheated steam temperature supply facility (3D) receives cheap liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion as simple gas engine (88q) 1 to multiple drive propeller (7A) multiple rotations Various energy storage cycle coalescing engine and coalescence method for driving simple injection engine (88s) jet propulsion airplane. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動プロペラ(7A)複数回転し簡単噴射機関(88s)噴射推進簡単ガス機関飛行機(7K)等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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Theoretical combustion chamber (4Q) that receives low-priced liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply equipment (3D) and sets the compression volume to 21/60000 of air compression (4Q) Ultra high pressure fuel combustion + inner compression blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion as simple gas engine (88q) 1 to multiple drive propeller (7A) Various energy storage cycle coalescence engines and coalescence methods for driving a plurality of rotations and simple injection engines (88s) injection propulsion simple gas engine airplane (7K) and the like. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動プロペラ(7A)複数回転し簡単噴射機関(88s)噴射推進簡単ガス機関飛行機(7K)等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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receive cold liquid oxygen (5K) + electricity from cold water + hot water to superheated steam hot water supply facility (3D), theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output wing (8s) Outer output wing (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion as simple gas engine (88q) 1 to multiple drive propeller (7A) Multiple rotation and simple injection engine (88s) Various energy storage cycle coalescing engines and coalescence methods for driving an injection propulsion simple gas engine airplane (7K) or the like. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動プロペラ(7A)複数回転し簡単噴射機関(88s)噴射推進簡単ガス機関飛行機(7K)等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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold liquid + high temperature water to superheated steam temperature supply facility (3D) receives cheap liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion as simple gas engine (88q) 1 to multiple drive propeller (7A) multiple rotations A simple injection engine (88s) injection propulsion simple gas engine airplane (7K) and other various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)駆動プロペラ(7A)回転し簡単噴射機関(88s)噴射推進簡単ガス機関飛行機(7K)等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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Theoretical combustion chamber (4Q) that receives low-priced liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply equipment (3D) and sets the compression volume to 21/60000 of air compression (4Q) Ultra high pressure fuel combustion + inner compression blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion as simple gas engine (88q) drive propeller (7A) Various energy storage cycle coalescence engines and coalescence methods that rotate and drive simple injection engine (88s) injection propulsion simple gas engine airplane (7K) and the like. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とし、高圧高温燃焼ガス(5M)を噴射して簡単ガス機関(88q)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Theoretical combustion chamber (4Q) that receives low-priced liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply equipment (3D) and sets the compression volume to 21/60000 of air compression (4Q) Ultra high pressure fuel combustion + inner compression blade (8q) Outer compression blades (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production compressed air (28a) combustion, high pressure high temperature combustion gas (5M) is injected Various energy storage cycle coalescing engine and coalescence method for driving a simple gas engine (88q). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とし、高圧高温燃焼ガス(5M)を噴射して簡単ガス機関(88q)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receive cold liquid oxygen (5K) + electricity from cold water + hot water to superheated steam hot water supply facility (3D), theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output wing (8s) Outer output wing (8t) + horizontal axis bearing load 0 approaching counter-rotating production Compressed air (28a) combustion, high pressure high temperature combustion gas (5M) is injected and simple gas engine (88q) is driven Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とし、高圧高温燃焼ガス(5M)を噴射して簡単ガス機関(88q)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold liquid + high temperature water to superheated steam temperature supply facility (3D) receives cheap liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production compressed air (28a) combustion, high pressure high temperature combustion gas (5M) is injected, and simple gas engine (88q ) Various energy storage cycle coalescence engines and coalescence methods to be driven. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とし、高圧高温燃焼ガス(5M)を噴射して横軸(1h)二重反転する簡単ガス機関(88q)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Theoretical combustion chamber (4Q) that receives low-priced liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply equipment (3D) and sets the compression volume to 21/60000 of air compression (4Q) Ultra high pressure fuel combustion + inner compression blade (8q) Outer compression blades (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production compressed air (28a) combustion, high pressure high temperature combustion gas (5M) is injected The horizontal axis (1h) is a simple gas engine (88q) that is doubly inverted, and various energy storage cycle coalescing engines and coalescence methods. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とし、高圧高温燃焼ガス(5M)を噴射して横軸(1h)二重反転する簡単ガス機関(88q)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receive cold liquid oxygen (5K) + electricity from cold water + hot water to superheated steam hot water supply facility (3D), theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal axis bearing load 0 approaching counter-rotating production Compressed air (28a) combustion, high-pressure high-temperature combustion gas (5M) is injected, and horizontal axis (1h) counter-rotating Various energy storage cycle coalescence engine and coalescence method for driving simple gas engine (88q). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とし、高圧高温燃焼ガス(5M)を噴射して横軸(1h)二重反転する簡単ガス機関(88q)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold liquid + high temperature water to superheated steam temperature supply facility (3D) receives cheap liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output vane (8s) Outer output vane (8t) + horizontal axis bearing load 0 approaching counter-rotating production compressed air (28a) combustion, high pressure high temperature combustion gas (5M) is injected and horizontal axis (1h) Various energy storage cycle coalescence engine and coalescence method driven by a double gas reversing simple gas engine (88q). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とし、高圧高温燃焼ガス(5M)を噴射して横軸(1h)二重反転複数組の簡単ガス機関(88q)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Theoretical combustion chamber (4Q) that receives low-priced liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply equipment (3D) and sets the compression volume to 21/60000 of air compression (4Q) Ultra high pressure fuel combustion + inner compression blade (8q) Outer compression blades (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production compressed air (28a) combustion, high pressure high temperature combustion gas (5M) is injected The horizontal axis (1h) is a combination of a plurality of simple gas engines (88q) with a double reversal, and various energy storage cycle coalescing engines and coalescence methods. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とし、高圧高温燃焼ガス(5M)を噴射して横軸(1h)二重反転複数組の簡単ガス機関(88q)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receive cold liquid oxygen (5K) + electricity from cold water + hot water to superheated steam hot water supply facility (3D), theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal axis bearing load 0 approaching counter-rotating production Compressed air (28a) combustion, high-pressure high-temperature combustion gas (5M) is injected, and horizontal axis (1h) counter-rotating Various energy storage cycle coalescence engines and coalescence methods for driving a plurality of simple gas engines (88q). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とし、高圧高温燃焼ガス(5M)を噴射して横軸(1h)二重反転複数組の簡単ガス機関(88q)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold liquid + high temperature water to superheated steam temperature supply facility (3D) receives cheap liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output vane (8s) Outer output vane (8t) + horizontal axis bearing load 0 approaching counter-rotating production compressed air (28a) combustion, high pressure high temperature combustion gas (5M) is injected and horizontal axis (1h) Various energy storage cycle merging engines and merging methods for driving a plurality of contra-rotating simple gas engines (88q). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とし、高圧高温燃焼ガス(5M)を噴射して横軸(1h)二重反転複数組の簡単ガス機関(88q)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Theoretical combustion chamber (4Q) that receives low-priced liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply equipment (3D) and sets the compression volume to 21/60000 of air compression (4Q) Ultra high pressure fuel combustion + inner compression blade (8q) Outer compression blades (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production compressed air (28a) combustion, high pressure high temperature combustion gas (5M) is injected The horizontal axis (1h) is a combination of a plurality of simple gas engines (88q) with a double reversal, and various energy storage cycle coalescing engines and coalescence methods. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)に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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Theoretical combustion chamber (4Q) that receives low-priced liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply equipment (3D) and sets the compression volume to 21/60000 of air compression (4Q) Ultra high pressure fuel combustion + inner compression blade (8q) Outer compression blades (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Various energy storage to make simple gas engine (88q) as combustion Cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)に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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receive cold liquid oxygen (5K) + electricity from cold water + hot water to superheated steam hot water supply facility (3D), theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output wing (8s) Outer output wing (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion engine for various energy storage cycles and a coalescence method for simple gas engine (88q) combustion. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)に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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold liquid + high temperature water to superheated steam temperature supply facility (3D) receives cheap liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Various energy storage cycle coalescence engine and coalescence method for simple gas engine (88q) combustion . 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として最大速度にする簡単ガス機関(88q)に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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Theoretical combustion chamber (4Q) that receives low-priced liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply equipment (3D) and sets the compression volume to 21/60000 of air compression (4Q) Ultra high pressure fuel combustion + inner compression blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Various energy storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として最大速度にする簡単ガス機関(88q)に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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receive cold liquid oxygen (5K) + electricity from cold water + hot water to superheated steam hot water supply facility (3D), theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output wing (8s) Outer output wing (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion engine and combination of various energy storage cycles to make simple gas engine (88q) to maximum speed as combustion Method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として最大速度にする簡単ガス機関(88q)に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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold liquid + high temperature water to superheated steam temperature supply facility (3D) receives cheap liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combining various energy conservation cycles to make simple gas engine (88q) to maximum speed as combustion Organization and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として最大駆動速度にする簡単ガス機関(88q)に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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Theoretical combustion chamber (4Q) that receives low-priced liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply equipment (3D) and sets the compression volume to 21/60000 of air compression (4Q) Ultra high pressure fuel combustion + inner compression blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Simple gas engine (88q) for maximum driving speed as combustion Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として最大駆動速度にする簡単ガス機関(88q)に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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receive cold liquid oxygen (5K) + electricity from cold water + hot water to superheated steam hot water supply facility (3D), theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Various energy storage cycle coalesced engines for simple gas engine (88q) for maximum driving speed as combustion Merge method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として最大駆動速度にする簡単ガス機関(88q)に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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold liquid + high temperature water to superheated steam temperature supply facility (3D) receives cheap liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compressor blade (8q) outer compressor blade (8r) Inner output vane (8s) Outer output vane (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Various energy storage cycles to make a simple gas engine (88q) with maximum driving speed as combustion Merger engine and merger method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として最高速度にする簡単ガス機関(88q)に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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Theoretical combustion chamber (4Q) that receives low-priced liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply equipment (3D) and sets the compression volume to 21/60000 of air compression (4Q) Ultra high pressure fuel combustion + inner compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Various energy storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)は液体で圧縮し、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+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼する2種類理論燃焼室(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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) is received from cold water + high temperature water to superheated steam temperature heat supply equipment (3D), liquid fuel (1c) and water (52a) are compressed with liquid, and the compression volume is 21/60000 of air compression. Ultra high-pressure compressed fuel injection combustion by volume etc. + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Various energy storage cycle coalescing engine and coalescence method to make two kinds of theoretical combustion chambers (4Q) to burn. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)は液体で圧縮し、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+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼する2種類理論燃焼室(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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receive cold liquid oxygen (5K) + electricity from cold heat + hot water to superheated steam temperature heat supply equipment (3D), compress liquid fuel (1c) and water (52a) with liquid, and reduce the compression volume to 21 of air compression / Ultra high pressure compressed fuel injection combustion with 60000 volume etc. + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air ( 28a) Various energy storage cycle coalescing engines and coalescence methods for making two types of theoretical combustion chambers (4Q) to burn. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)は液体で圧縮し、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+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼する2種類理論燃焼室(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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receiving cheap liquid oxygen (5K) + electricity + hot water from cold heat + hot water to superheated steam hot water supply equipment (3D), liquid fuel (1c) and water (52a) are compressed with liquid, and the compressed volume is air Ultra-high pressure compressed fuel injection combustion with 21/60000 volume of compression + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter reversal manufacture Various energy storage cycle coalescing engines and coalescence methods for two types of theoretical combustion chambers (4Q) that burn with compressed air (28a). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)は液体で圧縮して理論燃焼室(4Q)内壁で最適温度に加熱+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receives cheap liquid oxygen (5K) from cold heat + hot water to superheated steam temperature supply equipment (3D), compresses liquid fuel (1c) and water (52a) with liquid, and is optimal on the inner wall of the theoretical combustion chamber (4Q) Heating to temperature + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Merger engine and merger method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)は液体で圧縮して理論燃焼室(4Q)内壁で最適温度に加熱+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cool liquid + high temperature water to superheated steam temperature supply equipment (3D) receives cheap liquid oxygen (5K) + electricity, liquid fuel (1c) and water (52a) are compressed with liquid, and the inner wall of theoretical combustion chamber (4Q) Heating to optimum temperature + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + horizontal axis bearing load 0 approaching counter-rotating production compressed air (28a) Storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)は液体で圧縮して理論燃焼室(4Q)内壁で最適温度に加熱+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold liquid + high temperature water to superheated steam temperature supply facility (3D) receives cheap liquid oxygen (5K) + electricity + high temperature water, and liquid fuel (1c) and water (52a) are compressed with liquid to theoretical combustion chamber ( 4Q) Heating to the optimum temperature on the inner wall + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) combustion Various energy storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)は液体で圧縮して理論燃焼室(4Q)内壁で最適温度に加熱+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼酸素噴射ノズル(6L)+燃料噴射ノズル(6X)+過熱蒸気噴射ノズル(6A)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receives cheap liquid oxygen (5K) from cold heat + hot water to superheated steam temperature supply equipment (3D), compresses liquid fuel (1c) and water (52a) with liquid, and is optimal on the inner wall of the theoretical combustion chamber (4Q) Heating to temperature + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion oxygen injection nozzle (6L ) + Fuel injection nozzle (6X) + superheated steam injection nozzle (6A) various energy storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)は液体で圧縮して理論燃焼室(4Q)内壁で最適温度に加熱+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼酸素噴射ノズル(6L)+燃料噴射ノズル(6X)+過熱蒸気噴射ノズル(6A)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cool liquid + high temperature water to superheated steam temperature supply equipment (3D) receives cheap liquid oxygen (5K) + electricity, liquid fuel (1c) and water (52a) are compressed with liquid, and the inner wall of theoretical combustion chamber (4Q) To the optimum temperature + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion oxygen injection nozzle (6L) + Fuel-injection nozzle (6X) + superheated steam injection nozzle (6A), various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)は液体で圧縮して理論燃焼室(4Q)内壁で最適温度に加熱+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼酸素噴射ノズル(6L)+燃料噴射ノズル(6X)+過熱蒸気噴射ノズル(6A)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold liquid + high temperature water to superheated steam temperature supply facility (3D) receives cheap liquid oxygen (5K) + electricity + high temperature water, and liquid fuel (1c) and water (52a) are compressed with liquid to theoretical combustion chamber ( 4Q) Heating to the optimum temperature on the inner wall + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) combustion Various energy storage cycle coalescence engines and coalescence methods for opening the oxygen injection nozzle (6L) + fuel injection nozzle (6X) + superheated steam injection nozzle (6A). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)は液体で圧縮して理論燃焼室(4Q)内壁で最適温度に加熱+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼酸素噴射ノズル(6L)+燃料噴射ノズル(6X)+過熱蒸気噴射ノズル(6A)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) + high temperature water is received from cold heat + high temperature water to superheated steam temperature heat supply equipment (3D), and liquid fuel (1c) and water (52a) are compressed with liquid and theoretical combustion chamber (4Q) Heated to optimum temperature at inner wall + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion oxygen injection Various energy storage cycle coalescence engines and coalescence methods for injecting a nozzle (6L) + fuel injection nozzle (6X) + superheated steam injection nozzle (6A) together with an open received superheated steam. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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噴射ノズル(6L)+燃料噴射ノズル(6X)+過熱蒸気噴射ノズル(6A)を開放+過熱蒸気(50)を加熱+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼する理論燃焼室(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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receiving cheap liquid oxygen (5K) from cold water + hot water to superheated steam temperature supply equipment (3D), heated oxygen injection nozzle (6L) + fuel injection nozzle (6X) + superheated steam injection nozzle (6A) to the optimum temperature + Heating superheated steam (50) + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) ) Various energy storage cycle coalescing engine and coalescence method to make the theoretical combustion chamber (4Q) to burn. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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噴射ノズル(6L)+燃料噴射ノズル(6X)+過熱蒸気噴射ノズル(6A)を開放+過熱蒸気(50)を加熱+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼する理論燃焼室(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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receiving cheap liquid oxygen (5K) + electricity from cold heat + hot water to superheated steam temperature heat supply equipment (3D), heating oxygen injection nozzle (6L) + fuel injection nozzle (6X) + superheated steam injection nozzle ( 6A) is opened + superheated steam (50) is heated + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Various energy storage cycle coalescing engine and coalescence method for making a theoretical combustion chamber (4Q) to burn. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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噴射ノズル(6L)+燃料噴射ノズル(6X)+過熱蒸気噴射ノズル(6A)を開放+過熱蒸気(50)を加熱+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼する2種類理論燃焼室(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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receiving cold liquid + hot water to superheated steam hot water supply facility (3D) cheaper liquid oxygen (5K) + electricity + hot water, heated oxygen injection nozzle (6L) + fuel injection nozzle (6X) + superheated steam to the optimum temperature Open injection nozzle (6A) + Heat superheated steam (50) + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approach double reversal Manufacture compressed air (28a) Two types of theoretical combustion chambers (4Q) to burn various energy storage cycle coalescing engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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噴射ノズル(6L)+燃料噴射ノズル(6X)+過熱蒸気噴射ノズル(6A)を開放+過熱蒸気(50)を加熱高温にする+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼2種類理論燃焼室(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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receiving cheap liquid oxygen (5K) from cold water + hot water to superheated steam temperature supply equipment (3D), heated oxygen injection nozzle (6L) + fuel injection nozzle (6X) + superheated steam injection nozzle (6A) to the optimum temperature + Heating superheated steam (50) to high temperature + Inner compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production compression Various energy storage cycle coalescing engine and coalescence method for making two types of combustion chambers (4Q) with air (28a) combustion. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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噴射ノズル(6L)+燃料噴射ノズル(6X)+過熱蒸気噴射ノズル(6A)を開放+過熱蒸気(50)を加熱高温にする+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼2種類理論燃焼室(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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receiving cheap liquid oxygen (5K) + electricity from cold heat + hot water to superheated steam temperature heat supply equipment (3D), heating oxygen injection nozzle (6L) + fuel injection nozzle (6X) + superheated steam injection nozzle ( 6A) is opened + superheated steam (50) is heated to high temperature + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + horizontal axis bearing load 0 approach double reversal Various types of energy storage cycle coalescence engine and coalescence method for producing compressed air (28a) combustion and two types of theoretical combustion chamber (4Q). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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噴射ノズル(6L)+燃料噴射ノズル(6X)+過熱蒸気噴射ノズル(6A)を開放+過熱蒸気(50)を加熱高温にする+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼2種類理論燃焼室(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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receiving cold liquid + hot water to superheated steam hot water supply facility (3D) cheaper liquid oxygen (5K) + electricity + hot water, heated oxygen injection nozzle (6L) + fuel injection nozzle (6X) + superheated steam to the optimum temperature Open injection nozzle (6A) + Superheated steam (50) is heated to high temperature + Inner compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load approach 0 Various energy storage cycle coalescing engine and coalescence method for producing two types of theoretical combustion chambers (4Q) with counter-rotating manufactured compressed air (28a) combustion. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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噴射ノズル(6L)+燃料噴射ノズル(6X)+過熱蒸気噴射ノズル(6A)を開放+過熱蒸気(50)を加熱する+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼2種類理論燃焼室(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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receiving cheap liquid oxygen (5K) from cold water + hot water to superheated steam temperature supply equipment (3D), heated oxygen injection nozzle (6L) + fuel injection nozzle (6X) + superheated steam injection nozzle (6A) to the optimum temperature + Heating superheated steam (50) + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air ( 28a) Various types of energy storage cycle coalescence engine and coalescence method for making two kinds of combustion theoretical combustion chambers (4Q). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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噴射ノズル(6L)+燃料噴射ノズル(6X)+過熱蒸気噴射ノズル(6A)を開放+過熱蒸気(50)を加熱する+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼2種類理論燃焼室(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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receiving cheap liquid oxygen (5K) + electricity from cold heat + hot water to superheated steam temperature heat supply equipment (3D), heating oxygen injection nozzle (6L) + fuel injection nozzle (6X) + superheated steam injection nozzle ( 6A) is opened + superheated steam (50) is heated + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + horizontal shaft bearing load 0 approaching counter-rotating production compression Various energy storage cycle coalescing engine and coalescence method for making two types of combustion chambers (4Q) with air (28a) combustion. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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噴射ノズル(6L)+燃料噴射ノズル(6X)+過熱蒸気噴射ノズル(6A)を開放+過熱蒸気(50)を加熱する+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼2種類理論燃焼室(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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receiving cold liquid + hot water to superheated steam hot water supply facility (3D) cheaper liquid oxygen (5K) + electricity + hot water, heated oxygen injection nozzle (6L) + fuel injection nozzle (6X) + superheated steam to the optimum temperature Open the injection nozzle (6A) + heat the superheated steam (50) + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + horizontal shaft bearing load 0 approach double Various energy storage cycle coalescing engine and coalescence method for producing two types of inverted combustion air (28a) combustion theoretical combustion chamber (4Q). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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噴射ノズル(6L)+燃料噴射ノズル(6X)+過熱蒸気噴射ノズル(6A)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)を加熱する+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼2種類理論燃焼室(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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receiving cheap liquid oxygen (5K) + high temperature water from cold heat + high temperature water to superheated steam temperature supply equipment (3D), heated oxygen injection nozzle (6L) + fuel injection nozzle (6X) + superheated steam injection nozzle to the optimum temperature Heat the outer superheated steam (50) including the received superheated steam by combustion at 3000 ° C. or more in the vicinity of the center of the open oxygen fuel burner (6A) + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output Blades (8t) + horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion 2 types of theoretical combustion chamber (4Q) Various energy storage cycle coalescing engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)を複数具備の高圧高温燃焼ガス(5M)噴射加速噴射+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼の簡単空気噴射機関(88r)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) is received from cold heat + high temperature water to superheated steam temperature heat supply equipment (3D), and high pressure high temperature combustion gas (5M) injection acceleration injection + inner compression blades (multiple theoretical combustion chambers (4Q)) 8q) Outer compressor blades (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion simple air injection engine (88r) Cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)を複数具備の高圧高温燃焼ガス(5M)噴射加速噴射+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼の簡単空気噴射機関(88r)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) + electricity is received from cold water + high temperature water to superheated steam temperature heat supply equipment (3D), high pressure high temperature combustion gas (5M) injection acceleration injection + inner compression with multiple theoretical combustion chambers (4Q) Blades (8q) Outer compression blades (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion simple air injection engine (88r) Energy conservation cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)を複数具備の高圧高温燃焼ガス(5M)噴射加速噴射+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼の簡単空気噴射機関(88r)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receive cold liquid oxygen (5K) + electricity + hot water from cold water + hot water to superheated steam hot water supply equipment (3D), high pressure hot combustion gas (5M) injection accelerated injection with multiple theoretical combustion chambers (4Q) + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion simple air injection engine (88r) Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)を複数具備の高圧高温燃焼ガス(5M)で(4Q)内壁の酸素+燃料+過熱蒸気を最適温度加熱して使用+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼する簡単空気噴射機関(88r)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) is received from cold heat + hot water to superheated steam temperature heat supply equipment (3D), and oxygen in the inner wall of (4Q) is high pressure high temperature combustion gas (5M) equipped with a plurality of theoretical combustion chambers (4Q) + Fuel + Superheated steam heated at optimal temperature + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air ( 28a) Various energy storage cycle coalescing engines and coalescence methods for a simple air injection engine (88r) that burns. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)を複数具備の高圧高温燃焼ガス(5M)で(4Q)内壁の酸素+燃料+過熱蒸気を最適温度加熱して使用+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼する簡単空気噴射機関(88r)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) + electricity is received from cold heat + high temperature water to superheated steam temperature heat supply equipment (3D), and high pressure high temperature combustion gas (5M) having a plurality of theoretical combustion chambers (4Q) Oxygen + fuel + superheated steam heated at optimal temperature + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + horizontal shaft bearing load 0 approaching counter-rotating production compression Various energy storage cycle coalescing engines and coalescing methods in a simple air injection engine (88r) that burns air (28a). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)を複数具備の高圧高温燃焼ガス(5M)で(4Q)内壁の酸素+燃料+過熱蒸気を最適温度加熱して使用+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼する簡単空気噴射機関(88r)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receiving low temperature liquid oxygen (5K) + electricity + high temperature water from cold heat + high temperature water to superheated steam temperature supply equipment (3D), high pressure high temperature combustion gas (5M) with multiple theoretical combustion chambers (4Q) (4Q ) Inner wall oxygen + fuel + superheated steam heated at optimal temperature + inner compressor blade (8q) outer compressor blade (8r) inner output blade (8s) outer output blade (8t) + horizontal shaft bearing load 0 approach double Various energy storage cycle coalescing engine and coalescence method in the form of a simple air injection engine (88r) that burns inverted compressed air (28a). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)を複数具備の高圧高温燃焼ガス(5M)で(4Q)内壁の酸素+燃料+過熱蒸気を最適温度加熱+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼して2種類理論燃焼室(4Q)燃焼等にする簡単空気噴射機関(88r)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) is received from cold heat + hot water to superheated steam temperature heat supply equipment (3D), and oxygen in the inner wall of (4Q) is high pressure high temperature combustion gas (5M) equipped with a plurality of theoretical combustion chambers (4Q) + Fuel + superheated steam at optimum temperature heating + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + horizontal axis bearing load 0 approach counter-rotating production compressed air (28a) combustion Then, various energy storage cycle coalescing engines and coalescence methods that are made into a simple air injection engine (88r) to make two kinds of theoretical combustion chambers (4Q) combustion, etc. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)を複数具備の高圧高温燃焼ガス(5M)で(4Q)内壁の酸素+燃料+過熱蒸気を最適温度加熱+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼して2種類理論燃焼室(4Q)燃焼等にする簡単空気噴射機関(88r)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) + electricity is received from cold heat + high temperature water to superheated steam temperature heat supply equipment (3D), and high pressure high temperature combustion gas (5M) having a plurality of theoretical combustion chambers (4Q) Oxygen + fuel + superheated steam at optimum temperature heating + inner compressor blade (8q) outer compressor blade (8r) inner output blade (8s) outer output blade (8t) + horizontal axis bearing load 0 approaching counter-rotating manufactured compressed air (28a) ) Various energy storage cycle coalescence engine and coalescence method in a simple air injection engine (88r) that burns into two types of theoretical combustion chamber (4Q) combustion and the like. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)を複数具備の高圧高温燃焼ガス(5M)で(4Q)内壁の酸素+燃料+過熱蒸気を最適温度加熱+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼して2種類理論燃焼室(4Q)燃焼等にする簡単空気噴射機関(88r)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receiving low temperature liquid oxygen (5K) + electricity + high temperature water from cold heat + high temperature water to superheated steam temperature supply equipment (3D), high pressure high temperature combustion gas (5M) with multiple theoretical combustion chambers (4Q) (4Q ) Inner wall oxygen + fuel + superheated steam at optimum temperature heating + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + horizontal shaft bearing load 0 approaching counter-rotating production compression Various energy storage cycle coalescing engine and coalescence method, which is a simple air injection engine (88r) that burns air (28a) into two types of theoretical combustion chamber (4Q) combustion, etc. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)を複数具備の高圧高温燃焼ガス(5M)で(4Q)内壁の酸素+燃料+受給高温水を含む過熱蒸気を最適温度加熱+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼して2種類理論燃焼室(4Q)燃焼等にする簡単空気噴射機関(88r)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) + high temperature water is received from cold heat + high temperature water to superheated steam temperature heat supply equipment (3D), and the inner wall of the high pressure high temperature combustion gas (5M) with multiple theoretical combustion chambers (4Q) (4Q) Oxygen + Fuel + Superheated steam containing high-temperature water received at optimum temperature heating + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Double bearing load approaching zero Various energy storage cycle coalescing engine and coalescence method, which is a simple air injection engine (88r) which burns inversion manufactured compressed air (28a) to form two kinds of theoretical combustion chambers (4Q) combustion and the like. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、内壁で酸素+燃料+過熱蒸気を最適温度加熱して2種類理論燃焼室(4Q)燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼の簡単空気噴射機関(88r)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold liquid + hot water to superheated steam temperature supply equipment (3D) receives cheap liquid oxygen (5K), oxygen + fuel + superheated steam is heated at the optimum temperature on the inner wall, and two types of theoretical combustion chamber (4Q) combustion + inside Compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion simple air injection engine (88r) Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、内壁で酸素+燃料+過熱蒸気を最適温度加熱+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼して2種類理論燃焼室(4Q)燃焼の簡単空気噴射機関(88r)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receiving low temperature liquid oxygen (5K) + electricity from cold heat + hot water to superheated steam temperature supply equipment (3D), oxygen + fuel + superheated steam at the inner wall at the optimum temperature heating + inner compressor blade (8q) outer compressor blade ( 8r) Inner output vane (8s) Outer output vane (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) burned and two types of theoretical combustion chamber (4Q) combustion simple air injection engine (88r) Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、内壁で酸素+燃料+過熱蒸気を最適温度加熱して理論燃焼室(4Q)燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼の簡単空気噴射機関(88r)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) + electricity + high temperature water is received from cold heat + high temperature water to superheated steam heat supply equipment (3D), and oxygen + fuel + superheated steam is heated at the optimum temperature on the inner wall, theoretical combustion chamber (4Q) Combustion + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion simple air injection engine (88r) ) Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、内壁で酸素+燃料+過熱蒸気を最適温度加熱して理論燃焼室(4Q)燃焼する+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼の簡単空気噴射機関(88r)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receiving cheap liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply facility (3D), heating oxygen + fuel + superheated steam at the optimum temperature on the inner wall and burning in the theoretical combustion chamber (4Q) + inner compression Blades (8q) Outer compression blades (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion simple air injection engine (88r) Energy conservation cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、内壁で酸素+燃料+過熱蒸気を最適温度加熱して理論燃焼室(4Q)燃焼する+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼の簡単空気噴射機関(88r)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold liquid + hot water to superheated steam temperature supply equipment (3D) receives cheap liquid oxygen (5K) + electricity, and oxygen + fuel + superheated steam is heated at the optimum temperature on the inner wall and burned in the theoretical combustion chamber (4Q) + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion simple air injection engine (88r) Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、内壁で酸素+燃料+過熱蒸気を最適温度加熱して理論燃焼室(4Q)燃焼する+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼の簡単空気噴射機関(88r)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) + electricity + high temperature water is received from cold heat + high temperature water to superheated steam heat supply equipment (3D), and oxygen + fuel + superheated steam is heated at the optimum temperature on the inner wall, theoretical combustion chamber (4Q) Combustion + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion simple air injection engine ( 88r) various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、内壁で酸素+燃料+過熱蒸気を最適温度加熱して理論燃焼室(4Q)燃焼で高温水加熱管(5H)の過熱蒸気(50)を加熱噴射+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼する簡単空気噴射機関(88r)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receive cold liquid oxygen (5K) from cold water + high temperature water to superheated steam temperature supply facility (3D), heat oxygen + fuel + superheated steam at the inner wall at the optimum temperature, and heat high temperature water in the theoretical combustion chamber (4Q) combustion Superheated steam (50) of pipe (5H) is heated and injected + Inner compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production compression Various energy storage cycle coalescing engines and coalescing methods in a simple air injection engine (88r) that burns air (28a). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、内壁で酸素+燃料+過熱蒸気を最適温度加熱して理論燃焼室(4Q)燃焼で高温水加熱管(5H)の過熱蒸気(50)を加熱噴射+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼する簡単空気噴射機関(88r)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) + electricity is received from cold heat + hot water to superheated steam temperature supply equipment (3D), oxygen + fuel + superheated steam is heated at the optimum temperature on the inner wall, and the temperature is high in the theoretical combustion chamber (4Q) combustion Superheated steam (50) of water heating pipe (5H) is heated and injected + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + horizontal axis bearing load 0 approach double reversal Manufacturing compressed air (28a) Various energy storage cycle coalescing engine and coalescing method in a simple air injection engine (88r) that burns. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、内壁で酸素+燃料+過熱蒸気を最適温度加熱して理論燃焼室(4Q)燃焼で高温水加熱管(5H)の過熱蒸気(50)を加熱噴射+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼する簡単空気噴射機関(88r)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) + electricity + high temperature water is received from cold heat + high temperature water to superheated steam heat supply equipment (3D), and oxygen + fuel + superheated steam is heated at the optimum temperature on the inner wall, theoretical combustion chamber (4Q) Combustion and heating injection of superheated steam (50) in high-temperature water heating pipe (5H) + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + approach to horizontal shaft bearing load 0 Combined engine and method for combining various energy storage cycles into a simple air injection engine (88r) that burns counter-rotating manufactured compressed air (28a). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、内壁で酸素+燃料+過熱蒸気を最適温度加熱して理論燃焼室(4Q)燃焼で高温水加熱管(5H)の受給過熱蒸気を含む過熱蒸気(50)を加熱噴射+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼する簡単空気噴射機関(88r)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) + high temperature water is received from cold heat + high temperature water to superheated steam temperature supply equipment (3D), and oxygen + fuel + superheated steam is heated at the optimum temperature on the inner wall, and the combustion in the theoretical combustion chamber (4Q) Superheated steam (50) including superheated steam received by the high-temperature water heating pipe (5H) is heated and injected + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + horizontal shaft bearing Various energy storage cycle coalescing engine and coalescence method, which is a simple air injection engine (88r) that burns with zero-load approaching counter-rotating manufactured compressed air (28a). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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理論燃焼室(4Q)具備同様に燃焼噴射+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼する簡単空気噴射機関(88r)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receive cold liquid oxygen (5K) from cold water + hot water to superheated steam hot water supply equipment (3D), and also inject the air (28a) at the optimum location for suction injection flow as well as multiple theoretical combustion chambers (4Q) combustion injection + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combusting simple air injection engine (88r) Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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理論燃焼室(4Q)具備同様に燃焼噴射+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼する簡単空気噴射機関(88r)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold liquid + hot water to superheated steam hot water supply facility (3D) receives cheap liquid oxygen (5K) + electricity, and burns in the same way with multiple theoretical combustion chambers (4Q) at the optimum location of air (28a) suction jet flow Injection + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + horizontal shaft bearing load 0 approaching counter-rotating production compressed air (28a) Burning simple air injection engine (88r) ) Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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理論燃焼室(4Q)具備同様に燃焼噴射+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼する簡単空気噴射機関(88r)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receiving low temperature liquid oxygen (5K) + electricity + high temperature water from cold heat + high temperature water to superheated steam temperature heat supply equipment (3D), air (28a) also equipped with multiple theoretical combustion chambers (4Q) at the optimum place of suction injection flow Similarly, combustion injection + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + horizontal axis bearing load 0 approaching counter-rotating production compressed air (28a) Various energy storage cycle coalescing engine and coalescence method for engine (88r). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、簡単空気噴射機関(88r)にして空気入口を前向+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receiving cheap liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply equipment (3D), making it a simple air injection engine (88r) with the air inlet facing forward + inner compression blade (8q) outer compression blade ( 8r) Inner output vane (8s) Outer output vane (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combusted various energy storage cycle coalescing engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、簡単空気噴射機関(88r)にして空気入口を前向+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receiving cheap liquid oxygen (5K) + electricity from cold heat + hot water to superheated steam heat supply equipment (3D), making it a simple air injection engine (88r), forward air inlet + outer compression blade (8q) outer compression Blades (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combusted various energy storage cycle coalescing engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、簡単空気噴射機関(88r)にして空気入口を前向+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold liquid + high temperature water-superheated steam temperature supply equipment (3D) receives cheap liquid oxygen (5K) + electricity + high temperature water, makes it a simple air injection engine (88r), air inlet forward + inner compression blade (8q ) Outer compression blades (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combusted various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、簡単空気噴射機関(88r)にして空気入口を前向+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receiving cheap liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply equipment (3D), making it a simple air injection engine (88r) with the air inlet facing forward + inner compression blade (8q) outer compression blade ( 8r) Inner output wing (8s) Outer output wing (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combusting various energy storage cycle coalesced engines that approach the straight line and inject maximum bubbles to the bottom of the ship, Merge method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、簡単空気噴射機関(88r)にして空気入口を前向+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receiving cheap liquid oxygen (5K) + electricity from cold heat + hot water to superheated steam heat supply equipment (3D), making it a simple air injection engine (88r), forward air inlet + outer compression blade (8q) outer compression Wing (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combusting various energy conservation cycle coalescing near the straight line and injecting bubbles to the bottom of the ship Organization and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、簡単空気噴射機関(88r)にして空気入口を前向+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold liquid + high temperature water-superheated steam temperature supply equipment (3D) receives cheap liquid oxygen (5K) + electricity + high temperature water, makes it a simple air injection engine (88r), air inlet forward + inner compression blade (8q ) Outer compression wing (8r) Inner output wing (8s) Outer output wing (8t) + Horizontal axis bearing load 0 approaching counter-rotating production Compressed air (28a) Combusting and approaching a straight line, various energies to inject maximum bubbles to the bottom of the ship Storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、簡単空気噴射機関(88r)にして空気入口を前向+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold liquid + high temperature water to superheated steam temperature supply equipment (3D) receives low-priced liquid oxygen (5K) + high temperature water, makes it a simple air injection engine (88r), forward air inlet + outside inner compression blade (8q) outside Compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combusting various energy storage cycles that inject bubbles to the bottom of the ship close to a straight line Merger engine and merger method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)を複数具備の高圧高温燃焼ガス(5M)噴射加速噴射+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼の簡単噴射機関(88s)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) is received from cold heat + high temperature water to superheated steam temperature heat supply equipment (3D), and high pressure high temperature combustion gas (5M) injection acceleration injection + inner compression blades (multiple theoretical combustion chambers (4Q)) 8q) Outer compression blades (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Various energy storage cycles in a simple injection engine (88s) for combustion Merger engine and merger method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)を複数具備の高圧高温燃焼ガス(5M)噴射加速噴射+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼の簡単噴射機関(88s)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) + electricity is received from cold water + high temperature water to superheated steam temperature heat supply equipment (3D), high pressure high temperature combustion gas (5M) injection acceleration injection + inner compression with multiple theoretical combustion chambers (4Q) Blades (8q) Outer compression blades (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion simple injection engine (88s) Storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)を複数具備の高圧高温燃焼ガス(5M)噴射加速噴射+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼の簡単噴射機関(88s)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receive cold liquid oxygen (5K) + electricity + hot water from cold water + hot water to superheated steam hot water supply equipment (3D), high pressure hot combustion gas (5M) injection accelerated injection with multiple theoretical combustion chambers (4Q) + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion simple injection engine (88s) Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)を複数具備の高圧高温燃焼ガス(5M)で(4Q)内壁の酸素+燃料+過熱蒸気を最適温度加熱して使用+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼する簡単噴射機関(88s)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) is received from cold heat + hot water to superheated steam temperature heat supply equipment (3D), and oxygen in the inner wall of (4Q) is high pressure high temperature combustion gas (5M) equipped with a plurality of theoretical combustion chambers (4Q) + Fuel + Superheated steam heated at optimal temperature + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air ( 28a) Various energy storage cycle coalescing engines and coalescing methods in a simple injection engine (88s) for burning. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)を複数具備の高圧高温燃焼ガス(5M)で(4Q)内壁の酸素+燃料+過熱蒸気を最適温度加熱して使用+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼する簡単噴射機関(88s)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) + electricity is received from cold heat + high temperature water to superheated steam temperature heat supply equipment (3D), and high pressure high temperature combustion gas (5M) having a plurality of theoretical combustion chambers (4Q) Oxygen + fuel + superheated steam heated at optimal temperature + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + horizontal shaft bearing load 0 approaching counter-rotating production compression Various energy storage cycle coalescing engine and coalescence method in a simple injection engine (88s) that burns air (28a). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)を複数具備の高圧高温燃焼ガス(5M)で(4Q)内壁の酸素+燃料+過熱蒸気を最適温度加熱して使用+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼する簡単噴射機関(88s)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receiving low temperature liquid oxygen (5K) + electricity + high temperature water from cold heat + high temperature water to superheated steam temperature supply equipment (3D), high pressure high temperature combustion gas (5M) with multiple theoretical combustion chambers (4Q) (4Q ) Inner wall oxygen + fuel + superheated steam heated at optimal temperature + inner compressor blade (8q) outer compressor blade (8r) inner output blade (8s) outer output blade (8t) + horizontal shaft bearing load 0 approach double Various energy storage cycle coalescing engine and coalescence method in a simple injection engine (88s) that burns with inverted manufactured compressed air (28a). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)を複数具備の高圧高温燃焼ガス(5M)で(4Q)内壁の酸素+燃料+過熱蒸気を最適温度加熱+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼して2種類理論燃焼室(4Q)燃焼等にする簡単噴射機関(88s)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) is received from cold heat + hot water to superheated steam temperature heat supply equipment (3D), and oxygen in the inner wall of (4Q) is high pressure high temperature combustion gas (5M) equipped with a plurality of theoretical combustion chambers (4Q) + Fuel + superheated steam at optimum temperature heating + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + horizontal axis bearing load 0 approach counter-rotating production compressed air (28a) combustion Then, various energy storage cycle coalescing engines and coalescence methods that are made into a simple injection engine (88s) for two types of theoretical combustion chamber (4Q) combustion or the like. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)を複数具備の高圧高温燃焼ガス(5M)で(4Q)内壁の酸素+燃料+過熱蒸気を最適温度加熱+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼して2種類理論燃焼室(4Q)燃焼等にする簡単噴射機関(88s)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) + electricity is received from cold heat + high temperature water to superheated steam temperature heat supply equipment (3D), and high pressure high temperature combustion gas (5M) having a plurality of theoretical combustion chambers (4Q) Oxygen + fuel + superheated steam at optimum temperature heating + inner compressor blade (8q) outer compressor blade (8r) inner output blade (8s) outer output blade (8t) + horizontal axis bearing load 0 approaching counter-rotating manufactured compressed air (28a) ) Various energy storage cycle coalescing engine and coalescence method in a simple injection engine (88s) that burns into two types of theoretical combustion chamber (4Q) combustion, etc. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)を複数具備の高圧高温燃焼ガス(5M)で(4Q)内壁の酸素+燃料+過熱蒸気を最適温度加熱+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼して2種類理論燃焼室(4Q)燃焼等にする簡単噴射機関(88s)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receiving low temperature liquid oxygen (5K) + electricity + high temperature water from cold heat + high temperature water to superheated steam temperature supply equipment (3D), high pressure high temperature combustion gas (5M) with multiple theoretical combustion chambers (4Q) (4Q ) Inner wall oxygen + fuel + superheated steam at optimum temperature heating + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + horizontal shaft bearing load 0 approaching counter-rotating production compression Various energy storage cycle coalescing engine and coalescence method, which is a simple injection engine (88s) that burns air (28a) into two types of theoretical combustion chamber (4Q) combustion, etc. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、理論燃焼室(4Q)を複数具備の高圧高温燃焼ガス(5M)で(4Q)内壁の酸素+燃料+受給高温水を含む過熱蒸気を最適温度加熱+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼して2種類理論燃焼室(4Q)燃焼等にする簡単噴射機関(88s)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) + high temperature water is received from cold heat + high temperature water to superheated steam temperature heat supply equipment (3D), and the inner wall of the high pressure high temperature combustion gas (5M) with multiple theoretical combustion chambers (4Q) (4Q) Oxygen + Fuel + Superheated steam containing high-temperature water received at optimum temperature heating + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Double bearing load approaching zero Various energy storage cycle coalescing engine and coalescence method in a simple injection engine (88s) which burns inversion manufactured compressed air (28a) to make two types of theoretical combustion chamber (4Q) combustion, etc. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、内壁で酸素+燃料+過熱蒸気を最適温度加熱して理論燃焼室(4Q)燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼の簡単噴射機関(88s)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receive cold liquid oxygen (5K) from cold water + hot water to superheated steam temperature supply facility (3D), heat oxygen + fuel + superheated steam on the inner wall at the optimum temperature, theoretical combustion chamber (4Q) combustion + inner compressor blade (8q) Outer compression blades (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion simple injection engine (88s) Cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、内壁で酸素+燃料+過熱蒸気を最適温度加熱して理論燃焼室(4Q)燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼の簡単噴射機関(88s)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) + electricity is received from cold water + hot water to superheated steam heat supply equipment (3D), oxygen + fuel + superheated steam is heated at the optimum temperature on the inner wall, and combustion in the theoretical combustion chamber (4Q) + inside Compressed blade (8q) Outer compressed blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion simple injection engine (88s) Energy conservation cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、内壁で酸素+燃料+過熱蒸気を最適温度加熱して理論燃焼室(4Q)燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼の簡単噴射機関(88s)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) + electricity + high temperature water is received from cold heat + high temperature water to superheated steam heat supply equipment (3D), and oxygen + fuel + superheated steam is heated at the optimum temperature on the inner wall, theoretical combustion chamber (4Q) Combustion + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion simple injection engine (88s) Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、内壁で酸素+燃料+過熱蒸気を最適温度加熱して理論燃焼室(4Q)燃焼する+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼の簡単噴射機関(88s)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receiving cheap liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply facility (3D), heating oxygen + fuel + superheated steam at the optimum temperature on the inner wall and burning in the theoretical combustion chamber (4Q) + inner compression Blades (8q) Outer compression blades (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion simple injection engine (88s) Storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、内壁で酸素+燃料+過熱蒸気を最適温度加熱して理論燃焼室(4Q)燃焼する+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼の簡単噴射機関(88s)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold liquid + hot water to superheated steam temperature supply equipment (3D) receives cheap liquid oxygen (5K) + electricity, and oxygen + fuel + superheated steam is heated at the optimum temperature on the inner wall and burned in the theoretical combustion chamber (4Q) + Inner compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion simple injection engine (88s) Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、内壁で酸素+燃料+過熱蒸気を最適温度加熱して理論燃焼室(4Q)燃焼する+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼の簡単噴射機関(88s)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) + electricity + high temperature water is received from cold heat + high temperature water to superheated steam heat supply equipment (3D), and oxygen + fuel + superheated steam is heated at the optimum temperature on the inner wall, theoretical combustion chamber (4Q) Combustion + Inner compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion simple injection engine (88s ) Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、内壁で酸素+燃料+過熱蒸気を最適温度加熱して理論燃焼室(4Q)燃焼で高温水加熱管(5H)の過熱蒸気(50)を加熱噴射+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼する簡単噴射機関(88s)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receive cold liquid oxygen (5K) from cold water + high temperature water to superheated steam temperature supply facility (3D), heat oxygen + fuel + superheated steam at the inner wall at the optimum temperature, and heat high temperature water in the theoretical combustion chamber (4Q) combustion Superheated steam (50) of pipe (5H) is heated and injected + Inner compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production compression Various energy storage cycle coalescing engine and coalescence method in a simple injection engine (88s) that burns air (28a). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、内壁で酸素+燃料+過熱蒸気を最適温度加熱して理論燃焼室(4Q)燃焼で高温水加熱管(5H)の過熱蒸気(50)を加熱噴射+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼する簡単噴射機関(88s)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) + electricity is received from cold heat + hot water to superheated steam temperature supply equipment (3D), oxygen + fuel + superheated steam is heated at the optimum temperature on the inner wall, and the temperature is high in the theoretical combustion chamber (4Q) combustion Superheated steam (50) of water heating pipe (5H) is heated and injected + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + horizontal axis bearing load 0 approach double reversal Manufacture compressed air (28a) A simple injection engine (88s) combusting various energy storage cycle coalescing engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、内壁で酸素+燃料+過熱蒸気を最適温度加熱して理論燃焼室(4Q)燃焼で高温水加熱管(5H)の過熱蒸気(50)を加熱噴射+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼する簡単噴射機関(88s)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) + electricity + high temperature water is received from cold heat + high temperature water to superheated steam heat supply equipment (3D), and oxygen + fuel + superheated steam is heated at the optimum temperature on the inner wall, theoretical combustion chamber (4Q) Combustion and heating injection of superheated steam (50) in high-temperature water heating pipe (5H) + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + approach to horizontal shaft bearing load 0 Combined engine and method for combining various energy storage cycles into a simple injection engine (88s) that burns counter-rotating manufactured compressed air (28a). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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、内壁で酸素+燃料+過熱蒸気を最適温度加熱して理論燃焼室(4Q)燃焼で高温水加熱管(5H)の受給過熱蒸気を含む過熱蒸気(50)を加熱噴射+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼する簡単噴射機関(88s)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) + high temperature water is received from cold heat + high temperature water to superheated steam temperature supply equipment (3D), and oxygen + fuel + superheated steam is heated at the optimum temperature on the inner wall, and the combustion in the theoretical combustion chamber (4Q) Superheated steam (50) including superheated steam received by the high-temperature water heating pipe (5H) is heated and injected + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + horizontal shaft bearing Various energy storage cycle coalescing engine and coalescence method in a simple injection engine (88s) that burns with zero-load approaching counter-rotating manufactured compressed air (28a). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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理論燃焼室(4Q)噴射部具備同様に燃焼噴射+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼する簡単噴射機関(88s)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receive cold liquid oxygen (5K) from cold water + hot water to superheated steam hot water supply facility (3D), and burn in the same way with multiple theoretical combustion chambers (4Q) injection units at the optimal location of air (28a) suction injection flow Injection + Inner compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion simple injection engine (88s) Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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理論燃焼室(4Q)噴射部具備同様に燃焼噴射+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼する簡単噴射機関(88s)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receiving cheap liquid oxygen (5K) + electricity from cold water + hot water to superheated steam temperature heat supply equipment (3D), air (28a) as well as a plurality of theoretical combustion chambers (4Q) injection parts at the optimum place of suction injection flow Combustion injection + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + horizontal shaft bearing load 0 approaching counter-rotating production compressed air (28a) 88s) various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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理論燃焼室(4Q)噴射部具備同様に燃焼噴射+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼する簡単噴射機関(88s)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receiving low temperature liquid oxygen (5K) + electricity + high temperature water from cold heat + high temperature water to superheated steam temperature heat supply equipment (3D), multiple theoretical combustion chambers (4Q) injection at the optimum place of air (28a) suction injection flow Combustion injection + Inner compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approach counter-rotating manufactured compressed air (28a) Various energy storage cycle coalescing engine and coalescence method for an injection engine (88s). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼して、簡単噴射機関(88s)と共に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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receiving cheap liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply equipment (3D) + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + horizontal axis Various energy storage cycle coalescence engines and coalescence methods that burn with compressed air (28a) approaching bearing load 0 approach and rotating with a simple injection engine (88s) to enable vertical ascent and descent. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼して、簡単噴射機関(88s)と共に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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold oxygen + low temperature liquid oxygen (5K) + electricity received from the hot water to superheated steam temperature supply facility (3D) + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + Various energy storage cycle coalescence engines and coalescence methods that burn with compressed air (28a) near the horizontal axis bearing load 0 and rotate with the simple injection engine (88s) to enable vertical ascent and descent. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼して、簡単噴射機関(88s)と共に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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) + electricity + high temperature water received from cold heat + high temperature water to superheated steam temperature supply equipment (3D) + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade ( 8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) combusted and rotated with a simple injection engine (88s) 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+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼して、簡単噴射機関(88s)と共に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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Receiving cheap liquid oxygen (5K) from cold heat + hot water to superheated steam heat supply equipment (3D) + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + horizontal axis Various energy storage cycle coalescence engines and coalescence methods in which compressed air (28a) is burned with a bearing load approaching zero and rotated with a simple injection engine (88s) to enable reverse injection. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼して、簡単噴射機関(88s)と共に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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold oxygen + low temperature liquid oxygen (5K) + electricity received from the hot water to superheated steam temperature supply facility (3D) + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + Various energy storage cycle coalescence engines and coalescence methods in which compressed air (28a) is combusted with a horizontal axis bearing load close to zero and rotated with a simple injection engine (88s) to enable reverse injection. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼して、簡単噴射機関(88s)と共に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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) + electricity + high temperature water received from cold heat + high temperature water to superheated steam temperature supply equipment (3D) + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade ( 8t) + horizontal axis bearing load 0 approaching counter-rotating manufactured compressed air (28a) combusted and rotated with a simple injection engine (88s) to enable reverse injection and various energy storage cycle combined engines and methods. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼して、簡単噴射機関(88s)と共に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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold heat + high temperature water to superheated steam temperature supply equipment (3D) less expensive liquid oxygen (5K) + high temperature water received + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) burns and rotates with a simple injection engine (88s) to enable reverse injection, and various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)として電気+高温水(52b)を供給液体酸素製造する、簡単狙い吸入速度最大にする電気駆動の両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Electricity + hot water (52b) is supplied as cold heat + hot water to superheated steam hot water supply equipment (3D), liquid oxygen production, easy aiming to maximize suction speed, both sides center support bearing combined load 0 approach + horizontal shaft bearing Various energy storage cycle coalescence engines and coalescence methods with a load 0 approaching simple multistage compressor (3h) + liquid oxygen production machine (88p). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)として電気を供給液体酸素製造する、簡単狙い吸入速度最大にする電気駆動の両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Electricity is supplied as cold heat + hot water to superheated steam heat supply equipment (3D) Liquid oxygen production, easy aiming to maximize the suction speed, both sides of the center drive bearing combined with electric drive 0 approach + horizontal shaft bearing load 0 approach easy multistage compression Various energy storage cycle coalescence engine and coalescence method as a machine (3h) + liquid oxygen production machine (88p). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)として電気+過熱蒸気を供給液体酸素製造する、簡単狙い吸入速度最大にする電気駆動の両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold + hot water to superheated steam temperature supply equipment (3D) Electricity + superheated steam supply liquid oxygen production, easy aiming to maximize suction speed, double-sided center support bearing combined load approach 0 + horizontal axis bearing load approach 0 Various energy storage cycle coalescence engines and coalescence methods as simple multistage compressor (3h) + liquid oxygen production machine (88p). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)として電気+高温水(52b)を供給液体酸素製造する、簡単狙い吸入速度最大にする電気駆動の両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)として液体酸素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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Electricity + hot water (52b) is supplied as cold heat + hot water to superheated steam hot water supply equipment (3D), liquid oxygen production, easy aiming to maximize suction speed, both sides center support bearing combined load 0 approach + horizontal shaft bearing Various energy storage cycle coalescence engine and coalescence method for producing liquid oxygen as a load 0 approaching simple multistage compressor (3h) + liquid oxygen production machine (88p). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)として電気を供給液体酸素製造する、簡単狙い吸入速度最大にする電気駆動の両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)として液体酸素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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Electricity is supplied as cold heat + hot water to superheated steam heat supply equipment (3D) Liquid oxygen production, easy aiming to maximize the suction speed, both sides of the center drive bearing combined with electric drive 0 approach + horizontal shaft bearing load 0 approach easy multistage compression Various energy storage cycle coalescence engine and coalescence method for producing liquid oxygen as a machine (3h) + liquid oxygen production machine (88p). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)として電気+過熱蒸気を供給液体酸素製造する、簡単狙い吸入速度最大にする電気駆動の両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)として液体酸素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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold + hot water to superheated steam temperature supply equipment (3D) Electricity + superheated steam supply liquid oxygen production, easy aiming to maximize suction speed, double-sided center support bearing combined load approach 0 + horizontal axis bearing load approach 0 Various energy storage cycle coalescence engines and coalescence methods for producing liquid oxygen as a simple multistage compressor (3h) + liquid oxygen production machine (88p). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)として電気+高温水(52b)を供給液体酸素製造する、簡単狙い吸入速度最大にする電気駆動の両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Electricity + hot water (52b) is supplied as cold heat + hot water to superheated steam hot water supply equipment (3D), liquid oxygen production, easy aiming to maximize suction speed, both sides center support bearing combined load 0 approach + horizontal shaft bearing Various energy storage cycle coalescence engines and coalescence methods for producing compressed heat exchange superheated steam by sucking air as a load 0 approaching simple multistage compressor (3h) + liquid oxygen production machine (88p). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)として電気を供給液体酸素製造する、簡単狙い吸入速度最大にする電気駆動の両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Electricity is supplied as cold heat + hot water to superheated steam heat supply equipment (3D) Liquid oxygen production, easy aiming to maximize the suction speed, both sides of the center drive bearing combined with electric drive 0 approach + horizontal shaft bearing load 0 approach easy multistage compression Various energy storage cycle coalescence engine and coalescence method for producing compressed heat exchange superheated steam by sucking air as a machine (3h) + liquid oxygen production machine (88p). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)として電気+過熱蒸気を供給液体酸素製造する、簡単狙い吸入速度最大にする電気駆動の両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold + hot water to superheated steam temperature supply equipment (3D) Electricity + superheated steam supply liquid oxygen production, easy aiming to maximize suction speed, double-sided center support bearing combined load approach 0 + horizontal axis bearing load approach 0 Various energy storage cycle coalescence engines and coalescence methods for producing compressed heat exchange superheated steam by sucking air as a simple multistage compressor (3h) + liquid oxygen production machine (88p). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)として電気+高温水(52b)+過熱蒸気を供給液体酸素製造する、簡単狙い吸入速度最大にする電気駆動の両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Electricity + hot water (52b) + superheated steam supply liquid oxygen production as cold heat + hot water to superheated steam heat supply facility (3D), easy aiming to maximize suction speed, double-sided center support bearing load combined 0 approach + Various energy storage cycle coalescence engine and coalescence method for producing compressed heat exchange superheated steam by sucking air as a multistage compressor (3h) + liquid oxygen producing machine (88p) with a horizontal axis bearing load approaching zero. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)として電気+高温水(52b)を供給液体酸素製造する、簡単狙い吸入速度最大にする電気駆動の両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)として液体窒素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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Electricity + hot water (52b) is supplied as cold heat + hot water to superheated steam hot water supply equipment (3D), liquid oxygen production, easy aiming to maximize suction speed, both sides center support bearing combined load 0 approach + horizontal shaft bearing Various energy storage cycle coalescence engine and coalescence method for producing liquid nitrogen as a load 0 approaching simple multistage compressor (3h) + liquid oxygen production machine (88p). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)として電気を供給液体酸素製造する、簡単狙い吸入速度最大にする電気駆動の両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)として液体窒素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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Electricity is supplied as cold heat + hot water to superheated steam heat supply equipment (3D) Liquid oxygen production, easy aiming to maximize the suction speed, both sides of the center drive bearing combined with electric drive 0 approach + horizontal shaft bearing load 0 approach easy multistage compression Various energy storage cycle coalescence engine and coalescence method for producing liquid nitrogen as a machine (3h) + liquid oxygen production machine (88p). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)として電気+過熱蒸気を供給液体酸素製造する、簡単狙い吸入速度最大にする電気駆動の両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)として液体窒素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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold + hot water to superheated steam temperature supply equipment (3D) Electricity + superheated steam supply liquid oxygen production, easy aiming to maximize suction speed, double-sided center support bearing combined load approach 0 + horizontal axis bearing load approach 0 Various energy storage cycle coalescence engine and coalescence method for producing liquid nitrogen as a simple multistage compressor (3h) + liquid oxygen production machine (88p). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)として電気+高温水(52b)を供給液体酸素製造する、簡単狙い吸入速度最大にする電気駆動の両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)として液体窒素を製造供給設備(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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Electricity + hot water (52b) is supplied as cold heat + hot water to superheated steam hot water supply equipment (3D), liquid oxygen production, easy aiming to maximize suction speed, both sides center support bearing combined load 0 approach + horizontal shaft bearing Various energy storage cycle coalescence engine and coalescence method for supplying liquid nitrogen to the production supply facility (3D) as a load 0 approaching simple multistage compressor (3h) + liquid oxygen production machine (88p). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)として電気を供給液体酸素製造する、簡単狙い吸入速度最大にする電気駆動の両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)として液体窒素を製造供給設備(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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Electricity is supplied as cold heat + hot water to superheated steam heat supply equipment (3D) Liquid oxygen production, easy aiming to maximize the suction speed, both sides of the center drive bearing combined with electric drive 0 approach + horizontal shaft bearing load 0 approach easy multistage compression Various energy storage cycle coalescence engine and coalescence method for supplying liquid nitrogen to the production supply facility (3D) as a machine (3h) + liquid oxygen production machine (88p). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)として電気+過熱蒸気を供給液体酸素製造する、簡単狙い吸入速度最大にする電気駆動の両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)として液体窒素を製造供給設備(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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold + hot water to superheated steam temperature supply equipment (3D) Electricity + superheated steam supply liquid oxygen production, easy aiming to maximize suction speed, double-sided center support bearing combined load approach 0 + horizontal axis bearing load approach 0 Various energy storage cycle coalescence engines and coalescence methods for supplying liquid nitrogen to the production supply facility (3D) as a simple multistage compressor (3h) + liquid oxygen production machine (88p). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)として電気+高温水(52b)を供給液体酸素製造する、簡単狙い吸入速度最大にする電気駆動の両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)として液体窒素+液体酸素+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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Electricity + hot water (52b) is supplied as cold heat + hot water to superheated steam hot water supply equipment (3D), liquid oxygen production, easy aiming to maximize suction speed, both sides center support bearing combined load 0 approach + horizontal shaft bearing Various energy storage cycle coalescence engines and coalescence methods for supplying liquid nitrogen + liquid oxygen + superheated steam to the production and supply equipment (3D) as a load 0 approaching simple multistage compressor (3h) + liquid oxygen production machine (88p). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)として電気を供給液体酸素製造する、簡単狙い吸入速度最大にする電気駆動の両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)として液体窒素+液体酸素+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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Electricity is supplied as cold heat + hot water to superheated steam heat supply equipment (3D) Liquid oxygen production, easy aiming to maximize the suction speed, both sides of the center drive bearing combined with electric drive 0 approach + horizontal shaft bearing load 0 approach easy multistage compression Various energy storage cycle coalescence engine and coalescence method for supplying liquid nitrogen + liquid oxygen + superheated steam to the production supply facility (3D) as a machine (3h) + liquid oxygen production machine (88p). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)として電気+過熱蒸気を供給液体酸素製造する、簡単狙い吸入速度最大にする電気駆動の両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)として液体窒素+液体酸素+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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold + hot water to superheated steam temperature supply equipment (3D) Electricity + superheated steam supply liquid oxygen production, easy aiming to maximize suction speed, double-sided center support bearing combined load approach 0 + horizontal axis bearing load approach 0 Various energy storage cycle coalescence engine and coalescence method for supplying liquid nitrogen + liquid oxygen + superheated steam to the production supply facility (3D) as a simple multistage compressor (3h) + liquid oxygen production machine (88p). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)として電気+高温水(52b)+過熱蒸気を供給液体酸素製造する、簡単狙い吸入速度最大にする電気駆動の両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)として液体窒素+液体酸素+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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Electricity + hot water (52b) + superheated steam supply liquid oxygen production as cold heat + hot water to superheated steam heat supply facility (3D), easy aiming to maximize suction speed, double-sided center support bearing load combined 0 approach + Various energy storage cycle coalescence engine and coalescence method for supplying liquid nitrogen + liquid oxygen + superheated steam to the production supply facility (3D) as a multi-stage compressor (3h) + liquid oxygen production machine (88p) with a horizontal shaft bearing load of 0 approach. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)極端に安価発電電気駆動の、両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)を簡単として吸入速度最大に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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears. Various energy storage cycle coalescence engines and coalescence methods that are configured to maximize the intake speed by simplifying the load coalescence 0 approach + horizontal shaft bearing load 0 approach easy multistage compressor (3h) + liquid oxygen production machine (88p). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)極端に安価発電電気駆動の、両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)を簡単として吸入速度最大に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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears. Various energy storage cycle coalescence engines and coalescence methods for compressing air as a constitution that maximizes the suction speed by simplifying the load coalescence 0 approach + horizontal shaft bearing load 0 approach easy multistage compressor (3h) + liquid oxygen production machine (88p). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)極端に安価発電電気駆動の、両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)を簡単として吸入速度最大に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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears. Various energy storage cycle coalescence engines and coalescence that compress air (28a) as a configuration that maximizes the suction speed by simplifying the load coalescence 0 approach + horizontal shaft bearing load 0 approach easy multistage compressor (3h) + liquid oxygen production machine (88p) Method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)極端に安価発電電気駆動の、両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)を簡単として吸入速度最大にする構成として1〜複数段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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears. Various energy storage cycle coalescence engines and coalescence that compress one to several stages as a structure that maximizes the suction speed by simplifying the load coalescence 0 approach + horizontal shaft bearing load 0 approach easy multistage compressor (3h) + liquid oxygen production machine (88p) Method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)極端に安価発電電気駆動の、両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)を簡単として吸入速度最大にする構成として1〜複数段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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears. Load uniting approach 0 + horizontal axis bearing load approaching 0 easy multi-stage compressor (3h) + liquid oxygen production machine (88p) as a configuration that maximizes the suction speed and various energy storage cycle coalescing to heat 1 to multi-stage compressed water Organization and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)極端に安価発電電気駆動の、両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)を簡単として吸入速度最大にする構成として1〜複数段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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears. Various energy storage cycles for heating 1 to multi-stage compressed high-temperature water as a structure that maximizes the suction speed by simplifying the load coalescence 0 approach + horizontal shaft bearing load 0 approach simple multistage compressor (3h) + liquid oxygen production machine (88p) Merger engine and merger method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)極端に安価発電電気駆動の、両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)を簡単として吸入速度最大にする構成として1〜複数段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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears. Various energy storage cycles for heating 1 to multi-stage compressed superheated steam as a structure that maximizes the suction speed by simplifying multi-stage compressor (3h) + liquid oxygen production machine (88p) with load coalescence 0 approach + horizontal shaft bearing load 0 approach Merger engine and merger method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)極端に安価発電電気駆動の、両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)を簡単として吸入速度最大にする構成として1〜複数段圧縮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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears. Various energy storage cycles in which water is heated by 1 to multi-stage compression as a structure that maximizes the suction speed by simplifying multi-stage compressor (3h) + liquid oxygen production machine (88p) with load approach 0 approach + horizontal shaft bearing load 0 approach Merger engine and merger method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)極端に安価発電電気駆動の、両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)を簡単として吸入速度最大にする構成として1〜複数段圧縮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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears. Various energy storages that heat high-temperature water with 1 to multi-stage compression as a structure that maximizes the suction speed by simplifying multi-stage compressor (3h) + liquid oxygen production machine (88p) with load union approaching 0 + horizontal axis bearing load approaching 0 Cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)極端に安価発電電気駆動の、両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)を簡単として吸入速度最大にする構成として1〜複数段圧縮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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears. Various energy storage cycle coalescence engines and coalescence methods in which superheated steam is heated by 1 to multi-stage compression as a configuration that maximizes the suction speed by simplifying the load coalescence 0 approach + horizontal shaft bearing load 0 approach simple multistage compressor (3h). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)極端に安価発電電気駆動の、両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)を簡単として吸入速度最大にする構成として圧縮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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears. Various energy storage cycle coalescence engines and coalescence that produce superheated steam by compression as a structure that maximizes the suction speed by simplifying the load coalescence 0 approach + horizontal shaft bearing load 0 approach easy multistage compressor (3h) + liquid oxygen production machine (88p) Method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)極端に安価発電電気駆動の、両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)を簡単として吸入速度最大にする構成として圧縮で液体酸素+液体窒素+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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears. Various energy to produce liquid oxygen + liquid nitrogen + superheated steam by compression as a structure that maximizes the suction speed by simplifying multi-stage compressor (3h) + liquid oxygen production machine (88p) with load coalescence 0 approach + horizontal shaft bearing load 0 approach Storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)極端に安価発電電気駆動の、両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)を簡単として吸入速度最大にする構成として圧縮で液体酸素+液体窒素+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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears. Load uniting approach 0 + horizontal shaft bearing load approaching 0 easy multi-stage compressor (3h) + liquid oxygen production machine (88p) as a configuration that maximizes the suction speed and various types of liquid oxygen + liquid nitrogen + high pressure superheated steam production by compression Energy conservation cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)極端に安価発電電気駆動の、両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)を簡単として吸入速度最大にする構成として圧縮で液体酸素+液体窒素+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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears. Compressed liquid oxygen + liquid nitrogen + super high pressure superheated steam is produced as a structure that maximizes the suction speed by simplifying the load coalescence 0 approach + horizontal axis bearing load 0 approach simple multistage compressor (3h) + liquid oxygen production machine (88p) Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)極端に安価発電電気駆動の、両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)を簡単として吸入速度最大にする構成として圧縮で液体酸素+液体窒素+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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears. Compressed liquid oxygen + liquid nitrogen + superheated steam production and supply equipment as a configuration that maximizes the suction speed by simplifying the load coalescence 0 approach + horizontal shaft bearing load 0 approach simple multistage compressor (3h) + liquid oxygen production machine (88p) ( 3D) various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)極端に安価発電電気駆動の、両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)を簡単として吸入速度最大にする構成として圧縮で液体酸素+液体窒素+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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears. Compressed liquid oxygen + liquid nitrogen + high pressure superheated steam production and supply equipment with a structure that maximizes the suction speed by simplifying the multi-stage compressor (3h) + liquid oxygen production machine (88p) Various energy storage cycle coalescence engines and coalescence methods supplied to (3D). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)極端に安価発電電気駆動の、両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)を簡単として吸入速度最大にする構成として圧縮で液体窒素+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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears. Compressed liquid nitrogen + super high pressure superheated steam production and supply equipment (3D) as a configuration that maximizes the suction speed by simplifying multi-stage compressor (3h) + liquid oxygen production machine (88p) with load coalescence 0 approach + horizontal shaft bearing load 0 approach ) Various energy storage cycle coalescence engines and coalescence methods to be supplied to 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)極端に安価発電電気駆動の、両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)を簡単として吸入速度最大にする構成として圧縮で液体酸素+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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears. Compressed liquid oxygen + super high pressure superheated steam production and supply equipment (3D) with a structure that maximizes the suction speed by simplifying multi-stage compressor (3h) + liquid oxygen producing machine (88p) ) Various energy storage cycle coalescence engines and coalescence methods to be supplied to 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)極端に安価発電電気駆動の、両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)を簡単として吸入速度最大にする構成として圧縮で液体酸素+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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears. Compressed liquid oxygen + liquid nitrogen + super high pressure superheated steam production supply as a structure that maximizes the suction speed by simplifying multi-stage compressor (3h) + liquid oxygen production machine (88p) Various energy storage cycle coalescence engines and coalescence methods to be supplied to the facility (3D). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)極端に安価発電電気駆動の、両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)を簡単として吸入速度最大にする構成として圧縮で電気+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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears. Load uniting 0 approach + horizontal axis bearing load 0 approach simple multi-stage compressor (3h) + liquid oxygen production machine (88p) as a configuration that maximizes suction speed by compression with electricity + liquid oxygen + liquid nitrogen + super high pressure superheated steam Various energy storage cycle coalescence engine and coalescence method to be supplied to the production supply facility (3D). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)より両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単ガス機関(88q)に安価液体酸素(5K)を受給燃料噴射燃焼+圧縮空気に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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) is received into the gas engine (88q) with low-temperature + hot water to superheated steam heat supply equipment (3D), both sides center support bearing combined unity approach + horizontal axis bearing load 0 approach, fuel injection combustion + compressed air Various energy storage cycle coalescence engine and coalescence method for fuel injection and combustion. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)より両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単噴射機関(88s)に安価液体酸素(5K)を受給燃料噴射燃焼+圧縮空気に燃料噴射燃焼の2種類に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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low-temperature liquid oxygen (5K) is received into the simple injection engine (88s) from both sides of the central support bearing load combined 0 approach from the cold heat + hot water to superheated steam heat supply facility (3D) Fuel injection combustion + compressed air Various types of energy storage cycle coalescing engine and coalescence method for making two types of fuel injection and combustion. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)より両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単空気噴射機関(88r)に安価液体酸素(5K)を受給燃料噴射燃焼+圧縮空気に燃料噴射燃焼の2種類理論燃焼室に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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low-temperature liquid oxygen (5K) is received into the air injection engine (88r) with low-temperature liquid oxygen (5K) received by fuel injection combustion + compression from cold + hot water to superheated steam heat supply equipment (3D) Various energy storage cycle coalescing engines and coalescence methods for making two types of theoretical combustion chambers for fuel injection combustion into air. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)より両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単ガス機関(88q)に安価液体酸素(5K)を受給燃料噴射燃焼+圧縮空気に燃料噴射燃焼の2種類理論燃焼室(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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) is received into the gas engine (88q) with low-temperature + hot water to superheated steam heat supply equipment (3D), both sides center support bearing combined unity approach + horizontal axis bearing load 0 approach, fuel injection combustion + compressed air Various energy storage cycle coalescing engines and coalescence methods for making two types of theoretical combustion chambers (4Q) for fuel injection combustion. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)より両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単噴射機関(88s)に安価液体酸素(5K)を受給燃料噴射燃焼+圧縮空気に燃料噴射燃焼の2種類理論燃焼室(4Q)にし1種類入口に開閉弁(1Q)具備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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low-temperature liquid oxygen (5K) is received into the simple injection engine (88s) from both sides of the central support bearing load combined 0 approach from the cold heat + hot water to superheated steam heat supply facility (3D) Fuel injection combustion + compressed air 2 types of energy storage cycle coalescence engine and coalescence method comprising two types of theoretical combustion chambers (4Q) for fuel injection combustion and an on-off valve (1Q) at one type of inlet. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)より両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単空気噴射機関(88r)に安価液体酸素(5K)を受給燃料噴射燃焼+圧縮空気に燃料噴射燃焼の2種類理論燃焼室(4Q)にし1種類入口に開閉弁(1Q)酸素噴射ノズル(6L)具備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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low-temperature liquid oxygen (5K) is received into the air injection engine (88r) with low-temperature liquid oxygen (5K) received by fuel injection combustion + compression from cold + hot water to superheated steam heat supply equipment (3D) Various energy storage cycle coalescence engines and coalescence methods comprising two types of theoretical combustion chambers (4Q) for fuel injection combustion into air, and one type of inlet / closing valve (1Q) oxygen injection nozzle (6L). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)より両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単ガス機関(88q)に安価液体酸素(5K)を受給燃料噴射燃焼+圧縮空気に燃料噴射燃焼の2種類理論燃焼室(4Q)にし1種類入口に開閉弁(1Q)酸素噴射ノズル(6L)燃料噴射ノズル(6X)具備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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) is received into the gas engine (88q) with low-temperature + hot water to superheated steam heat supply equipment (3D), both sides center support bearing combined unity approach + horizontal axis bearing load 0 approach, fuel injection combustion + compressed air Various types of energy storage cycle coalescence engines and coalescence methods comprising two types of theoretical combustion chambers (4Q) for fuel injection combustion and an on-off valve (1Q) oxygen injection nozzle (6L) fuel injection nozzle (6X) at one type inlet. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)より両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単噴射機関(88s)に安価液体酸素(5K)を受給燃料噴射燃焼+圧縮空気に燃料噴射燃焼の2種類理論燃焼室(4Q)にし1種類入口に開閉弁(1Q)酸素噴射ノズル(6L)燃料噴射ノズル(6X)具備開閉弁(1Q)閉止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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low-temperature liquid oxygen (5K) is received into the simple injection engine (88s) from both sides of the central support bearing load combined 0 approach from the cold heat + hot water to superheated steam heat supply facility (3D) Fuel injection combustion + compressed air Two types of theoretical combustion chambers (4Q) for fuel injection combustion, and various types of energy storage cycle coalescence engines that close an on-off valve (1Q), an oxygen injection nozzle (6L), a fuel injection nozzle (6X) and an on-off valve (1Q) at one type of inlet Merge method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)より両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単空気噴射機関(88r)に安価液体酸素(5K)を受給燃料噴射燃焼+圧縮空気に燃料噴射燃焼の2種類理論燃焼室(4Q)にし1種類入口に開閉弁(1Q)酸素噴射ノズル(6L)燃料噴射ノズル(6X)具備開閉弁(1Q)閉止酸素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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low-temperature liquid oxygen (5K) is received into the air injection engine (88r) with low-temperature liquid oxygen (5K) received by fuel injection combustion + compression from cold + hot water to superheated steam heat supply equipment (3D) Two types of theoretical combustion chamber (4Q) for fuel injection combustion into air One type of inlet / off valve (1Q) Oxygen injection nozzle (6L) Fuel injection nozzle (6X) On-off valve (1Q) Closed oxygen fuel injection Combustion various energy Storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)より両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単ガス機関(88q)に安価液体酸素(5K)を受給燃料噴射燃焼+圧縮空気に燃料噴射燃焼の2種類理論燃焼室(4Q)にし1種類入口に開閉弁(1Q)酸素噴射ノズル(6L)燃料噴射ノズル(6X)具備開閉弁(1Q)閉止酸素燃料噴射燃焼回転出力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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) is received into the gas engine (88q) with low-temperature + hot water to superheated steam heat supply equipment (3D), both sides center support bearing combined unity approach + horizontal axis bearing load 0 approach, fuel injection combustion + compressed air Two types of theoretical combustion chambers (4Q) for fuel injection combustion are provided, and one type of inlet is provided with an on-off valve (1Q), an oxygen injection nozzle (6L), a fuel injection nozzle (6X), an on-off valve (1Q), a closed oxygen fuel injection combustion rotation output increase. Various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)より両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単噴射機関(88s)に安価液体酸素(5K)を受給燃料噴射燃焼+圧縮空気に燃料噴射燃焼の2種類理論燃焼室(4Q)にし1種類入口に開閉弁(1Q)酸素噴射ノズル(6L)燃料噴射ノズル(6X)具備開閉弁(1Q)閉止酸素燃料噴射燃焼回転出力増大2種類(4Q)過熱蒸気(50)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low-temperature liquid oxygen (5K) is received into the simple injection engine (88s) from both sides of the central support bearing load combined 0 approach from the cold heat + hot water to superheated steam heat supply facility (3D) Fuel injection combustion + compressed air Two kinds of theoretical combustion chambers (4Q) for fuel injection combustion are provided, and one kind of inlet is provided with an on-off valve (1Q), an oxygen injection nozzle (6L), a fuel injection nozzle (6X), an on-off valve (1Q), an increase in closed oxygen fuel injection combustion rotation output 2 Type (4Q) Superheated steam (50) Various energy storage cycle coalescing engine and coalescence method for injecting. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)より両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単空気噴射機関(88r)に安価液体酸素(5K)を受給燃料噴射燃焼+圧縮空気に燃料噴射燃焼の2種類理論燃焼室(4Q)にし1種類入口に開閉弁(1Q)酸素噴射ノズル(6L)燃料噴射ノズル(6X)具備開閉弁(1Q)閉止酸素燃料噴射燃焼回転出力増大2種類(4Q)過熱蒸気(50)噴射で燃焼ガス(49)を吸引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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low-temperature liquid oxygen (5K) is received into the air injection engine (88r) with low-temperature liquid oxygen (5K) received by fuel injection combustion + compression from cold + hot water to superheated steam heat supply equipment (3D) 2 types of theoretical combustion chamber (4Q) for fuel injection combustion into air 1 type inlet on / off valve (1Q) oxygen injection nozzle (6L) fuel injection nozzle (6X) on-off valve (1Q) closed oxygen fuel injection combustion rotation output increase Various energy storage cycle coalescing engines and coalescence methods for sucking and injecting combustion gas (49) by two types (4Q) superheated steam (50) injection. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)より両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単ガス機関(88q)に安価液体酸素(5K)を受給燃料噴射燃焼+圧縮空気に燃料噴射燃焼の2種類理論燃焼室(4Q)にし1種類入口に開閉弁(1Q)酸素噴射ノズル(6L)燃料噴射ノズル(6X)具備開閉弁(1Q)閉止酸素燃料噴射燃焼回転出力増大2種類(4Q)過熱蒸気(50)噴射で燃焼ガス(49)を吸引噴射噴射推進出力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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) is received into the gas engine (88q) with low-temperature + hot water to superheated steam heat supply equipment (3D), both sides center support bearing combined unity approach + horizontal axis bearing load 0 approach, fuel injection combustion + compressed air Two kinds of theoretical combustion chambers (4Q) for fuel injection combustion are provided, and one kind of inlet is provided with an on-off valve (1Q), an oxygen injection nozzle (6L), a fuel injection nozzle (6X), an on-off valve (1Q), an increase in closed oxygen fuel injection combustion rotation output 2 Various energy storage cycle coalescing engine and coalescence method for increasing the suction injection injection propulsion output of combustion gas (49) by type (4Q) superheated steam (50) injection. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)より両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単噴射機関(88s)に安価液体酸素(5K)を受給燃料噴射燃焼+圧縮空気に燃料噴射燃焼の2種類理論燃焼室(4Q)にし1種類入口出口に開閉弁(1Q)酸素噴射ノズル(6L)燃料噴射ノズル(6X)具備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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low-temperature liquid oxygen (5K) is received into the simple injection engine (88s) from both sides of the central support bearing load combined 0 approach from the cold heat + hot water to superheated steam heat supply facility (3D) Fuel injection combustion + compressed air Various types of energy storage cycle coalescence engine and coalescence method comprising two types of theoretical combustion chambers (4Q) for fuel injection combustion, and one type of inlet / outlet opening / closing valve (1Q), oxygen injection nozzle (6L) and fuel injection nozzle (6X). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)より両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単空気噴射機関(88r)に安価液体酸素(5K)を受給燃料噴射燃焼+圧縮空気に燃料噴射燃焼の2種類理論燃焼室(4Q)にし1種類入口出口に開閉弁(1Q)酸素噴射ノズル(6L)燃料噴射ノズル(6X)具備開閉弁(1Q)閉止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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low-temperature liquid oxygen (5K) is received into the air injection engine (88r) with low-temperature liquid oxygen (5K) received by fuel injection combustion + compression from cold + hot water to superheated steam heat supply equipment (3D) Two types of theoretical combustion chamber (4Q) for fuel injection combustion into air One type of inlet / outlet opening / closing valve (1Q) Oxygen injection nozzle (6L) Fuel injection nozzle (6X) Equipped with various on-off valves (1Q) Organization and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)より両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単ガス機関(88q)に安価液体酸素(5K)を受給燃料噴射燃焼+圧縮空気に燃料噴射燃焼の2種類理論燃焼室(4Q)にし1種類入口出口に開閉弁(1Q)酸素噴射ノズル(6L)燃料噴射ノズル(6X)具備開閉弁(1Q)閉止酸素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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low temperature liquid oxygen (5K) is received into the gas engine (88q) with low-temperature + hot water to superheated steam heat supply equipment (3D), both sides center support bearing combined unity approach + horizontal axis bearing load 0 approach, fuel injection combustion + compressed air Two types of fuel injection combustion in the theoretical combustion chamber (4Q), one type at the inlet and outlet at the on-off valve (1Q) oxygen injection nozzle (6L) fuel injection nozzle (6X) on-off valve (1Q) closed oxygen fuel injection combustion energy Storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)より両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単噴射機関(88s)に安価液体酸素(5K)を受給燃料噴射燃焼+圧縮空気に燃料噴射燃焼の2種類理論燃焼室(4Q)にし1種類入口出口に開閉弁(1Q)酸素噴射ノズル(6L)燃料噴射ノズル(6X)具備開閉弁(1Q)閉止酸素燃料噴射燃焼高圧高温燃焼ガス(5M)を外周(6Y)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low-temperature liquid oxygen (5K) is received into the simple injection engine (88s) from both sides of the central support bearing load combined 0 approach from the cold heat + hot water to superheated steam heat supply facility (3D) Fuel injection combustion + compressed air 2 types of theoretical combustion chambers (4Q) for fuel injection combustion, 1 type of inlet / outlet on / off valve (1Q) oxygen injection nozzle (6L) fuel injection nozzle (6X) on-off valve (1Q) closed oxygen fuel injection combustion high pressure high temperature combustion Various energy storage cycle coalescence engines and coalescence methods for injecting gas (5M) to the outer periphery (6Y). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)より両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単噴射機関(88s)に安価液体酸素(5K)を受給燃料噴射燃焼+圧縮空気に燃料噴射燃焼の2種類理論燃焼室(4Q)にし1種類入口出口に開閉弁(1Q)酸素噴射ノズル(6L)燃料噴射ノズル(6X)具備開閉弁(1Q)閉止酸素燃料噴射燃焼高圧高温燃焼ガス(5M)を外周(6Y)噴射過熱蒸気(50)も外周(6A)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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Low-temperature liquid oxygen (5K) is received into the simple injection engine (88s) from both sides of the central support bearing load combined 0 approach from the cold heat + hot water to superheated steam heat supply facility (3D) Fuel injection combustion + compressed air 2 types of theoretical combustion chambers (4Q) for fuel injection combustion, 1 type of inlet / outlet on / off valve (1Q) oxygen injection nozzle (6L) fuel injection nozzle (6X) on-off valve (1Q) closed oxygen fuel injection combustion high pressure high temperature combustion Various energy storage cycle coalescence engines and coalescence methods for injecting gas (5M) into the outer circumference (6Y) and the outer circumference (6A) as well as overheated steam (50). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)より両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単噴射機関(88s)安価液体酸素(5K)を受給燃料噴射燃焼+圧縮空気に燃料噴射燃焼の2種類理論燃焼室(4Q)にし1種類入口出口に開閉弁(1Q)酸素噴射ノズル(6L)燃料噴射ノズル(6X)具備開閉弁(1Q)閉止酸素燃料噴射燃焼高圧高温燃焼ガス(5M)を外周(6Y)ロケット噴射過熱蒸気(50)も外周(6A)ロケット噴射噴射推進出力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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold heat + hot water to superheated steam heat supply facility (3D) Both sides center support bearing combined load 0 approach + horizontal shaft bearing load 0 approach Easy injection engine (88s) Low cost liquid oxygen (5K) received fuel injection combustion + compressed air 2 types of theoretical combustion chamber (4Q) of fuel injection combustion 1 type of inlet / outlet on / off valve (1Q) oxygen injection nozzle (6L) fuel injection nozzle (6X) on-off valve (1Q) closed oxygen fuel injection combustion high pressure high temperature combustion gas (5M) outer periphery (6Y) rocket injection superheated steam (50) also outer periphery (6A) rocket injection injection propulsion output various energy storage cycle coalescence engine and coalescence method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)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)より両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単空気噴射機関(88r)安価液体酸素(5K)を受給燃料噴射燃焼+圧縮空気に燃料噴射燃焼の2種類理論燃焼室(4Q)にし1種類入口出口に開閉弁(1Q)酸素噴射ノズル(6L)燃料噴射ノズル(6X)具備開閉弁(1Q)閉止酸素燃料噴射燃焼高圧高温燃焼ガス(5M)を外周(6Y)ロケット噴射過熱蒸気(50)も外周(6A)ロケット噴射して前方の水を吸引噴射噴射推進出力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。   Magnetically utilized bearing load approaching 0 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Electricity + liquid air of extremely low cost electric power production Cold air + hot water to superheated steam hot water supply facility (3D) Both sides center support bearing load combined 0 approach + horizontal shaft bearing load 0 approach Easy air injection engine (88r) Low cost liquid oxygen (5K) received Fuel injection combustion + Compressed air 2 types of theoretical combustion chambers (4Q) for fuel injection combustion, 1 type of inlet / outlet on / off valve (1Q) oxygen injection nozzle (6L) fuel injection nozzle (6X) on-off valve (1Q) closed oxygen fuel injection combustion high pressure high temperature combustion Various energy storage cycle coalescence engines and coalescence methods in which gas (5M) is injected into the outer periphery (6Y) rocket injection superheated steam (50) also into the outer periphery (6A) rocket, and the forward water is sucked, injected, and propulsion output is increased. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)真空中超高圧垂直下方に水噴射し重力加速度加速して円筒タービン翼群(8A)水平軸(16A)対向同期歯車(4C)直列同回転歯車(4D)回転して複数タービンで発電の電気駆動太陽光加熱器(21)+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)に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 0 approach + (4C) (4D) Horizontal type full-scale blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Water jet under vacuum ultra high pressure vertically and gravity acceleration acceleration The cylindrical turbine blade group (8A), the horizontal shaft (16A), the counter synchronous gear (4C), the series rotation gear (4D), and the electric drive solar heater (21) + inner compression blade (8q) ) Outer compressor blades (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approach easy multistage compressor (3h) + Liquid oxygen production machine (88p) Merge method. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)真空中超高圧垂直下方に水噴射し重力加速度加速して円筒タービン翼群(8A)水平軸(16A)直列同回転歯車(4D)回転して複数タービンで発電の電気駆動太陽光加熱器(21)+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)に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 0 approach + (4C) (4D) Horizontal type full-scale blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Water jet under vacuum ultra high pressure vertically and gravity acceleration acceleration Then, the cylindrical turbine blade group (8A), the horizontal shaft (16A), the series rotating gear (4D), and the electric drive solar heater (21) + the inner compression blades (8q) and the outer compression blades (8r) that generate electric power by a plurality of turbines. ) Various energy storage cycle coalescence engines and coalescence methods, including an inner output vane (8s), an outer output vane (8t), a horizontal shaft bearing load 0 approaching multistage compressor (3h), and a liquid oxygen production machine (88p). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)真空中超高圧垂直下方に水噴射し重力加速度加速して円筒タービン翼群(8A)水平軸(16A)回転して円筒タービン翼群(8A)多数発電の電気駆動太陽光加熱器(21)+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)に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 0 approach + (4C) (4D) Horizontal type full-scale blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Water jet under vacuum ultra high pressure vertically and gravity acceleration acceleration The cylindrical turbine blade group (8A) rotates horizontally (16A), and the cylindrical turbine blade group (8A) generates multiple electric drive solar heaters (21) + inner compression blades (8q) outer compression blades (8r) inside Various energy storage cycle coalescence engines and coalescence methods: output vane (8s) outer output vane (8t) + horizontal bearing load 0 approaching simple multistage compressor (3h) + liquid oxygen producing machine (88p). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)真空中超高圧垂直下方に水噴射し重力加速度加速して円筒タービン翼群(8A)水平軸(16A)回転して円筒タービン翼群(8A)20組発電の電気駆動太陽光加熱器(21)+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)に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 0 approach + (4C) (4D) Horizontal type full-scale blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Water jet under vacuum ultra high pressure vertically and gravity acceleration acceleration The cylindrical turbine blade group (8A) rotates horizontally (16A) and the cylindrical turbine blade group (8A) 20 sets of electric drive solar heater (21) + inner compressor blade (8q) outer compressor blade (8r) Various energy storage cycle coalescence engines and coalescence methods, including an inner output vane (8s), an outer output vane (8t), a horizontal bearing load 0 approaching simple multistage compressor (3h), and a liquid oxygen production machine (88p). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)真空中超高圧垂直下方に水噴射し重力加速度加速して円筒タービン翼群(8A)水平軸(16A)回転して円筒タービン翼群(8A)40組発電の電気駆動太陽光加熱器(21)+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)に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 0 approach + (4C) (4D) Horizontal type full-scale blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Water jet under vacuum ultra high pressure vertically and gravity acceleration acceleration The cylindrical turbine blade group (8A) rotates horizontally (16A) and the cylindrical turbine blade group (8A) 40 sets of electric drive solar heater (21) + inner compressor blade (8q) outer compressor blade (8r) Various energy storage cycle coalescence engines and coalescence methods, including an inner output vane (8s), an outer output vane (8t), a horizontal bearing load 0 approaching simple multistage compressor (3h), and a liquid oxygen production machine (88p). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)真空中超高圧垂直下方に水噴射し重力加速度加速して円筒タービン翼群(8A)水平軸(16A)回転して円筒タービン翼群(8A)80組発電の電気駆動太陽光加熱器(21)+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)に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 0 approach + (4C) (4D) Horizontal type full-scale blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Water jet under vacuum ultra high pressure vertically and gravity acceleration acceleration The cylindrical turbine blade group (8A) rotates horizontally (16A) and the cylindrical turbine blade group (8A) 80 sets of electric drive solar heater (21) + inner compressor blade (8q) outer compressor blade (8r) Various energy storage cycle coalescence engines and coalescence methods, including an inner output vane (8s), an outer output vane (8t), a horizontal bearing load 0 approaching simple multistage compressor (3h), and a liquid oxygen production machine (88p). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)真空中超高圧垂直下方に水噴射し重力加速度加速して円筒タービン翼群(8A)水平軸(16A)回転して円筒タービン翼群(8A)100組発電の電気駆動太陽光加熱器(21)+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)に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 0 approach + (4C) (4D) Horizontal type full-scale blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Water jet under vacuum ultra high pressure vertically and gravity acceleration acceleration The cylindrical turbine blade group (8A) rotates horizontally (16A) and the cylindrical turbine blade group (8A) 100 sets of electric drive solar heater (21) + inner compressor blade (8q) outer compressor blade (8r) Various energy storage cycle coalescence engines and coalescence methods, including an inner output vane (8s), an outer output vane (8t), a horizontal bearing load 0 approaching simple multistage compressor (3h), and a liquid oxygen production machine (88p). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)真空中超高圧垂直下方に水噴射し重力加速度加速して円筒タービン翼群(8A)水平軸(16A)回転して円筒タービン翼群(8A)150組発電の電気駆動太陽光加熱器(21)+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)に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 0 approach + (4C) (4D) Horizontal type full-scale blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Water jet under vacuum ultra high pressure vertically and gravity acceleration acceleration The cylindrical turbine blade group (8A) rotates horizontally (16A) and the cylindrical turbine blade group (8A) 150 sets of electric drive solar heater (21) + inner compressor blade (8q) outer compressor blade (8r) Various energy storage cycle coalescence engines and coalescence methods, including an inner output vane (8s), an outer output vane (8t), a horizontal bearing load 0 approaching simple multistage compressor (3h), and a liquid oxygen production machine (88p). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)真空中超高圧垂直下方に水噴射し重力加速度加速して円筒タービン翼群(8A)水平軸(16A)回転して円筒タービン翼群(8A)200組発電の電気駆動太陽光加熱器(21)+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近簡単多段圧縮機(3h)+液体酸素製造機(88p)に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 0 approach + (4C) (4D) Horizontal type full-scale blade hydrogravity turbine (8B) turbine blade (8b) with super high speed circumferential speed with magnetic gears Water jet under vacuum ultra high pressure vertically and gravity acceleration acceleration The cylindrical turbine blade group (8A) rotates horizontally (16A) and the cylindrical turbine blade group (8A) 200 sets of electric drive solar heater (21) + inner compressor blade (8q) outer compressor blade (8r) Various energy storage cycle coalescence engines and coalescence methods, including an inner output vane (8s), an outer output vane (8t), a horizontal bearing load 0 approaching simple multistage compressor (3h), and a liquid oxygen production machine (88p). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造物+ロケット燃焼+ジェット燃焼として両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単空気噴射機関(88r)等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 0 approach + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) power generation electrical product + rocket combustion + jet combustion on both sides as ultra high speed circumferential speed with magnetic gear Center support bearing load coalescence 0 approach + horizontal axis bearing load 0 approach simple air injection engine (88r) and other various energy storage cycle coalescence engines and coalescence methods. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造物+ロケット燃焼2箇所+ジェット燃焼2箇所として両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単空気噴射機関(88r)等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 0 approach + (4C) (4D) horizontal all-wheel blade water gravity turbine (8B) turbine blade (8b) power generation electrical product + 2 rocket combustion + jet combustion Various energy storage cycle coalescence engines and coalescence methods for driving two-way center support bearing load coalescence 0 approach + horizontal shaft bearing load 0 approach simple air injection engine (88r) and the like as two places. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造物+ロケット燃焼3箇所+ジェット燃焼3箇所として両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単空気噴射機関(88r)等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 0 approach + (4C) (4D) horizontal all-wheel blade water gravity turbine (8B) turbine blade (8b) power generation electric product + 3 rocket combustion + jet combustion with super high speed circumferential speed with magnetic gear Various energy storage cycle coalescence engines and coalescence methods for driving, for example, both sides center support bearing load coalescence 0 approach + horizontal shaft bearing load 0 approach simple air injection engine (88r) as three places. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造物+ロケット燃焼4箇所+ジェット燃焼4箇所として両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単空気噴射機関(88r)等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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) power generation electric product + 4 rocket combustion + jet combustion Various energy storage cycle coalescence engines and coalescence methods for driving, for example, both sides center support bearing load coalescence 0 approach + horizontal shaft bearing load 0 approach simple air injection engine (88r) as four places. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造物+ロケット燃焼5箇所+ジェット燃焼5箇所として両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単空気噴射機関(88r)等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 0 approach + (4C) (4D) horizontal all-wheel blade water gravity turbine (8B) turbine blade (8b) power generation electrical product + 5 rocket combustion + jet combustion Various energy storage cycle coalescing engines and coalescence methods for driving, for example, both sides center support bearing load coalescence 0 approach + horizontal shaft bearing load 0 approach simple air injection engine (88r) as 5 locations. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造物+ロケット燃焼6箇所+ジェット燃焼6箇所として両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単空気噴射機関(88r)等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 + (4C) (4D) horizontal full-speed blade hydrogravity turbine (8B) turbine blade (8b) power generation electrical product + 6 rocket combustion + jet combustion 6 types of energy storage cycle coalescence engine and coalescence method for driving the center support bearing load coalescence 0 approach + lateral shaft bearing load 0 approach and the simple air injection engine (88r) etc. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造物+ロケット燃焼+ジェット燃焼として両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単噴射機関(88s)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 0 approach + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) power generation electrical product + rocket combustion + jet combustion on both sides as ultra high speed circumferential speed with magnetic gear Various energy storage cycle coalescence engines and coalescence methods for driving a central support bearing load coalescence 0 approach + horizontal bearing load 0 approach simple injection engine (88s). 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造物+ロケット燃焼2箇所+ジェット燃焼2箇所として両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単噴射機関(88s)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 0 approach + (4C) (4D) horizontal all-wheel blade water gravity turbine (8B) turbine blade (8b) power generation electrical product + 2 rocket combustion + jet combustion Various energy storage cycle coalescence engine and coalescence method for driving both sides center support bearing load coalescence 0 approach + horizontal shaft bearing load 0 approach simple injection engine (88s) as two places. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造物+ロケット燃焼3箇所+ジェット燃焼3箇所として両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単噴射機関(88s)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 0 approach + (4C) (4D) horizontal all-wheel blade water gravity turbine (8B) turbine blade (8b) power generation electric product + 3 rocket combustion + jet combustion with super high speed circumferential speed with magnetic gear Various energy storage cycle coalescence engines and coalescence methods for driving both sides center support bearing load coalescence 0 approach + horizontal shaft bearing load 0 approach simple injection engine (88s) as three places. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造物+ロケット燃焼4箇所+ジェット燃焼4箇所として両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単噴射機関(88s)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 + (4C) (4D) Horizontal type full-blade hydrogravity turbine (8B) turbine blade (8b) power generation electric product + 4 rocket combustion + jet combustion Various energy storage cycle coalescence engines and coalescence methods for driving both sides center support bearing load coalescence 0 approach + horizontal shaft bearing load 0 approach simple injection engine (88s) as four locations. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造物+ロケット燃焼5箇所+ジェット燃焼5箇所として両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単噴射機関(88s)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 0 approach + (4C) (4D) horizontal all-wheel blade water gravity turbine (8B) turbine blade (8b) power generation electrical product + 5 rocket combustion + jet combustion Various energy storage cycle coalescing engines and coalescence methods for driving both sides center support bearing load coalescence 0 approach + horizontal shaft bearing load 0 approach simple injection engine (88s) as 5 locations. 磁気利用軸受荷重0接近+(4C)(4D)磁気歯車で超高速円周速度とした横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造物+ロケット燃焼6箇所+ジェット燃焼6箇所として両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単噴射機関(88s)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 + (4C) (4D) horizontal full-speed blade hydrogravity turbine (8B) turbine blade (8b) power generation electrical product + 6 rocket combustion + jet combustion 6 types of energy storage cycle coalescence engine and coalescence method for driving both sides center support bearing load coalescence 0 approach + horizontal axis bearing load 0 approach simple injection engine (88s). 横型全動翼水重力タービン(8B)タービン翼(8b)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、両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単空気噴射機関(88r)等駆動簡単空気噴射機関船舶(7L)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。   Horizontal full-blade water gravity turbine (8B) Turbine blade (8b) 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 manufacturing, Both sides center support bearing combined load 0 approach + horizontal shaft bearing load 0 approach Easy air injection engine (88r), etc. Driven simple air injection engine Vessel (7L) Various energy storage to inject the maximum amount of bubbles into the bottom vertical parallel plate (9Q) Cycle coalescence engine and coalescence method. 横型全動翼水重力タービン(8B)タービン翼(8b)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、両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単空気噴射機関(88r)等駆動スクリュー噴射船舶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。   Horizontal full-blade water gravity turbine (8B) Turbine blade (8b) 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 manufacturing, Both-side center support bearing load coalescence 0 approach + horizontal shaft bearing load 0 approach Easy air injection engine (88r) etc. Drive screw injection ship Various energy conservation cycle coalescence engine and coalescence that inject maximum bubbles into ship bottom vertical parallel plate (9Q) Method. 横型全動翼水重力タービン(8B)タービン翼(8b)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、両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単空気噴射機関(88r)等駆動簡単空気噴射機関船舶(7L)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。   Horizontal full-blade water gravity turbine (8B) Turbine blade (8b) 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 manufacturing, Both sides center support bearing combined load 0 approach + horizontal shaft bearing load 0 approach Easy air injection engine (88r), etc. Driven simple air injection engine Ship (7L) has a vertical bottom plate (9Q) wide to maximize air floating Various energy storage cycle coalescence engine and coalescence method. 横型全動翼水重力タービン(8B)タービン翼(8b)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、両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単空気噴射機関(88r)等駆動スクリュー噴射船舶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。   Horizontal full-blade water gravity turbine (8B) Turbine blade (8b) 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 manufacturing, Both sides center support bearing load coalescence 0 approach + horizontal shaft bearing load 0 approach Easy air injection engine (88r), etc. Drive screw injection ship and various bottoms vertical parallel plate (9Q) wide and various energy conservation cycles to maximize the air flying height Merger engine and merger method. 横型全動翼水重力タービン(8B)タービン翼(8b)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、両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単空気噴射機関(88r)等駆動簡単空気噴射機関船舶(7L)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。   Horizontal full-blade water gravity turbine (8B) Turbine blade (8b) 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 manufacturing, Both sides center support bearing load combined 0 approach + horizontal shaft bearing load 0 approach Simple air injection engine (88r), etc. Driven simple air injection engine Ship (7L) has wide bottom bottom vertical parallel plate (9Q) to maximize friction reduction Various energy storage cycle coalescence engine and coalescence method. 横型全動翼水重力タービン(8B)タービン翼(8b)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、両側中心支持軸受荷重合体0接近+横軸軸受荷重0接近簡単空気噴射機関(88r)等駆動スクリュー噴射船舶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。   Horizontal full-blade water gravity turbine (8B) Turbine blade (8b) 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 manufacturing, Both sides center support bearing combined load 0 approach + horizontal shaft bearing load 0 approach Easy air injection engine (88r), etc. Drive screw injection ship, bottom vertical parallel plate (9Q) wide and various energy conservation cycles to maximize friction reduction Merger engine and merger method. 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする理論燃焼室(4Q)複数超高圧燃料燃焼噴射推進+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単噴射機関(88s)回転翼噴射飛行機(7O)にする各種エネルギ保存サイクル合体機関及び合体方法。   Horizontal all-blade hydrogravity turbine (8B) Turbine blade (8b) Theoretical combustion chamber (4Q) multiple ultra-high pressure that receives liquid oxygen (5K) and produces compressed volume 21/60000 of power generation electricity production Fuel combustion injection propulsion + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + horizontal shaft bearing load 0 approaching counter-rotating production compressed air (28a) combustion simple injection Various energy storage cycle coalescence engine and coalescence method for engine (88s) rotor blade jet airplane (70). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気を受給して、理論燃焼室(4Q)複数超高圧燃料燃焼噴射推進+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単噴射機関(88s)回転翼噴射飛行機(7O)にする各種エネルギ保存サイクル合体機関及び合体方法。   Horizontal full-blade hydrogravity turbine (8B) turbine blade (8b) receiving liquid oxygen (5K) + electricity from the generation of electricity, theoretical combustion chamber (4Q) multiple ultra high pressure fuel combustion injection propulsion + inner compression blade ( 8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion simple injection engine (88s) Rotary blade injection airplane ( 7O) Various energy storage cycle coalescence engines and coalescence methods. 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気+高温水を受給して、理論燃焼室(4Q)複数超高圧燃料燃焼噴射推進+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単噴射機関(88s)回転翼噴射飛行機(7O)にする各種エネルギ保存サイクル合体機関及び合体方法。   Horizontal full blade water gravity turbine (8B) Turbine blade (8b) Power generation electric manufacturing, receiving liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) multiple ultra high pressure fuel combustion injection propulsion + inside Compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion simple injection engine (88s) rotor blade Various energy storage cycle coalescing engine and coalescence method for jet airplane (7O). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、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+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単噴射機関(88s)回転翼噴射飛行機(7O)に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 combustion blade (8B) turbine blade (8b) theoretical combustion chamber (4Q) air suction flow that receives liquid oxygen (5K) and produces a compression volume of 21/60000 of air compression, produced by power generation electricity production Plural super high pressure fuel combustion injection propulsion including road + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + horizontal axis bearing load 0 approaching counter-rotating manufactured compressed air (28a) ) Various energy storage cycle coalescing engine and coalescence method for making a simple injection engine (88s) rotary blade injection airplane (70) as a combustion. 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気を受給して、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+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単噴射機関(88s)回転翼噴射飛行機(7O)にする各種エネルギ保存サイクル合体機関及び合体方法。   Horizontal full blade hydrogravity turbine (8B) Turbine blade (8b) Multi-high pressure fuel combustion injection that receives liquid oxygen (5K) + electricity and includes a theoretical combustion chamber (4Q) air suction channel Propulsion + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter rotating manufactured compressed air (28a) Combustion simple injection engine (88s ) Various energy storage cycle coalescing engines and coalescence methods for rotating blade jet airplanes (7O). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気+高温水を受給して、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+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単噴射機関(88s)回転翼噴射飛行機(7O)にする各種エネルギ保存サイクル合体機関及び合体方法。   Horizontal all-blade water gravity turbine (8B) Turbine blade (8b) Multiple ultra-high pressures that receive liquid oxygen (5K) + electricity + high-temperature water, and have a theoretical combustion chamber (4Q) air suction channel Fuel combustion injection propulsion + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + horizontal shaft bearing load 0 approaching counter-rotating production compressed air (28a) combustion simple injection Various energy storage cycle coalescence engine and coalescence method for engine (88s) rotor blade jet airplane (70). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、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+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単噴射機関(88s)回転翼噴射飛行機(7O)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。   A horizontal combustion blade (8B) turbine blade (8b) theoretical combustion chamber (4Q) air suction flow that receives liquid oxygen (5K) and produces a compression volume of 21/60000 of air compression, produced by power generation electricity production Plural super high pressure fuel combustion injection propulsion including road + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + horizontal axis bearing load 0 approaching counter-rotating manufactured compressed air (28a) ) Various energy storage cycle coalescing engines and coalescence methods driven by combustion simple injection engine (88s) rotor bladed airplane (70). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気を受給して、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+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単噴射機関(88s)回転翼噴射飛行機(7O)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。   Horizontal full blade hydrogravity turbine (8B) Turbine blade (8b) Multi-high pressure fuel combustion injection that receives liquid oxygen (5K) + electricity and includes a theoretical combustion chamber (4Q) air suction channel Propulsion + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter rotating manufactured compressed air (28a) Combustion simple injection engine (88s ) Various energy storage cycle coalescing engine and coalescence method for driving a rotary wing jet airplane (70). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気+高温水を受給して、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+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単噴射機関(88s)回転翼噴射飛行機(7O)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。   Horizontal all-blade water gravity turbine (8B) Turbine blade (8b) Multiple ultra-high pressures that receive liquid oxygen (5K) + electricity + high-temperature water, and have a theoretical combustion chamber (4Q) air suction channel Fuel combustion injection propulsion + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + horizontal shaft bearing load 0 approaching counter-rotating production compressed air (28a) combustion simple injection Engine (88s) Rotary blade jet airplane (70) Various energy storage cycle coalescing engine and coalescence method. 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする理論燃焼室(4Q)複数+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単噴射機関(88s)回転翼噴射飛行機(7O)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。   Horizontal all-blade hydrogravity turbine (8B) Turbine blade (8b) Theoretical combustion chamber (4Q) + inner side that receives liquid oxygen (5K) and produces compression volume 21/60000 of power generation electricity production Compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion simple injection engine (88s) rotor blade Various energy storage cycle coalescence engine and coalescence method for driving an injection plane (70). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)駆動して回転翼飛行機(7N)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。   Theoretical combustion chamber (4Q) ultra high pressure fuel that receives liquid oxygen (5K) and produces a compression volume of 21/60000 of air compression from horizontal full-blade water gravity turbine (8B) turbine blade (8b) generator Combustion + Inner compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Simple gas engine (88q) as combustion Various energy storage cycle coalescence engine and coalescence method for driving and driving a rotary wing airplane (7N). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気を受給して、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)駆動して回転翼飛行機(7N)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。   Horizontal full blade hydrogravity turbine (8B) Turbine blade (8b) Power generation electricity production, liquid oxygen (5K) + electricity received, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compression blade (8q) outside Compressed wing (8r) Inner output wing (8s) Outer output wing (8t) + Horizontal axis bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion driven by simple gas engine (88q) and rotary wing airplane (7N) Various energy storage cycle coalescence engines and coalescence methods to be driven. 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気+高温水を受給して、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)駆動して回転翼飛行機(7N)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。   Horizontal full-blade water gravity turbine (8B) Turbine blade (8b) Received liquid oxygen (5K) + electricity + high-temperature water from power generation electricity production, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compression blade ( 8q) Outer compression wing (8r) Inner output wing (8s) Outer output wing (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) As a combustion, a simple gas engine (88q) is driven and a rotorcraft (7N) Various energy storage cycle coalescence engines and coalescence methods to be driven. 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動して回転翼飛行機(7N)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。   Theoretical combustion chamber (4Q) ultra high pressure fuel that receives liquid oxygen (5K) and produces a compression volume of 21/60000 of air compression from horizontal full-blade water gravity turbine (8B) turbine blade (8b) generator Combustion + Inner compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Simple gas engine (88q) as combustion Various energy storage cycle coalescing engine and coalescence method for driving one or more to drive a rotary wing airplane (7N). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気を受給して、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動して回転翼飛行機(7N)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。   Horizontal full blade hydrogravity turbine (8B) Turbine blade (8b) Power generation electricity production, liquid oxygen (5K) + electricity received, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compression blade (8q) outside Compressed wing (8r) Inner output wing (8s) Outer output wing (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) As a combustion, simple gas engine (88q) 1 to multiple drives to drive a rotorcraft (7N) Various energy storage cycle coalescence engines and coalescence methods to be driven. 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気+高温水を受給して、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動して回転翼飛行機(7N)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。   Horizontal full-blade water gravity turbine (8B) Turbine blade (8b) Received liquid oxygen (5K) + electricity + high-temperature water from power generation electricity production, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compression blade ( 8q) Outer compressor blades (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion as simple gas engine (88q) 1 to multiple drives Various energy storage cycle coalescence engine and coalescence method for driving a rotary wing airplane (7N). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動して回転翼飛行機(7N)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。   Theoretical combustion chamber (4Q) ultra high pressure fuel that receives liquid oxygen (5K) and produces a compression volume of 21/60000 of air compression from horizontal full-blade water gravity turbine (8B) turbine blade (8b) generator Combustion + Inner compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Simple gas engine (88q) as combustion Various energy storage cycle coalescing engine and coalescence method for driving one or more to drive a rotary wing airplane (7N). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気を受給して、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動して回転翼飛行機(7N)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。   Horizontal full blade hydrogravity turbine (8B) Turbine blade (8b) Power generation electricity production, liquid oxygen (5K) + electricity received, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compression blade (8q) outside Compressed wing (8r) Inner output wing (8s) Outer output wing (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) As a combustion, simple gas engine (88q) 1 to multiple drives to drive a rotorcraft (7N) Various energy storage cycle coalescence engines and coalescence methods to be driven. 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気+高温水を受給して、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動して回転翼飛行機(7N)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。   Horizontal full-blade water gravity turbine (8B) Turbine blade (8b) Received liquid oxygen (5K) + electricity + high-temperature water from power generation electricity production, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compression blade ( 8q) Outer compressor blades (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion as simple gas engine (88q) 1 to multiple drives Various energy storage cycle coalescence engine and coalescence method for driving a rotary wing airplane (7N). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)駆動して回転翼飛行機(7N)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。   Theoretical combustion chamber (4Q) ultra high pressure fuel that receives liquid oxygen (5K) and produces a compression volume of 21/60000 of air compression from horizontal full-blade water gravity turbine (8B) turbine blade (8b) generator Combustion + Inner compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Simple gas engine (88q) as combustion Various energy storage cycle coalescence engine and coalescence method for driving and driving a rotary wing airplane (7N). 横型全動翼水重力タービン(R)発電電気製造の、液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)駆動回転翼(7B)回転して回転翼飛行機(7N)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。   Theoretical combustion chamber (4Q) ultra-high pressure fuel combustion + inner compression blades that receive liquid oxygen (5K) and make the compression volume 21/60000 of air compression, manufactured by horizontal full-blade water gravity turbine (R) generator (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion as simple gas engine (88q) driven rotor blade (7B ) Various energy conservation cycle coalescing engines and coalescence methods that rotate and drive a rotorcraft (7N). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気を受給して、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)駆動回転翼(7B)回転して回転翼飛行機(7N)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。   Horizontal full blade hydrogravity turbine (8B) Turbine blade (8b) Power generation electricity production, liquid oxygen (5K) + electricity received, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compression blade (8q) outside Compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion as simple gas engine (88q) driven rotor blade (7B) Various energy storage cycle coalescence engine and coalescence method for driving a rotary wing airplane (7N). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気+高温水を受給して、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)駆動回転翼(7B)回転して回転翼飛行機(7N)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。   Horizontal full-blade water gravity turbine (8B) Turbine blade (8b) Received liquid oxygen (5K) + electricity + high-temperature water from power generation electricity production, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compression blade ( 8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion as simple gas engine (88q) Drive rotor (7B) Various energy storage cycle coalescence engine and coalescence method for rotating and driving a rotorcraft (7N). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動回転翼(7B)複数回転して回転翼飛行機(7N)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。   Theoretical combustion chamber (4Q) ultra high pressure fuel that receives liquid oxygen (5K) and produces a compression volume of 21/60000 of air compression from horizontal full-blade water gravity turbine (8B) turbine blade (8b) generator Combustion + Inner compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Simple gas engine (88q) as combustion 1-multiple drive rotor (7B) various energy storage cycle coalescing engine and coalescence method for driving a rotorcraft (7N) by rotating a plurality of rotor blades (7B). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気を受給して、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動回転翼(7B)複数回転して回転翼飛行機(7N)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。   Horizontal full blade hydrogravity turbine (8B) Turbine blade (8b) Power generation electricity production, liquid oxygen (5K) + electricity received, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compression blade (8q) outside Compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) As simple combustion gas engine (88q) 1 to multiple drive rotor blades (7B) Various energy storage cycle coalescing engines and coalescence methods for driving a rotary wing airplane (7N) with multiple rotations. 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気+高温水を受給して、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動回転翼(7B)複数回転して回転翼飛行機(7N)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。   Horizontal full-blade water gravity turbine (8B) Turbine blade (8b) Received liquid oxygen (5K) + electricity + high-temperature water from power generation electricity production, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compression blade ( 8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion as simple gas engine (88q) 1 to multiple drive rotor blades (7B) Various energy storage cycle coalescence engines and coalescence methods for driving a rotary wing airplane (7N) by rotating a plurality of rotations. 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動回転翼(7B)複数回転して回転翼飛行機(7N)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。   Theoretical combustion chamber (4Q) ultra high pressure fuel that receives liquid oxygen (5K) and produces a compression volume of 21/60000 of air compression from horizontal full-blade water gravity turbine (8B) turbine blade (8b) generator Combustion + Inner compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Simple gas engine (88q) as combustion 1-multiple drive rotor (7B) various energy storage cycle coalescing engine and coalescence method for driving a rotorcraft (7N) by rotating a plurality of rotor blades (7B). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気を受給して、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動回転翼(7B)複数回転して回転翼飛行機(7N)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。   Horizontal full blade hydrogravity turbine (8B) Turbine blade (8b) Power generation electricity production, liquid oxygen (5K) + electricity received, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compression blade (8q) outside Compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) As simple combustion gas engine (88q) 1 to multiple drive rotor blades (7B) Various energy storage cycle coalescing engines and coalescence methods for driving a rotary wing airplane (7N) with multiple rotations. 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気+高温水を受給して、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動回転翼(7B)複数回転して回転翼飛行機(7N)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。   Horizontal full-blade water gravity turbine (8B) Turbine blade (8b) Received liquid oxygen (5K) + electricity + high-temperature water from power generation electricity production, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compression blade ( 8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion as simple gas engine (88q) 1 to multiple drive rotor blades (7B) Various energy storage cycle coalescence engines and coalescence methods for driving a rotary wing airplane (7N) by rotating a plurality of rotations. 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)駆動回転翼(7B)回転して回転翼飛行機(7N)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。   Theoretical combustion chamber (4Q) ultra high pressure fuel that receives liquid oxygen (5K) and produces a compression volume of 21/60000 of air compression from horizontal full-blade water gravity turbine (8B) turbine blade (8b) generator Combustion + Inner compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Simple gas engine (88q) as combustion Various energy storage cycle coalescing engines and coalescence methods for driving a rotor blade (7N) by rotating a driving rotor blade (7B). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)駆動簡単噴射機関(88s)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。   Theoretical combustion chamber (4Q) ultra high pressure fuel that receives liquid oxygen (5K) and produces a compression volume of 21/60000 of air compression from horizontal full-blade water gravity turbine (8B) turbine blade (8b) generator Combustion + Inner compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Simple gas engine (88q) as combustion Various energy storage cycle coalescence engine and coalescence method for driving simple injection engine (88s). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気を受給して、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)駆動簡単噴射機関(88s)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。   Horizontal full blade hydrogravity turbine (8B) Turbine blade (8b) Power generation electricity production, liquid oxygen (5K) + electricity received, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compression blade (8q) outside Compressed wing (8r) Inner output wing (8s) Outer output wing (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) combustion as simple gas engine (88q) drive Simple injection engine (88s) drive Various energy storage cycle coalescence engines and coalescence methods. 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気+高温水を受給して、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)駆動簡単噴射機関(88s)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。   Horizontal full-blade water gravity turbine (8B) Turbine blade (8b) Received liquid oxygen (5K) + electricity + high-temperature water from power generation electricity production, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compression blade ( 8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion as simple gas engine (88q) driven simple injection engine (88s) ) Various energy storage cycle coalescence engines and coalescence methods to be driven. 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動簡単噴射機関(88s)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。   Theoretical combustion chamber (4Q) ultra high pressure fuel that receives liquid oxygen (5K) and produces a compression volume of 21/60000 of air compression from horizontal full-blade water gravity turbine (8B) turbine blade (8b) generator Combustion + Inner compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Simple gas engine (88q) as combustion Various energy storage cycle coalescing engine and coalescence method for driving one or more drive simple injection engines (88s). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気を受給して、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動簡単噴射機関(88s)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。   Horizontal full blade hydrogravity turbine (8B) Turbine blade (8b) Power generation electricity production, liquid oxygen (5K) + electricity received, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compression blade (8q) outside Compressed blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion as simple gas engine (88q) 1 to multiple drive simple injection engine (88s) ) Various energy storage cycle coalescence engines and coalescence methods to be driven. 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気+高温水を受給して、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動簡単噴射機関(88s)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。   Horizontal full-blade water gravity turbine (8B) Turbine blade (8b) Received liquid oxygen (5K) + electricity + high-temperature water from power generation electricity production, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compression blade ( 8q) Outer compression blades (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion as simple gas engine (88q) 1 to multiple drive simple injection Various energy storage cycle coalescence engine and coalescence method for driving the engine (88s). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動簡単噴射機関(88s)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。   Theoretical combustion chamber (4Q) ultra high pressure fuel that receives liquid oxygen (5K) and produces a compression volume of 21/60000 of air compression from horizontal full-blade water gravity turbine (8B) turbine blade (8b) generator Combustion + Inner compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Simple gas engine (88q) as combustion Various energy storage cycle coalescing engine and coalescence method for driving one or more drive simple injection engines (88s). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気を受給して、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動簡単噴射機関(88s)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。   Horizontal full blade hydrogravity turbine (8B) Turbine blade (8b) Power generation electricity production, liquid oxygen (5K) + electricity received, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compression blade (8q) outside Compressed blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion as simple gas engine (88q) 1 to multiple drive simple injection engine (88s) ) Various energy storage cycle coalescence engines and coalescence methods to be driven. 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気+高温水を受給して、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動簡単噴射機関(88s)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。   Horizontal full-blade water gravity turbine (8B) Turbine blade (8b) Received liquid oxygen (5K) + electricity + high-temperature water from power generation electricity production, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compression blade ( 8q) Outer compression blades (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion as simple gas engine (88q) 1 to multiple drive simple injection Various energy storage cycle coalescence engine and coalescence method for driving the engine (88s). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)駆動簡単噴射機関(88s)複数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。   Theoretical combustion chamber (4Q) ultra high pressure fuel that receives liquid oxygen (5K) and produces a compression volume of 21/60000 of air compression from horizontal full-blade water gravity turbine (8B) turbine blade (8b) generator Combustion + Inner compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Simple gas engine (88q) as combustion Drive simple injection engine (88s) Various energy storage cycle coalescence engine and coalescence method for driving a plurality of energy storage cycles. 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする理論燃焼室(4Q)複数超高圧燃料燃焼噴射推進+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単噴射機関(88s)特大オスプレイ(7P)にする各種エネルギ保存サイクル合体機関及び合体方法。   Horizontal all-blade hydrogravity turbine (8B) Turbine blade (8b) Theoretical combustion chamber (4Q) multiple ultra-high pressure that receives liquid oxygen (5K) and produces compressed volume 21/60000 of power generation electricity production Fuel combustion injection propulsion + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + horizontal shaft bearing load 0 approaching counter-rotating production compressed air (28a) combustion simple injection Various energy storage cycle coalescing engine and coalescence method for engine (88s) extra large Osprey (7P). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気を受給して、理論燃焼室(4Q)複数超高圧燃料燃焼噴射推進+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単噴射機関(88s)特大オスプレイ(7P)にする各種エネルギ保存サイクル合体機関及び合体方法。   Horizontal full-blade hydrogravity turbine (8B) turbine blade (8b) receiving liquid oxygen (5K) + electricity from the generation of electricity, theoretical combustion chamber (4Q) multiple ultra high pressure fuel combustion injection propulsion + inner compression blade ( 8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion simple injection engine (88s) Extra large Osprey (7P) Various energy storage cycle coalescence engines and coalescence methods. 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気+高温水を受給して、理論燃焼室(4Q)複数超高圧燃料燃焼噴射推進+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単噴射機関(88s)特大オスプレイ(7P)にする各種エネルギ保存サイクル合体機関及び合体方法。   Horizontal full blade water gravity turbine (8B) Turbine blade (8b) Power generation electric manufacturing, receiving liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) multiple ultra high pressure fuel combustion injection propulsion + inside Compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion simple injection engine (88s) Oversized osprey (7P) Various energy storage cycle coalescence engines and coalescence methods. 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、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+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単噴射機関(88s)特大オスプレイ(7P)に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 combustion blade (8B) turbine blade (8b) theoretical combustion chamber (4Q) air suction flow that receives liquid oxygen (5K) and produces a compression volume of 21/60000 of air compression, produced by power generation electricity production Plural super high pressure fuel combustion injection propulsion including road + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + horizontal axis bearing load 0 approaching counter-rotating manufactured compressed air (28a) ) Various energy storage cycle coalescence engine and coalescence method to make a simple injection engine (88s) oversized Osprey (7P) as a combustion. 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気を受給して、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+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単噴射機関(88s)特大オスプレイ(7P)にする各種エネルギ保存サイクル合体機関及び合体方法。   Horizontal full blade hydrogravity turbine (8B) Turbine blade (8b) Multi-high pressure fuel combustion injection that receives liquid oxygen (5K) + electricity and includes a theoretical combustion chamber (4Q) air suction channel Propulsion + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter rotating manufactured compressed air (28a) Combustion simple injection engine (88s ) Various energy conservation cycle coalescence engine and coalescence method to make oversized Osprey (7P). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気+高温水を受給して、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+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単噴射機関(88s)特大オスプレイ(7P)にする各種エネルギ保存サイクル合体機関及び合体方法。   Horizontal all-blade water gravity turbine (8B) Turbine blade (8b) Multiple ultra-high pressures that receive liquid oxygen (5K) + electricity + high-temperature water, and have a theoretical combustion chamber (4Q) air suction channel Fuel combustion injection propulsion + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + horizontal shaft bearing load 0 approaching counter-rotating production compressed air (28a) combustion simple injection Various energy storage cycle coalescing engine and coalescence method for engine (88s) extra large Osprey (7P). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、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+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単噴射機関(88s)特大オスプレイ(7P)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。   A horizontal combustion blade (8B) turbine blade (8b) theoretical combustion chamber (4Q) air suction flow that receives liquid oxygen (5K) and produces a compression volume of 21/60000 of air compression, produced by power generation electricity production Plural super high pressure fuel combustion injection propulsion including road + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + horizontal axis bearing load 0 approaching counter-rotating manufactured compressed air (28a) ) Various energy storage cycle coalescence engine and coalescence method driven by combustion simple injection engine (88s) extra large Osprey (7P). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気を受給して、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+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単噴射機関(88s)特大オスプレイ(7P)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。   Horizontal full blade hydrogravity turbine (8B) Turbine blade (8b) Multi-high pressure fuel combustion injection that receives liquid oxygen (5K) + electricity and includes a theoretical combustion chamber (4Q) air suction channel Propulsion + Inner compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter rotating manufactured compressed air (28a) Combustion simple injection engine (88s ) Various energy storage cycle coalescence engine and coalescence method driven by extra large Osprey (7P). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気+高温水を受給して、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+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単噴射機関(88s)特大オスプレイ(7P)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。   Horizontal all-blade water gravity turbine (8B) Turbine blade (8b) Multiple ultra-high pressures that receive liquid oxygen (5K) + electricity + high-temperature water, and have a theoretical combustion chamber (4Q) air suction channel Fuel combustion injection propulsion + inner compression blade (8q) outer compression blade (8r) inner output blade (8s) outer output blade (8t) + horizontal shaft bearing load 0 approaching counter-rotating production compressed air (28a) combustion simple injection Engine (88s) Extra large Osprey (7P) driven various energy storage cycle coalescing engine and coalescence method. 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする理論燃焼室(4Q)複数+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼とした簡単噴射機関(88s)特大オスプレイ(7P)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。   Horizontal all-blade hydrogravity turbine (8B) Turbine blade (8b) Theoretical combustion chamber (4Q) + inner side that receives liquid oxygen (5K) and produces compression volume 21/60000 of power generation electricity production Compressor blade (8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion simple injection engine (88s) Oversized osprey (7P) Various energy storage cycle coalescence engines and coalescence methods to be driven. 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)大型オスプレイ(7Q)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。   Theoretical combustion chamber (4Q) ultra high pressure fuel that receives liquid oxygen (5K) and produces a compression volume of 21/60000 of air compression from horizontal full-blade water gravity turbine (8B) turbine blade (8b) generator Combustion + Inner compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Simple gas engine (88q) as combustion Various energy storage cycle coalescence engine and coalescence method for driving large Osprey (7Q). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気を受給して、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)大型オスプレイ(7Q)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。   Horizontal full blade hydrogravity turbine (8B) Turbine blade (8b) Power generation electricity production, liquid oxygen (5K) + electricity received, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compression blade (8q) outside Compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion Simple gas engine (88q) Large osprey (7Q) Storage cycle coalescence engine and coalescence method. 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気+高温水を受給して、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)大型オスプレイ(7Q)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。   Horizontal full-blade water gravity turbine (8B) Turbine blade (8b) Received liquid oxygen (5K) + electricity + high-temperature water from power generation electricity production, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compression blade ( 8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion as simple gas engine (88q) Large Osprey (7Q) drive Various energy storage cycle coalescence engine and coalescence method. 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動して大型オスプレイ(7Q)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。   Theoretical combustion chamber (4Q) ultra high pressure fuel that receives liquid oxygen (5K) and produces a compression volume of 21/60000 of air compression from horizontal full-blade water gravity turbine (8B) turbine blade (8b) generator Combustion + Inner compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Simple gas engine (88q) as combustion Various energy storage cycle coalescence engine and coalescence method for driving one or more and driving a large Osprey (7Q). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気を受給して、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動して大型オスプレイ(7Q)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。   Horizontal full blade hydrogravity turbine (8B) Turbine blade (8b) Power generation electricity production, liquid oxygen (5K) + electricity received, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compression blade (8q) outside Compressed wing (8r) Inner output wing (8s) Outer output wing (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) As a combustion, simple gas engine (88q) 1 to multiple drive to large osprey ( 7Q) Various energy storage cycle coalescence engines and coalescence methods to be driven. 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気+高温水を受給して、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動して大型オスプレイ(7Q)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。   Horizontal full-blade water gravity turbine (8B) Turbine blade (8b) Received liquid oxygen (5K) + electricity + high-temperature water from power generation electricity production, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compression blade ( 8q) Outer compressor blades (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion as simple gas engine (88q) 1 to multiple drives Various energy storage cycle coalescence engine and coalescence method for driving large Osprey (7Q). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動して大型オスプレイ(7Q)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。   Theoretical combustion chamber (4Q) ultra high pressure fuel that receives liquid oxygen (5K) and produces a compression volume of 21/60000 of air compression from horizontal full-blade water gravity turbine (8B) turbine blade (8b) generator Combustion + Inner compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Simple gas engine (88q) as combustion Various energy storage cycle coalescence engine and coalescence method for driving one or more and driving a large Osprey (7Q). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気を受給して、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動して大型オスプレイ(7Q)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。   Horizontal full blade hydrogravity turbine (8B) Turbine blade (8b) Power generation electricity production, liquid oxygen (5K) + electricity received, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compression blade (8q) outside Compressed wing (8r) Inner output wing (8s) Outer output wing (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) As a combustion, simple gas engine (88q) 1 to multiple drive to large osprey ( 7Q) Various energy storage cycle coalescence engines and coalescence methods to be driven. 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気+高温水を受給して、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動して大型オスプレイ(7Q)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。   Horizontal full-blade water gravity turbine (8B) Turbine blade (8b) Received liquid oxygen (5K) + electricity + high-temperature water from power generation electricity production, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compression blade ( 8q) Outer compressor blades (8r) Inner output blades (8s) Outer output blades (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion as simple gas engine (88q) 1 to multiple drives Various energy storage cycle coalescence engine and coalescence method for driving large Osprey (7Q). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)駆動して大型オスプレイ(7Q)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。   Theoretical combustion chamber (4Q) ultra high pressure fuel that receives liquid oxygen (5K) and produces a compression volume of 21/60000 of air compression from horizontal full-blade water gravity turbine (8B) turbine blade (8b) generator Combustion + Inner compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Simple gas engine (88q) as combustion Various energy storage cycle coalescence engine and coalescence method for driving and driving a large Osprey (7Q). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)駆動プロペラ(7A)回転して大型オスプレイ(7Q)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。   Theoretical combustion chamber (4Q) ultra high pressure fuel that receives liquid oxygen (5K) and produces a compression volume of 21/60000 of air compression from horizontal full-blade water gravity turbine (8B) turbine blade (8b) generator Combustion + Inner compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Simple gas engine (88q) as combustion Various energy storage cycle coalescence engine and coalescence method for driving propeller (7A) to rotate to drive large osprey (7Q). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気を受給して、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)駆動プロペラ(7A)回転して大型オスプレイ(7Q)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。   Horizontal full blade hydrogravity turbine (8B) Turbine blade (8b) Power generation electricity production, liquid oxygen (5K) + electricity received, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compression blade (8q) outside Compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion as simple gas engine (88q) drive propeller (7A) Various energy storage cycle coalescence engine and coalescence method driven by Osprey (7Q). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気+高温水を受給して、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)駆動プロペラ(7A)回転して大型オスプレイ(7Q)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。   Horizontal full-blade water gravity turbine (8B) Turbine blade (8b) Received liquid oxygen (5K) + electricity + high-temperature water from power generation electricity production, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compression blade ( 8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion as simple gas engine (88q) drive propeller (7A) rotation Various energy storage cycle coalescence engines and coalescence methods for driving large Osprey (7Q). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動プロペラ(7A)複数回転して大型オスプレイ(7Q)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。   Theoretical combustion chamber (4Q) ultra high pressure fuel that receives liquid oxygen (5K) and produces a compression volume of 21/60000 of air compression from horizontal full-blade water gravity turbine (8B) turbine blade (8b) generator Combustion + Inner compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Simple gas engine (88q) as combustion 1-multiple drive propeller (7A) various energy storage cycle coalescing engine and coalescence method for driving large osprey (7Q) by multiple rotations. 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気を受給して、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動プロペラ(7A)複数回転して大型オスプレイ(7Q)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。   Horizontal full blade hydrogravity turbine (8B) Turbine blade (8b) Power generation electricity production, liquid oxygen (5K) + electricity received, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compression blade (8q) outside Compressed blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion as simple gas engine (88q) 1-multiple drive propellers (7A) Various energy storage cycle coalescence engines and coalescence methods that rotate and drive large Osprey (7Q). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気+高温水を受給して、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動プロペラ(7A)複数回転して大型オスプレイ(7Q)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。   Horizontal full-blade water gravity turbine (8B) Turbine blade (8b) Received liquid oxygen (5K) + electricity + high-temperature water from power generation electricity production, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compression blade ( 8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion as simple gas engine (88q) 1 to multiple drive propellers ( 7A) Various energy storage cycle coalescence engines and coalescence methods that rotate a plurality of times to drive a large Osprey (7Q). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動プロペラ(7A)複数回転して大型オスプレイ(7Q)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。   Theoretical combustion chamber (4Q) ultra high pressure fuel that receives liquid oxygen (5K) and produces a compression volume of 21/60000 of air compression from horizontal full-blade water gravity turbine (8B) turbine blade (8b) generator Combustion + Inner compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Simple gas engine (88q) as combustion 1-multiple drive propeller (7A) various energy storage cycle coalescing engine and coalescence method for driving large osprey (7Q) by multiple rotations. 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気を受給して、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動プロペラ(7A)複数回転して大型オスプレイ(7Q)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。   Horizontal full blade hydrogravity turbine (8B) Turbine blade (8b) Power generation electricity production, liquid oxygen (5K) + electricity received, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compression blade (8q) outside Compressed blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion as simple gas engine (88q) 1-multiple drive propellers (7A) Various energy storage cycle coalescence engines and coalescence methods that rotate and drive large Osprey (7Q). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気+高温水を受給して、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動プロペラ(7A)複数回転して大型オスプレイ(7Q)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。   Horizontal full-blade water gravity turbine (8B) Turbine blade (8b) Received liquid oxygen (5K) + electricity + high-temperature water from power generation electricity production, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compression blade ( 8q) Outer compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion as simple gas engine (88q) 1 to multiple drive propellers ( 7A) Various energy storage cycle coalescence engines and coalescence methods that rotate a plurality of times to drive a large Osprey (7Q). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)駆動プロペラ(7A)回転して大型オスプレイ(7Q)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。   Theoretical combustion chamber (4Q) ultra high pressure fuel that receives liquid oxygen (5K) and produces a compression volume of 21/60000 of air compression from horizontal full-blade water gravity turbine (8B) turbine blade (8b) generator Combustion + Inner compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Simple gas engine (88q) as combustion Various energy storage cycle coalescence engine and coalescence method for driving propeller (7A) to rotate to drive large osprey (7Q). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)駆動簡単噴射機関(88s)特大オスプレイ(7P)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。   Theoretical combustion chamber (4Q) ultra high pressure fuel that receives liquid oxygen (5K) and produces a compression volume of 21/60000 of air compression from horizontal full-blade water gravity turbine (8B) turbine blade (8b) generator Combustion + Inner compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Simple gas engine (88q) as combustion Various energy storage cycle coalescence engine and coalescence method for driving simple injection engine (88s) extra large Osprey (7P). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気を受給して、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)駆動簡単噴射機関(88s)特大オスプレイ(7P)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。   Horizontal full blade hydrogravity turbine (8B) Turbine blade (8b) Power generation electricity production, liquid oxygen (5K) + electricity received, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compression blade (8q) outside Compressor blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion as simple gas engine (88q) Driven simple injection engine (88s) oversized osprey (7P) Various energy storage cycle coalescence engines and coalescence methods to be driven. 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気+高温水を受給して、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)駆動簡単噴射機関(88s)特大オスプレイ(7P)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。   Horizontal full-blade water gravity turbine (8B) Turbine blade (8b) Received liquid oxygen (5K) + electricity + high-temperature water from power generation electricity production, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compression blade ( 8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion as simple gas engine (88q) driven simple injection engine (88s) ) Various energy storage cycle coalescence engine and coalescence method driven by extra large Osprey (7P). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動1〜複数簡単噴射機関(88s)特大オスプレイ(7P)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。   Theoretical combustion chamber (4Q) ultra high pressure fuel that receives liquid oxygen (5K) and produces a compression volume of 21/60000 of air compression from horizontal full-blade water gravity turbine (8B) turbine blade (8b) generator Combustion + Inner compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Simple gas engine (88q) as combustion 1-multiple drive 1-multiple simple injection engine (88s) extra large osprey (7P) drive various energy storage cycle coalescing engine and coalescing method. 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気を受給して、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動1〜複数簡単噴射機関(88s)特大オスプレイ(7P)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。   Horizontal full blade hydrogravity turbine (8B) Turbine blade (8b) Power generation electricity production, liquid oxygen (5K) + electricity received, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compression blade (8q) outside Compressed wing (8r) Inner output wing (8s) Outer output wing (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) as simple gas engine (88q) 1-multiple drive 1-multiple simple injection Engine (88s) Extra large Osprey (7P) driven various energy storage cycle coalescing engine and coalescence method. 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気+高温水を受給して、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動1〜複数簡単噴射機関(88s)特大オスプレイ(7P)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。   Horizontal full-blade water gravity turbine (8B) Turbine blade (8b) Received liquid oxygen (5K) + electricity + high-temperature water from power generation electricity production, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compression blade ( 8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion as simple gas engine (88q) 1-multiple drive 1- Various energy storage cycle coalescence engine and coalescence method for driving multiple simple injection engines (88s) extra large Osprey (7P). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動1〜複数簡単噴射機関(88s)特大オスプレイ(7P)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。   Theoretical combustion chamber (4Q) ultra high pressure fuel that receives liquid oxygen (5K) and produces a compression volume of 21/60000 of air compression from horizontal full-blade water gravity turbine (8B) turbine blade (8b) generator Combustion + Inner compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Simple gas engine (88q) as combustion 1-multiple drive 1-multiple simple injection engine (88s) extra large osprey (7P) drive various energy storage cycle coalescing engine and coalescing method. 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気を受給して、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動1〜複数簡単噴射機関(88s)特大オスプレイ(7P)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。   Horizontal full blade hydrogravity turbine (8B) Turbine blade (8b) Power generation electricity production, liquid oxygen (5K) + electricity received, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compression blade (8q) outside Compressed wing (8r) Inner output wing (8s) Outer output wing (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) as simple gas engine (88q) 1-multiple drive 1-multiple simple injection Engine (88s) Extra large Osprey (7P) driven various energy storage cycle coalescing engine and coalescence method. 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)+電気+高温水を受給して、理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)1〜複数駆動1〜複数簡単噴射機関(88s)特大オスプレイ(7P)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。   Horizontal full-blade water gravity turbine (8B) Turbine blade (8b) Received liquid oxygen (5K) + electricity + high-temperature water from power generation electricity production, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + inner compression blade ( 8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion as simple gas engine (88q) 1-multiple drive 1- Various energy storage cycle coalescence engine and coalescence method for driving multiple simple injection engines (88s) extra large Osprey (7P). 横型全動翼水重力タービン(8B)タービン翼(8b)発電電気製造の、液体酸素(5K)を受給して、圧縮容積を空気圧縮の21/60000にする理論燃焼室(4Q)超高圧燃料燃焼+内側圧縮翼(8q)外側圧縮翼(8r)内側出力翼(8s)外側出力翼(8t)+横軸軸受荷重0接近二重反転製造圧縮空気(28a)燃焼として簡単ガス機関(88q)駆動簡単噴射機関(88s)複数特大オスプレイ(7P)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。   Theoretical combustion chamber (4Q) ultra high pressure fuel that receives liquid oxygen (5K) and produces a compression volume of 21/60000 of air compression from horizontal full-blade water gravity turbine (8B) turbine blade (8b) generator Combustion + Inner compression blade (8q) Outer compression blade (8r) Inner output blade (8s) Outer output blade (8t) + Horizontal shaft bearing load 0 approaching counter-rotating production Compressed air (28a) Simple gas engine (88q) as combustion Various energy storage cycle coalescence engine and coalescence method for driving simple injection engine (88s) and multiple extra large Osprey (7P).
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