JP2014074375A - Various energy storing cycle integrated mechanism - Google Patents

Abstract

PROBLEM TO BE SOLVED: To provide a various energy storing cycle integrated mechanism in which an existing steam turbine power generation has stator vane of zero output in half 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 blades are doubly inverted by a lateral shaft 1h gear to realize, for example, mercury gravity acceleration power generation in 30 mmHg vacuum in order to achieve Mach 30, and 100 units of mercury injection turbines are combined to achieve 1355 times the existing power generation amount per unit power generation amount. 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

The liquid jet velocity + gravity acceleration in vacuum drives the Mach 30 mercury, and the horizontal full-blade ratio critical material gravity turbine 8U power generation aiming at super-high-speed circumferential speed uses the repulsive permanent magnet 9B + the attracting permanent magnet 9C to approach the bearing load 0+ Ultra high speed peripheral speed, opposed synchronous gear 4c and series co-rotating gear 4d make counter synchronous rotation and series co-rotation ultra-high-speed rotation large output, increase the degree of vacuum of renewable energy that is the largest unused in the earth for existing pumped storage power generation Gravity acceleration in the middle + Mach 3 or more high speed injection addition + Turbine number unlimited head drop unlimited addition, for example, mercury injection aiming at Mach 28 etc., vacuum gravity acceleration in vacuum, one unit with 100 sets of turbines to head 500 to 828m etc. Existing pumped storage power generation As a power generation that requires 0 times the fuel cost of boilers and nuclear reactors to be eliminated, the horizontal all-blade ratio critical material gravity turbine 8U power generation electric drive and electric Simple multi-stage compressor 3h + liquid oxygen production machine 88l, simple gas engine 88m, simple water injection engine 88n, simple injection engine 88o, etc. Various heat production such as heat recovery liquid oxygen by making the air heated by the solar heater 21 into a compressed high temperature, and divided and stored in 24-200 MPa superheated steam 50 warm heat + liquid air 28a cold heat, electricity + liquid air cold heat + high temperature water 52a ~ As superheated steam 50 temperature supply equipment 3D, various heat use + liquid use infinite use correspondence and ship, vehicle and airplane drive, for example, ship, vehicle and airplane receive liquid oxygen, and compressive volume work rate is Air compression is 21/60000 volumetric power, and the compression pressure of liquid oxygen or water is easy to be 20 times. Easy driving of simple gas engine 88m, simple injection engine 88o, etc. Water injection engine 88n combined injection propulsion, ship combined injection promotion speeding up natural phenomena 2a Supply nitrogen, oxygen and CO2 to seawater Increase microorganisms and seaweeds, greatly increase human food such as fish in the food chain, etc. In the case of airplane and automobile driving, CO2 exhaust 1/10, fuel cost 1/10 and 1 / 500,000 costs are aimed at reaching the space, airplanes and ships are aimed at 10 times speed, various energy conservation cycle coalescence engines and various energy conservation coalescence techniques About.

  The world's largest automobile driven reciprocating engine consumes enormous amount of fuel by compressing air. Horizontal type moving blade specific material gravity turbine 8U vacuum specific material gravity acceleration power generation of electricity + liquid air cold heat + hot water 52a ~ Superheated steam 50Supply from thermal supply facility 3D, superheated steam is injected into methane hydrate under permafrost and underwater, split into methane and water, methane is recovered with liquid nitrogen cooled liquid methane, liquid air is liquid oxygen chamber 5K Is received with 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, and it is set to 24-200 MPa ultrahigh pressure compression injection, liquid oxygen 5K + liquid fuel 1b + high temperature water 52a. Is heated at the inner periphery of the compression theoretical combustion chamber 4Q to an ultra-high pressure, heated to an ultra-high temperature or optimum temperature, and supplied and injected into the theoretical combustion chamber 4Q, respectively. Then, the high temperature water 52a of the high pressure and high temperature water heating pipe 5H is heated to superheated steam 50 by super high pressure oxygen + super high pressure fuel high temperature combustion, and both sides center support bearing load including easy driving of gas engine 88m etc. even with liquid oxygen 0 In the approach of union 0, super high speed double reversal research was conducted, and the combustion gas 49 was sucked and injected from the superheated steam rocket nozzle 6A as the superhigh pressure combustion gas 49 + superheated steam 50 in the theoretical combustion chamber 4Q, and a simple gas engine 88m was Drive, drive various vehicles such as automobiles and tillers, propeller 7A, rotor blade 7B and screw 7C, drive various vehicles, propeller airplane and screw ship, liquid fuel 5K for zero fuel cost electricity generation electricity production The present invention relates to technologies for various energy storage cycle coalescence engines and coalescence methods that aim to achieve a fuel cost of 1/10 or 10 times the speed of use, and the world's best operating profit rate.

  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 of liquid compression simple injection engine 88o combined with space rocket and jet, horizontal full blade ratio material gravity turbine 8U power generation electric drive many simple multistage compressor 3h heat pump 1G + solar heater 21 heat By manufacturing, it is divided and stored in high-temperature water of 24-200 MPa to superheated steam temperature 50 + liquid air cold heat 28a, and as an electric + liquid air cold heat + high temperature water 52a to superheated steam 50 heat supply equipment 3D, the jet injection propulsion is liquid oxygen 5K + Received by liquid fuel 1c + high-pressure high-temperature water 52a, compressed high-pressure compressed by liquid oxygen compression to 21/60000 volumetric power of air compression, The fuel heating pipe 1L high-pressure high-temperature water heating pipe 5H oxygen heating pipe 5F, such as not shown in the simple injection engine 88o theoretical combustion chamber 4Q inner peripheral view, etc., to the optimum heating temperature, fuel control valve 25b + oxygen control valve 24D + overheating not shown The steam control valve 25 is opened, and each of them is injected and burned into an inlet / outlet on / off valve 1Q closed theoretical combustion chamber 4Q aiming at one or more stoichiometric air-fuel ratio ultra-high pressure combustion, and superheated steam as oxygen injection nozzle 6L fuel injection nozzle 6X multiple combustion At 50, heat recovery superheated steam rocket nozzle 6A injection + combustion gas injection nozzle 6Y injection, aiming for combined injection of rocket injection or jet injection, super high-speed linear counter-rotating compressed air 28a + combustion at close to both side center support bearing load combination Gas 49 Ultra high speed linear injection rotation output, superheated steam rocket nozzle 6A in rocket outer box 77B + combustion gas injection nozzle 6Y 200MPa target rocket By launching a space trip cost of 1 / 500,000, it is possible to make a day trip anywhere on the earth, such as making 16 orbits of the earth a day with a space flight that is close to zero fuel cost. TECHNICAL FIELD The present invention relates to technologies for various energy conservation cycle coalescence engines and coalescence methods aiming at the best in the world.

  The existing ship consumes a large amount of fuel by air compression, reduces the rotational output and injection propulsion output, and consumes a large amount of fuel for low-speed movement. / 60000 volumetric power is included, air compressor of liquid oxygen production machine 88l is also added to use simple multi-stage compressor 3h which is simple in theory, horizontal full blade ratio critical material gravity turbine 8U power generation electric drive 1 to multi-stage simple As a heat pump 1G compression such as multi-stage compressor 3h, solar heating 21 solar heating air is compressed to high temperature, high pressure high temperature water heating tube 5H heat recovery divided and stored, 24 to 200MPa high temperature water 52a to superheat Steam 50 warm heat + liquid air 28a cold storage is divided and stored as electricity + liquid air cold heat + hot water 52a to superheated steam 50 warm heat supply equipment 3D, liquid oxygen 5K + liquid fuel 1c + hot water 52 In the receiving process, the target is pump compression of 200 MPa, and the liquid oxygen control valve 5T + liquid fuel control valve 1K + water control valve 5Q (not shown) is opened and heated to the optimum temperature in the inner periphery of the simple water injection engine 88n theoretical combustion chamber 4Q. The both sides of the center support bearings are combined in a simple water injection engine 88n and a simple gas engine 88m that are close to each other to drive the water suction injection of the simple water injection engine 88n and the screw 7C of the simple gas engine 88m. The screw propulsion simple gas engine 88m exhaust is the bottom bottom exhaust injection propulsion, aiming at 10 times the speed and 1/10 fuel cost, and natural phenomena are accelerated in the process of friction reduction injection propulsion, and oxygen, nitrogen, CO2 etc. in the sea To increase microorganism food, phytoplankton, seaweeds, corals, fish, etc. On the technology of the cycle combined institutions and coalescence method.

  Considering elementary school science without any brainwashing, the existing best steam turbine power generation at the same pressure and volumetric capacity kg weight m / sec is 1/2, 30,000 of the mercury gravity turbine 8S power, which is a significant material for the horizontal all-blade ratio. In addition, the steam speed is dammed and the zero-power stationary vane is half-damped alternately with the moving blade, the steam speed is approaching 1/100, and the total seawater temperature is 7 degrees It is rising, making the whole sea surface temperature-increasing natural phenomenon impossible, increasing abnormal weather without an upper limit, and increasing the danger of human beings approaching extinction due to heavy rains of seawater around 50 to 100 years. 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.

When the atmospheric pressure, the same speed, and the same volumetric power, kg weight m / second, are converted into a mercury-accelerated power generation in a vacuum by using 23,000 times more important material than the existing steam turbine power generation. Power generation is 230 times higher than that of the existing steam turbine power generation, but a huge power generation amount of 23,000 times power generation is expected in 100 pairs at a height of 500m or more, and further mercury gravity acceleration Mach 30 in vacuum is necessary for further experiments Infinite power generation with zero fuel cost, horizontal full blade ratio critical material mercury gravity turbine 8S power generation cylindrical turbine blade group 8A horizontal shaft plate 16 facilitates precise assembly, and includes all cylindrical turbine blade groups 8A with fixed cylindrical assembly Driven by mercury gravitational energy aiming at the Earth's largest vacuum acceleration acceleration Mach 30, aiming at easy generation and assembly, 100 times assembly of fully automatic processing and 23,000 times power generation amount Shift to expansion of low-cost electricity applications with zero fuel cost generation with mercury resources, solar heating of air with solar heater 21, 1-stage multi-stage compression of mercury gravity turbine 8S fuel cost 0 power generation electric drive Electricity + liquid air cold + high temperature water to superheated steam heat supply that is divided and stored in 24-200MPa high temperature water 52a-superheated steam temperature 50 + liquid air cold heat 28a by collecting heat multiple times with a heat pump 1G such as a machine 3h Supply from the facility 3D, receive it in the liquid oxygen chamber 5K, storage battery, etc., and make the liquid air driven car, airplane or ship a short time 1/10 fuel cost drive or 10 times speed drive, space flight or air floating ship There are backgrounds such as storage battery drive and electric drive for extremely inexpensive power generation, and prevention of global warming with little CO2 exhaust.

  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 ratio critical material gravity turbine 8U power generation is used, there is a background of low fuel cost power generation. The best fuel cost is heating. Therefore, the fuel cost 0 power generation electric drive solar heater 21 is used, and the solar heating air 28a is compressed multiple times by the fuel stage 0 power generation electric drive, multiple stage simple multistage compressor 3h + liquid oxygen production machine 88l. 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.

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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 43 applications, including PCT, from the filing date of Japanese Patent Application No. 2012-202141 to September 14, 2012.

  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.

Horizontal full-blade ratio critical material gravity turbine 8U fuel cost 0 power generation cheap electric drive all, solar heater 21 + both sides center support bearing load coalescence 0 approach, heat by simple multistage compressor 3h + liquid oxygen production machine 88l etc. Manufactured as electricity + liquid air cold heat + high temperature water to superheated steam temperature heat supply equipment 3D, the received liquid oxygen 5K is compressed to 21/60000 volumetric compression work rate of air compression, and super high pressure combustion and super high temperature combustion are easy As the rocket combustion theoretical combustion chamber 4Q, 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, A simple gas engine 88m, a simple water injection engine 88n, and a simple injection engine 88o that are close to the center support bearing load merge 0 are used to rotate vehicles, ships, and airplanes such as automobiles. In the case of ship propulsion propulsion drive, quick levitation propulsion and natural phenomenon acceleration 2a are performed by short-time rocket injection, oxygen, nitrogen, CO2 etc. are supplied into the sea, and microorganisms, phytoplankton, seaweeds, Increase coral, fish, etc., increase human food, and the plane also makes short rocket jets to make 16 orbits of the earth on a full day of space flight. The world's 100% monopoly, top-secret manufacturing power generation, ships, airplanes, automobiles, etc., making it the best in the world for profitability and the best for new jobs, dredging, concentrated torrential rains, typhoons, seasonal winds and heavy rains in seawater To prevent the global warming and postpone human extinction.

Horizontal type full blade ratio material Gravity turbine 8U Fuel cost 0 Low cost power generation The counter synchronous rotation by the counter synchronous gear 4C, and the effect of the same speed rotation by 100 series rotation gear 4D, etc. Group 8A is 100 types of fully automatic manufacturing of 100 sets, and the effect of 100 sets manufacturing is very great, the effect of simplifying the structure without the need of a boiler or nuclear reactor is also great, and the same degree of vacuum as the existing steam turbine final blade group When the driven horizontal full blade ratio material gravity turbine 8U power generation is compared with the final speed blade group of the maximum speed by the same vacuum water drive, the steam of 1700 times volume of water at an atmospheric pressure of 100 ° C. and 760 mmHg has an exhaust temperature of 29 According to Boyle's law at a degree of vacuum of 30 mmHg, 760 mmHg × 1700 = 30 mmHg × V2 volume water vapor, and V2 = 760/30 × 1700 = water 43000 Become a volume water vapor, it will be 430 times the amount of power generation in the 1/100 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 = Aiming for 30 times the amount of electricity generated by Mach 30 and further aiming for 406 times the amount of electricity generated by mercury injection, the experimental results are correct, but the power generation cost has been greatly reformed to 1/10, etc. Has the effect of

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 As an increase in the super high pressure high temperature combustion near the center of the theoretical combustion chamber 4Q, the simple gas engine 88m, the simple water injection engine 88n, and the simple water injection engine 88n, which are close to the both side center support bearing combined load 0 by the theoretical combustion chamber 4Q The injection engine 88o has the effect of being able to drive the super-high speed most efficiently. In addition to the effect of aiming for a fuel cost of 1/10 or 10 times the speed of automobiles, ships and airplanes, the space arrival cost is reduced to 1/50 of that of existing space rockets. There is an effect that can be aimed at all costs, and the wheels, screws 7C, propellers 7A and rotor blades 7B are driven by simple gas engines 88m, and ships, airplanes, automobiles, etc. are driven by rotational force, The jet propulsion drive speeds up the natural phenomenon 2a, and the effect of increasing the digestive capacity of underwater microorganisms such as CO2 to tens of thousands of times in the forest is great, and phytoplankton, seaweeds, corals, etc. are proliferated in food chains, etc. Greatly increase marine foods such as fish, prevent desertification, droughts, torrential rains, typhoons, seasonal winds, earthquake tsunamis, etc. There is an effect that can aim.

Airplane 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 type whole blade ratio critical material gravity turbine 8U power generation electric drive, theoretical combustion chamber Optimum heating of ultra-high pressure water, ultra-high pressure fuel, etc. with the high-temperature water heating pipe 5H etc. on the inner periphery of 4Q, open the fuel injection nozzle 6X + oxygen injection nozzle 6L, and mix injection ignition combustion near the center of multiple locations of oxygen gas + fuel gas Then, the theoretical combustion chamber 4Q of the existing improved technology is used as the 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 or the like. Combined with multiple 4Q units, driving a simple injection engine 88o with two-sided center support bearing load uniting close to zero, aiming for space arrival cost 1 / 500,000 of existing space rockets, and the same fuel cost 10 The jet propulsion output has the effect of aiming for the prime use of space. For example, the jet propulsion output is aimed at 100 times pressure 10 times calorie injection for a short time 1000 times injection propulsion output, and propeller flight and rotor blades with low fuel costs in the atmosphere With the aim of flying and jet propulsion, superheated steam injection speed and combustion gas injection speed are the highest in vacuum. When rising, the rocket injection amount of high pressure high temperature combustion gas 49 + high pressure high temperature superheated steam 50 of 24-200MPa is increased from the vicinity of the highest flight altitude of the existing aircraft, and 16 rounds of the earth per day etc. It has the effect of being able to aim for a possible use of space.

Explanatory drawing of 4C4D of horizontal type moving blade ratio critical material gravity turbine 8U (Example 1) Explanatory drawing of 8A9C9B of horizontal type moving blade ratio critical material gravity turbine 8U (Example 2) Explanatory drawing of the solar heater 21 (Example 3) Explanatory drawing of the liquid oxygen production machine 88l (Example 4) Explanatory drawing of simple multistage compressor 3h (Example 5) Illustration of simple gas engine 88m (Example 6) Explanatory drawing of the simple water injection engine 88n (Example 7) Explanatory drawing of the simple injection engine 88o (Example 8) Illustration of simple gas locomotive 7r (Example 9) Explanatory drawing of simple gas engine ship 7s (Example 10) Explanatory drawing of the simple gas engine airplane 7t (Example 11) Explanatory drawing of the simple water injection engine ship 7u (Example 12) Explanatory drawing of the simple injection engine airplane 7v (Example 13) Explanatory drawing of rotary wing airplane 7w (Example 14) Explanatory drawing of the rotary wing jet airplane 7x (Example 15) Illustration of oversized Osprey 7y (Example 16) Illustration of Large Osprey 7z (Example 17)

  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 atmospheric pressure, the same speed, the same volumetric power, kg-heavy m / sec, are reduced to 1/1700 of the water power, and the stationary blades are arranged alternately with the moving blades to dam and close the rotation output to zero. The total amount of heat generated by the power generation increases by 7 degrees in the seawater temperature, the fishes drastically decrease, the bottom bedrock expands into earthquakes and tsunamis, and the typhoon, seasonal winds, and sea tornadoes in the sea near Japan are increased to about 100m / sec. There is a danger that the drought of humans will rapidly extinguish due to the provision of salt coating on the land in about 50 to 100 years, such as a heavy rain of suctioned seawater is expected over the sea. In other words, since the invention becomes too large due to many fatal defects of the existing technology, the invention is described in the explanation of the reference numerals, and the parts that have been repeatedly explained in the previous application are omitted, and other than the horizontal type full blade ratio material gravity turbine 8U Is replaced with three types of examples, the use of existing technology such as magnetic bearings challenged the realization of the invention that omitted common sense, and gravity-accelerated power generation electric product drive in vacuum approaching both-side center support bearings combined 0 approach The simple multistage compressor 3h + liquid oxygen production machine 88l, the simple gas engine 88m, the simple water injection engine 88n, and the simple injection engine 88o are driven into automobiles, ships and airplanes.

Figure 1 Gravity acceleration in vacuum + mercury injection speed Mach 30 drive, etc., aiming to the limit, horizontal type blade blade critical material gravity turbine 8U power generation is proportional to kg weight m / second, so both sides of cylindrical turbine blade group 8A 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 and 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. Medium mercury gravity acceleration Mach 30 Turbine driving approach aiming, horizontal axis 16A with horizontal shaft plate 16 aiming at infinite increase of fixed rotation speed and rotation outer diameter, one type is manufactured 2 sets 1 set 100 sets in series Movement As a manufacture of flywheel turbines, or as one set, 200 series full-blade flywheel turbines and bite-in series full-blade flywheel turbines, each with 100-200 sets vertically by fully automatic casting, fully automatic processing, etc. One unit is manufactured, and 100 units, etc. are installed in the existing highest building height of vertical 828m, and one unit is provided. For example, the mercury 3E platinum ball 2E is vertically increased by 50 to 828m etc. by the specific material rising device 2F. The platinum sphere 2E is mixed and injected with the mercury 3E pressure by the specific material accelerator 6W to aim at the Mach 28 injection, and the gravitational acceleration acceleration vacuum acceleration drive is performed, and the cylindrical turbine blade group 8A is rotated counterclockwise by the countersynchronous gear 4C. The gravity acceleration part 1g that makes 100 sets of the same speed and the same direction and the same direction and the same rotation in the same direction and the same rotational speed 4D, facilitates mass production inexpensively, eliminates the need for a boiler and a reactor, and accelerates mercury etc. in a vacuum. The generator 1 is provided for each of the upper synchronous gear 4C main shaft and the series co-rotating gear 4D main shaft, and the generator power generation cost is targeted for 1/10 out of the turbine outer box 77a. Extremely simple and extremely inexpensive electric product drive infinity and electric drive infinity, and the world's best energy conservation cycle combined engine power generation and combined method power generation with outstanding profitability.

The horizontal full-blade specific material gravity turbine 8U power generation is composed of 100 units such as 100 existing vertical buildings in the turbine outer box 77a and one unit, and a platinum ball 2E with mercury 3E pressure, for example, by a specific material accelerator 6W. Mixed injection + acceleration of gravity acceleration in vacuum = Mach 28 aiming, injected into cylindrical turbine blade group 8A, horizontal full blade ratio material gravity turbine 8U drive power generation, maintaining Mach 28 speed aim, gravity acceleration in vacuum As the maximum acceleration effect, the next turbine is driven by the next turbine to make effective use of the head to make the gravity turbine 8U power generation, and by frictional heat cooling, it is easy to exceed the existing power generation maximum vacuum such as 30mmHg by air extractor 51 , 100 pairs are selected for the drop 828m, etc., and compared with the final stage of the existing steam turbine power generation, the vacuum is 30mmHg water 43000 times volume Mach 1st speed As a steam, a simple comparison with 100U of turbines with 100 sets of stacks will be described as follows: 1/1000 volume of mercury is 43 × 100 × 13, 55 = 58265 times mercury generated by Mach 1 speed injection, Various energy storage cycle coalescence engine fuel costs become extremely low-cost power generation, resulting in a power generation amount of astronomical magnification that requires experiments such as calculation of 91891 times platinum ball power generation amount.

  The horizontal full blade ratio critical material gravity turbine 8U power generation of FIG. 2 includes repulsive permanent magnets 9B attracting permanent magnets 9C on the cylindrical turbine blade group 8A on both sides and the center, and the cylindrical turbine blade group 8A side is in a ring shape. As per-pole 1-pole 1-pole magnetisation, the turbine outer box 77a side is a ring-type inner 2-pole upper attracting permanent magnet 9C lower repulsive permanent magnet 9B, and there are a plurality of locations, and the weight of the rotating part is determined by repulsive force or attractive force. The bearing load is brought close to 0 and the aim is to update the super high speed turbine peripheral speed record, and the most important configuration in the cylindrical turbine blade group 8A is the lowest friction loss, so the friction according to the material used is important. It is possible to select loss-reducing coating or wear-resistant coating, reduce the weight by cutting the entire inner cylinder surface, and increase the diameter of the cylindrical turbine blade group. Specific material gravity Bin 8U is easy to manufacture, fully automatic processing and precision assembly is easy. As long as possible, 100 sets can be manufactured in the vertical 828m as the maximum experimental diameter, and the horizontal synchronous shaft 4A is provided with the counter synchronous gear 4C on the horizontal shaft 16A. The counter-weight material gravity turbine 8U is opposed to the same speed synchronous rotation and connected by the series rotation gear 4D so as to rotate in the same direction and at the same speed. The rotor blade series ratio critical material gravity turbine 8U and the horizontal all blades bite serial ratio gravity material gravity turbine 8U are provided, and the horizontal shaft 16A is equipped with the generator 1 to generate 100 sets or more of driving power outside the turbine outer casing 77a. In addition, it is extremely simple in structure and requires no boilers or reactors, making the manufacturing cost extremely low, and making it the world's best with no comparisons such as zero fuel consumption. Down 8U to extremely low-cost power generation.

The heat production of the solar heater 21 in FIG. 3 is a horizontal all-blade ratio critical material gravity turbine 8U fuel cost 0 power generation power generation extremely cheap electric drive, cheap electricity + liquid air cold heat + superheated steam temperature supply equipment 3D The solar heater 21 is provided with a buoyancy on the water surface or a circular railroad on a flat ground, and maintains solar light at a right angle from east to west. The vessel 21 is provided with a rotation support portion 4f and is equipped with a gear device 4d and a roller 4e. As the cylindrical rotation portion 77G, the vertical rotation of the sunlight is maintained at a right angle in the vertical direction. A device that maintains the rotation of sunlight in two directions at right angles and maximizes the air temperature in the heat absorption tube 4H, collects sunlight with the largest amount of earth in a straight line by the rectangular long lens 2d, and the focal length Heat absorption in the vicinity The internal air passage 28A has the maximum temperature of the air 28a, the temperature of the external air passage 28A increases, and the existing lens cross section is linearly extended as a rectangular long lens 2d, so that all lens materials can be used. A heat insulating material 2c such as foamed plastic is surrounded by a cylindrical rotating portion 77G or the like to form 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. 28A selective suction as 1 to multi-stage heat pump 1G, suction compression, simple multi-stage compressor 3h or the like as heat pump 1G, 800 to 1200 ° C multiple times, 1 to multi-stage compression heat recovery unit 2C to recover heat per compression The liquid air 28a cold heat is stored in the liquid oxygen chamber 5K + liquid nitrogen chamber 5L, and the 24-heat of 24-200 MPa superheated steam 50 is heated to the high-pressure high-temperature steam chamber 5N. Save and electrical + liquid air cold + using various applications in the superheated steam heat supply facilities 3D, the electric drive flourish and battery driven prime, to various thermal utilization prime and various cold use PRIME electrical product.

  The liquid oxygen producing machine 88l, which has a center support on both sides + 9b + 9c and a combined bearing load of 0 in FIG. As a fitting assembly part 9M assembly, fully automatic mass production, fully automated processing, easy assembly, aiming at 1/100 parts count, simple multistage compressor 3h connection aim, horizontal type full blade ratio material gravity turbine 8U fuel cost 0 Power generation Extremely inexpensive electric drive, etc. For multi-stage compression, simple multi-stage compressor 3h and coupled drive compression, and for 1-multi-stage compression, simple compressor 3s water cooling + water injection compressed air multi-stage cooling Then, heat production heating air 28a of the solar heater 21 is used as compression heat recovery, and high pressure high temperature water heating pipe 5H temperature production + rectification tower exhaust gas pipe 5h cooling is prepared for production of liquid oxygen + liquid nitrogen, etc., ultra high pressure compressed air 28a is empty The turbine 3u is driven by ultra-high-speed injection counter-rotating to generate a large rotation output of the bearing load coalescence 0 approaching ultra-high speed rotation, thereby supplying exhaust gas to the rectifying tower as a significant reduction in motor drive power. The liquid oxygen is refined into liquid oxygen + liquid nitrogen and the exhaust gas is supplied to the rectifying tower exhaust pipe 5h, and the liquid oxygen production machine 88l is driven into a mass production of continuous warming + cold, electricity + liquid air cold + hot water ~ Supply to superheated steam temperature supply facility 3D, for example, in the heat supply, methane hydrate is recovered in the methane hydrate under the seafloor or permafrost land, and the methane recovery under permafrost land uses a transparent enclosure and uses specific gravity difference As recovery from the top of the top, the enclosure is eternal greenhouse pasture grazing, aiming at the prime of various heat utilization such as meat production, with liquid oxygen supply, the compression work rate is 21/60000 volumetric compression work of air compression As simple gas engine 88m drive, simple water injection engine 88n drive and simple injection engine 88o drive combined with liquid oxygen drive, various rotational drive such as car drive, ship drive and airplane drive and ultra high speed jet propulsion drive In the case of airplane driving, a space oxygen cost is 1 / 500,000, and a liquid oxygen production machine 88l that makes it possible to aim for a day trip anywhere on earth.

The simple multi-stage compressor 3h, which has a center support on both sides + 9b + 9c and a bearing load coalescence of 0 in FIG. As part 9M assembly, fully automated mass production, fully automated machining, easy assembly, 1/100 parts count, vertical full blade water gravity turbine 8P fuel cost 0 power generation extremely cheap electric drive, etc. In the case of compression, it is connected to a liquid oxygen production machine 88l or the like, and the compressed air heat recovery such as air 28a heated by the solar heater 21 is repeated one or more times to produce 50 heated superheated steam such as water heating + compressed air. 28a cold heat production is repeated one or more times to make mass production of super high pressure superheated steam 50 warm heat + ultra high pressure compressed air 28a cold heat, aiming at 1/10 production cost of the existing liquid oxygen production cost, etc. 60A Side center support bearing load coalescence approaching zero, enabling a large and large ultra-high speed counter rotating compressor and micro ultra high speed counter rotating compressor, making it a simple multistage compressor 3h that can handle all conditions, and double when assembling The reversing machine outer case 77C is divided into two parts at the horizontal shaft 1h, and the double reversing gear device 85Y is first assembled, so that the outer compression blade 8m outlet blade of the outer shaft device 60B60B and the inner blade device 60A60A are compressed inside. The blade 8k outlet blade and the inlet blade are assembled, and one to a plurality of inner compression blades 8k intermediate blade intermediate blades + outer compression blades 8m intermediate blade intermediate blades are assembled to each other, and each inner compression blade 8k is assembled. The inlet blade outlet blade + outer compression blade 8m inlet blade outlet blade is assembled into the fitting assembly 9M, the compressor outer box 77b77b is assembled into the counter-rotating machine outer box 77C, and the compressor assembly outer box 77b is assembled. The next box 7 The assembly assembly part 9M is assembled to C, and the simple two-stage compressor 3t is constructed one after another. Liquid oxygen production machine 88 l connected drive, etc. Horizontal axis 1h Double reversal drive simple multistage compressor 3h.

The simple gas engine 88m with the center support on both sides + 9b + 9c and the bearing load united 0 approach in FIG. As a combined assembly part 9M assembly, fully automatic mass production, fully automatic processing, easy assembly, aiming at 1/100 parts count, simple multistage compressor 3h connection aim, horizontal full blade ratio material gravity turbine 8U fuel cost 0 Power generation from electricity + liquid air cold heat + high temperature water to superheated steam temperature heat supply equipment 3D, which is extremely low power generation, receives liquid oxygen + electricity + high temperature water to the theoretical combustion chamber 4Q, etc. driven by low cost electric products, and liquid By compressing oxygen, the compression volume work rate is set to 21/60000 volume compression work rate of air compression, liquid oxygen + liquid fuel + high temperature water is compressed to ultra high pressure such as 24-200 MPa, and high pressure high temperature water heating pipe 5H etc. heating The rocket combustion theoretical combustion chamber 4Q with two types of on-off valves 1Q closed and oxygen-fuel injection heated to an optimal temperature from the oxygen injection nozzle 6L + fuel injection nozzle 6X in the theoretical combustion chamber 4Q, 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 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 four times the fuel of the existing technology As the theoretical air-fuel ratio combustion amount, superheated steam 50 having an increased heat quantity of 200 MPa or the like is injected from the production superheated steam rocket nozzle 6A, and high-pressure high-temperature combustion chamber 5M combustion gas 49 having a fourfold combustion amount is sucked and injected by rocket injection, Liquid oxygen driven theoretical combustion chamber 4Q with a compression work rate of 21/60000 volumetric compression work rate of air compression as a simple gas engine 88m with a greatly improved existing gas turbine A number of coalesced and simple gas engine 88m used any liquid oxygen 0.

In the case of simple gas engine 88m drive in the liquid oxygen 0 existing technology improved theoretical combustion chamber 4Q, the existing jet engine and the stationary blades of the gas turbine are almost completely abolished, the counter rotating magnetic device 85 to the counter rotating gear device 85Y. Thus, the inner shaft device 60A + outer shaft device 60B approaching both sides center support bearing load combined 0 is double-reversed and the air 28a sucked from the inlet stationary blade 6G is linearly compressed by the inner compression blade 8k + outer compression blade 8m, Double reverse linear ultra-high-speed expansion high-power drive, compression 800-1200 ° C rise process, linear compression simple multi-stage compressor 3h connected, 2 to 5 times the target of relative speed existing gas turbine etc. 2 times compressed air pressure or more Etc. are made to be ultra-high pressure, compressed air is injected into the theoretical combustion chamber 4Q from the stationary blade 6G for compressed air injection in the outer casing 77C of the counter-rotating machine, and fuel is injected and burned from the fuel injection nozzle 6X. By using the hot water heating pipe 5H to produce superheated steam 50 having a heat recovery of 200 MPa or the like and producing the theoretical air / fuel ratio combustion, the combustion air 49 is more than 3/4 heat quantity of the combustion gas 49 as the four times fuel combustion quantity of an existing gas turbine or the like. Superheated steam 50 of 20 times pressure, etc. is rocket-injected, and the inner output blade 8n + outer output blade 8p is double-reversed driven in cooperation with the combustion gas 49, and the same compressed air amount is propelled by 10 times injection of existing jet engines and gas turbines. Aiming for output and 10-fold rotation output, the horizontal shaft 1h or the inner shaft device 60A is extended to rotate and drive generators, automobiles, ships and airplanes. In addition to driving, particularly in the case of power generation, the entire exhaust gas of the simple gas engine 88m is heat recovered by the heat exchange heating air 28a, and the high temperature water 52b of the compressed water jet heat recovery by the inner compression blade 8k + the outer compression blade 8m is high pressure. The air 28a is press-fitted into the hot water heating pipe 5H, and the air 28a is generated by repeating fuel injection combustion in the theoretical combustion chamber 4Q. Further, the power generation amount is increased by the combined high-temperature air 28a heating of the solar heater 21 in FIG. Similarly, the temperature is converted into the temperature of the air 28a and compressed by suction compressed water injection, and similarly, a simple gas engine 88m with an increased power generation amount is obtained.

The simple water injection engine 88n with the center support on both sides + 9b + 9c and the bearing load coalescence approaching 0 in FIG. As a fitting assembly part 9M assembly, fully automatic mass production, fully automated processing, easy assembly, aiming at 1/100 parts count, simple multistage compressor 3h connection aim, horizontal type full blade ratio material gravity turbine 8U fuel 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 21/60000 volume compression work rate of air compression, liquid oxygen + liquid fuel + high temperature water is compressed to ultra high pressure such as 24-200 MPa, high pressure high temperature water heating pipe 5H etc. In addition Then, in the rocket combustion theoretical combustion chamber 4Q in which the opening / closing 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 + hot water to superheated steam 50 is heated to the optimum temperature on the inner wall, and the theoretical air-fuel ratio combustion is performed, aiming at 40 times the pressure 40 times the combustion amount of existing jet combustion, and the superheated steam in the theoretical combustion chamber 4Q peripheral air 28a suction flow The superheated steam 50 and the high-pressure high-temperature combustion chamber 5M combustion gas 49 approaching 200 MPa are injected from the rocket nozzle 6A + combustion gas injection nozzle 6Y, the air 28a is suction-injected and water is suction-injected, and the existing technology improved theoretical combustion chamber In 4Q, as the theoretical air-fuel ratio combustion amount of the quadruple fuel of the existing technology, the superheated steam 50 aiming at 200 MPa with increased heat quantity is manufactured and the outer rocket outer box 77B superheated steam rocket Simple water that is a greatly improved existing jet engine, injecting 6A, generating rotational output in the high-pressure high-temperature combustion chamber 5M combustion gas 49, sucking and jetting the air 28a in front of the suction flow of the outer air 28a and sucking and jetting water 52a The injection engine 88n is a simple water injection engine 88n that uses a combination of a plurality of liquid oxygen drive theoretical combustion chambers 4Q with a compression work rate of 21/60000 volume compression work of air compression and is used even with zero liquid oxygen.

In the case of driving the simple water injection engine 88n in the liquid oxygen 0 existing technology improved theoretical combustion chamber 4Q, 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 The inner shaft device 60A + outer shaft device 60B approaching the both-side center support bearing load uniting 0 is double-reversed by 85Y, and the air 28a sucked from the inlet stationary blade 6G is linearly compressed by the inner compression blade 8k + outer compression blade 8m. , Fuel-injection-combustion, counter-rotating linear, ultra-high-speed expansion, large output, simple multi-stage compressor 3h connection, relative speed 2-5 times that of existing gas turbines, etc. Compressed air 28a is injected into the theoretical combustion chamber 4Q from the compressed air injection stationary blade 6G of the reversing machine outer box 77C, fuel is injected and combusted from the fuel injection nozzle 6X, and heat recovery is overheated by the high-pressure high-temperature water heating pipe 5H. By making the gas 50 into the production theoretical air-fuel ratio combustion, the same amount of compressed air as the existing gas turbine or the like, the fuel combustion amount of 4 times or the outer periphery as the rocket injection part, the combustion gas 49 more than 3/4 heat amount, 20 times the pressure etc. The superheated steam 50 is injected into the rocket outer box 77B, and the inner output blade 8n + the outer output blade 8p is driven in reverse by the combustion gas 49 so that the same compressed air amount is 15 times the injection propulsion output of the existing jet engine or gas turbine +5 A simple water-injection engine 88n is provided, which has a double-rotation output target, and has an air suction / injection cylinder only at the rear, with an increase in water resistance and an air suction / injection amount with an increase in water resistance of 0, and so on.

The simple injection engine 88o with the center support on both sides + 9b + 9c and the bearing load coalescence approaching 0 in FIG. 8 and the long high-speed double reversal is easy. As a fitting assembly part 9M assembly, fully automatic mass production, fully automated processing, easy assembly, aiming at 1/100 parts count, simple multistage compressor 3h connection aim, horizontal type full blade ratio material gravity turbine 8U fuel 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 volumetric power is made to be 21/60000 volumetric compression work of air compression, and liquid oxygen + liquid fuel + high temperature water is compressed and heated to ultrahigh pressure such as 24 to 200 MPa. Open and close 1Q is closed in two types of rocket combustion theoretical combustion chamber 4Q, oxygen + fuel injection combustion heated to the optimum temperature from oxygen injection nozzle 6L + fuel injection nozzle 6X, fuel + oxygen + hot water ~ on the inner wall of theoretical combustion chamber 4Q The superheated steam 50 is heated to the optimum temperature and the 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 superheated steam rocket nozzle 6A in the rocket outer box 77B + combustion gas injection nozzle 6Y approaches 200 MPa. The superheated steam 50 and the high-pressure high-temperature combustion chamber 5M combustion gas 49 are injected, and when the on-off valve 1Q is closed, the high-power rocket combustion space utilization is primed. 4Q multiple rocket combustion chambers and jet combustion chambers driven by liquid oxygen, and the existing technology improved jet combustion theoretical combustion chamber 4Q has four times the fuel of the existing technology As the air-fuel ratio combustion amount, the superheated steam 50 is produced with an increased heat quantity and is aimed at 200 MPa, injected from the rocket outer box 77B superheated steam rocket nozzle 6A, rotated and generated in the high-pressure and high-temperature combustion chamber 5M combustion gas 49, and the front air 28a As a simple injection engine 88o that greatly improves the existing jet engine, a plurality of liquid oxygen drive theoretical combustion chambers 4Q are combined, and a simple injection engine 88o that uses even liquid oxygen is used.

The case of driving the simple injection engine 88o 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 substantially abolished, and the counter rotating magnetic device 85 to the counter rotating gear device 85Y. Accordingly, the inner shaft device 60A + outer shaft device 60B approaching both side center support bearing loads 0 is double-reversed and the air 28a sucked from the inlet stationary blade 6G is linearly compressed by the inner compression blade 8k + outer compression blade 8m. Fuel injection combustion counter-rotating linear ultra-high-speed expansion with large output, simple multi-stage compressor 3h connection, 2-5 times the relative speed of the existing gas turbine etc. Compressed air 28a is injected into the jet combustion theoretical combustion chamber 4Q from the compressed air injection stationary blade 6G of the outer box 77C, fuel is injected and combusted from the fuel injection nozzle 6X, and is heated by the high-pressure high-temperature water heating pipe 5H. By making the superheated steam 50 into a production theoretical air-fuel ratio combustion, the same compressed air amount 4 times the fuel combustion amount of the existing gas turbine or the like, and the outer periphery as the rocket injection part 3/4 heat amount or more of the combustion gas 49, 20 times the pressure, etc. The superheated steam 50 is injected into the rocket outer box 77B, and the inner output blade 8n + outer output blade 8p is driven in reverse by the combustion gas 49, and the same compressed air amount is 15 times the injection propulsion output of the existing jet engine or gas turbine. A simple injection engine 88o is used, which aims at +5 times rotation output, and makes the water-injected vessels and airplanes into injection propulsion drive.

The simple gas engine vehicle 7r of FIG. 9 is an improved invention of the existing micro gas turbine vehicle. The simple gas engine 88m can select a compressed air drive + a fuel cost zero power generation electric product selection drive. Large material gravity turbine 8U Fuel cost 0 Power generation Extremely inexpensive electricity production Electricity + Liquid air cold heat + High temperature water to superheated steam temperature heat supply equipment 3D, Low oxygen electric product driven theoretical combustion chamber 4Q etc. Liquid oxygen + electricity + By receiving 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 compressed and heated to an ultrahigh pressure such as 24-200 MPa. Then, in the rocket combustion theoretical combustion chamber 4Q in which the on-off valves 1Q at the plurality of inlets are closed, the oxygen + fuel injection combustion heated to the optimum temperature from the oxygen injection nozzle 6L + fuel injection nozzle 6X is performed. Fuel + oxygen + high-temperature water to superheated steam 50 is heated to the optimum temperature on the inner wall of the combustion chamber 4Q, and the combustion is aimed at the theoretical air-fuel ratio combustion. Then, as the theoretical air-fuel ratio combustion amount of 4 times fuel 4 times combustion amount of the existing technology, superheated steam 50 such as 200 MPa with increased heat quantity is injected from the production superheated steam rocket nozzle 6A, and 4 times combustion or 40 times combustion by rocket injection The high pressure high temperature combustion chamber 5M combustion gas 49 is sucked and injected, and as a simple gas engine 88m which is a greatly improved existing micro gas turbine, the generator 1 is driven to drive the storage battery drive wheel 4J to the storage battery 1A, and the compressed air drive Liquid oxygen-driven theoretical combustion chamber 4Q used as a power plant or power storage station. Combined with multiple combustion chambers 4Q, even with liquid oxygen 0, ultra-high speed rotation output + ultra-high pressure injection Corresponding to the binary output increase in weight, and easy gas engine automobile 7r.

The simple gas engine ship 7s shown in FIG. 10 is an improved invention of the existing gas turbine ship. The simple gas engine 88m can be selected from compressed air drive + fuel cost 0 generation electric product selection drive. Material Gravity Turbine 8U Fuel Cost 0 Power Generation Extremely Low Cost Electric Manufacturing Electricity + Liquid Air Cold Heat + High Temperature Water to Superheated Steam Heat Supply Facility 3D, Theoretical Combustion Driven Theoretical Combustion Chamber 4Q etc. Liquid Oxygen + Electricity + High Temperature By receiving water 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 + hot water is compressed and heated to an ultrahigh pressure such as 24-200 MPa. Thus, in the rocket combustion theoretical combustion chamber 4Q in which the on-off valves 1Q of the plurality of inlets are 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 4 Fuel + oxygen + high-temperature water to superheated steam 50 is heated to the optimum temperature on the inner wall, and the combustion is aimed at the theoretical air-fuel ratio combustion, aiming for 40 times the pressure and 40 times the combustion amount of the existing jet combustion, and the existing technology improved theoretical combustion chamber 4Q 4 As the stoichiometric air-fuel ratio combustion amount of quadruple fuel combustion amount, superheated steam 50 of 200MPa etc. with increased heat quantity is injected from the production superheated steam rocket nozzle 6A, and high pressure high temperature combustion aiming at quadruple combustion amount or 40 times combustion by rocket injection As a simple gas engine ship 7s that sucks and injects the combustion gas 49 in the chamber 5 and greatly improves the existing gas turbine ship, the screw 7C drive exhaust is injected to the top bottom of the ship with the rotational output of the simple gas engine 88m. As a result of rocket combustion capable of 10 times output, etc., it is possible to rapidly fly and approach a glide, to reduce fuel loss by drastically reducing friction loss, and to save liquid oxygen. As chamber 4Q plurality of coalesced, 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 7s.

The simple gas engine plane 7t of FIG. 11 is an improved invention of the existing jet aircraft. The simple gas engine 88m can be selected to be driven by compressed air + zero fuel cost generation electric product selection drive. 8U fuel cost 0 power generation Extremely cheap electricity production Electricity + liquid air cold heat + hot water to superheated steam heat supply facility 3D Receives liquid oxygen + electricity + hot 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 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 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 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 four times the fuel of the existing technology As the theoretical air-fuel ratio combustion amount of 4 times 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 by exhaust injection or rocket injection, 4 times combustion amount or 40 times combustion target high pressure As a simple gas engine airplane 7t that injects the high-temperature combustion chamber 5M combustion gas 49 and greatly improves the existing jet aircraft, the propeller 7A drive exhaust is injected backward with the rotational output of the simple gas engine 88m, aiming for 40 times output for a short time Rocket combustion + 4 times output targeted jet combustion, etc. As a combination of multiple liquid oxygen driven theoretical combustion chambers 4Q, space arrival cost 1 / 500,000 target and atmospheric return speed Mach 3 or less and, in the atmosphere to fly even LOX 0 corresponds to ultra high speed output + ultra high-pressure jet propulsion output increase in weight, and large simple gas engine airplane 7t.

The simple water injection engine ship 7u in FIG. 12 is an improved invention of an existing gas turbine ship. The simple injection engine 88e can be selected to be driven by compressed air + zero fuel cost, and a power generation electric product selection drive. Material Gravity Turbine 8U Fuel Cost 0 Power Generation Extremely Low Cost Electric Manufacturing Electricity + Liquid Air Cold Heat + High Temperature Water-Superheated Steam Heat Supply Facility 3D to Low Temperature Electric Product Driven Theoretical Combustion Chamber 4Q etc. Liquid Oxygen + Electricity + High Temperature By receiving water 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 + hot water is compressed and heated to an ultrahigh pressure such as 24-200 MPa. Then, oxygen + fuel injection combustion heated to an optimum temperature from the oxygen injection nozzle 6L + fuel injection nozzle 6X in the rocket combustion theoretical combustion chamber 4Q with the multiple inlet / outlet opening / closing valves 1Q closed, and theoretical combustion Fuel + oxygen + hot water to superheated steam 50 is heated to the optimal temperature on the 4Q inner wall, and the combustion is aimed at the theoretical air-fuel ratio combustion, aiming at 40 times the pressure 40 times the combustion amount of the existing jet combustion, and the superheated steam rocket nozzle 6A + around the theoretical combustion chamber 4Q From the combustion gas injection nozzle 6Y, superheated steam 50 and high-pressure high-temperature combustion chamber 5M combustion gas 49 approaching 200 MPa are injected. When the on-off valve 1Q is closed, high-power rocket combustion is performed, and when the on-off valve 1Q is opened, the front air 28a is sucked. As injection 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 Manufacture superheated steam 50 aiming at 200MPa, inject from rocket outer box 77B superheated steam rocket nozzle 6A, high pressure high temperature combustion chamber 5M combustion gas Rotational output is generated at 49, and the front air 28a is sucked and jetted to suck and jet water, and as a simple water jet engine 88n drive that greatly improves the existing jet engine, the liquid oxygen drive theoretical combustion chamber 4Q is suddenly combined with multiple. A simple water-injection engine ship 7u corresponding to an increase in weight of an ultra-high-speed rotation output + ultra-high-pressure injection propulsion output, aiming at maintaining the flight speed even in the vicinity of zero liquid oxygen, is set to a flying speed.

The simple injection engine airplane 7v of FIG. 13 is an improved invention of the existing jet aircraft. The simple injection engine 88e can be selected to be compressed air drive + zero fuel cost electric power generation electric product selection drive. 8U fuel cost 0 power generation Extremely cheap electricity production Electricity + liquid air cold heat + hot water to superheated steam heat supply facility 3D Receives liquid oxygen + electricity + hot 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 in which the opening / closing valve 1Q at the inlet / outlet 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 The superheated steam 50 and the high-pressure high-temperature combustion chamber 5M combustion gas 49 approaching 200 MPa are injected from the gas injection nozzle 6Y. 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, and the conventional technology improved theoretical combustion chamber 4Q is used as a theoretical air-fuel ratio combustion of four times the fuel of the existing technology with an increased amount of heat. Manufactured superheated steam 50 aiming at 200 MPa, injected from rocket outer box 77B superheated steam rocket nozzle 6A, and generated high-speed high-temperature combustion chamber 5M combustion gas 49 to generate rotational output. Then, as a simple injection engine 88o drive that sucks and injects the air 28a in front and greatly improves the existing jet engine, the liquid oxygen drive theoretical combustion chamber 4Q is combined with a plurality of the space arrival cost 1/5 million target of the existing technology, Atmospheric return speed Mach 3 or less, high-speed flight with zero liquid oxygen in the atmosphere, ultra-high-speed rotation output + ultra-high-pressure jet propulsion output weight increase driven by inner shaft device 60A and propeller 7A depending on application Let it be a jet engine plane 7v.

The rotary wing airplane 7w of FIG. 14 is an improved invention of the existing rotary wing aircraft. The simple gas engine 88m can be selected to be driven by compressed air + zero fuel cost power generation electric product selection drive. Turbine 8U Fuel cost 0 Power generation Extremely inexpensive electricity production Electricity + liquid air cold heat + high temperature water ~ superheated steam temperature heat supply equipment 3D, liquid oxygen + electricity + high temperature water is supplied 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 in which the on-off valve 1Q at the plurality of inlets 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 + hot water-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, the theory of 4 times fuel combustion of the existing technology in the jet combustion theory combustion chamber 4Q As the air-fuel ratio combustion, 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 the high pressure and high temperature combustion chamber 5M aiming at the four times combustion quantity or 40 times combustion by exhaust injection or rocket injection. As a rotor blade airplane 7w, which is an improved and improved existing rotor wing aircraft, the rotary output of the simple gas engine 88m is used to rotate the rotor 7B to drive the rotational force + jet propulsion, and the inner shaft device 60A is extended to the rotor 7B. Rocket combustion capable of 10 times output etc. + jet combustion + rotation output + injection propulsion output, compressed air + liquid oxygen driven theoretical combustion chamber 4Q Combining multiple combustion chambers 4Q 1/50 ten thousand aim or use existing technologies, 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 7w.

A rotary blade injection airplane 7x in FIG. 15 is an improved invention of an existing rotary blade aircraft. The simple injection engine 88e can be selected to be driven by compressed air + fuel cost 0 generation electric product selection drive. Gravity turbine 8U Fuel cost 0 Power generation Electricity + liquid air cold heat + high temperature water to superheated steam temperature heat supply equipment 3D from liquid electricity + electricity + high temperature water to the theoretical combustion chamber 4Q etc. driven by low cost electric products 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 / outlet on-off valves 1Q 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 at 40 times the pressure 40 times the combustion amount of the existing jet combustion, superheated steam rocket nozzle 6A + combustion gas injection around the theoretical combustion chamber 4Q From the 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, the high power rocket combustion space utilization prime is used, and when the on-off valve 1Q is opened, compressed air 28a combustion is performed. Injecting by theoretical air-fuel ratio combustion, etc., a plurality of theoretical combustion chambers 4Q are used as rocket combustion chambers and jet combustion chambers driven by liquid oxygen, and in the compressed air combustion jet combustion theoretical combustion chamber 4Q, the theoretical air-fuel ratio combustion of four times the fuel of the existing technology The superheated steam 50 aiming at 200 MPa with an increased heat quantity of 3 times is produced, the rotational output is generated by the high-pressure high-temperature combustion chamber 5M combustion gas 49 injection, and the outer air 28a Superheated steam 50 is jetted from the convection superheated steam rocket nozzle 6A, the air 28a in front is sucked and injected, and as a simple injection engine 88o driven close to the existing jet engine, the liquid oxygen drive theoretical combustion chamber 4Q is combined into a plurality of space Achieving cost 1 / 500,000 of existing technology, air return speed Mach 3 or less, flying in the atmosphere with liquid oxygen 0, driving inner shaft device 60A extension rotor 7B, ultra high speed rotation output + ultra high pressure injection propulsion A large rotary wing jet airplane 7x corresponding to an increase in output weight is assumed.

The oversized Osprey 7y in FIG. 16 is an improved invention simple injection engine 88o of an existing rotor blade and propeller aircraft, which can be selected from compressed air drive + zero power generation electric product selection drive. Large material gravity turbine 8U Fuel cost 0 Power generation Extremely inexpensive electricity production Electricity + Liquid air cold heat + High temperature water to superheated steam temperature heat supply equipment 3D, Low oxygen electric product driven theoretical combustion chamber 4Q etc. Liquid oxygen + electricity + By receiving 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 compressed and heated to an ultrahigh pressure such as 24-200 MPa. Then, 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, and the theoretical fuel Fuel + oxygen + hot water ~ 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. 6A + combustion gas injection nozzle 6Y is used to inject superheated steam 50 and high-pressure high-temperature combustion chamber 5M combustion gas 49 approaching 200 MPa. In the open state, 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 rocket combustion chambers / jet combustion chambers driven by liquid oxygen, and in the compressed air combustion jet combustion theoretical combustion chamber 4Q, the conventional technology 4 As the stoichiometric air-fuel ratio combustion of double fuel, superheated steam 50 is produced aiming at 200MPa with increased heat of 3 times, and it is rotated by high pressure high temperature combustion chamber 5M combustion gas 49 injection Generated, the superheated steam 50 is injected from the superheated steam rocket nozzle 6A of the peripheral air 28a suction flow, the front air 28a or vacuum is sucked and injected, and the existing jet engine is driven as a simple injection engine 88o with an ultra-high output. Liquid oxygen-driven theoretical combustion chamber 4Q Combined with multiple chambers to reach the space for 1 / 500,000 months of the existing technology. Atmospheric return speed Mach 3 or less, in the atmosphere, flying with liquid oxygen 0, inner shaft device 60A extended rotation A plurality of wing and propellers 7A are driven vertically ascending and horizontally flying to form an ultra-large extra large Osprey 7y corresponding to an ultra-high-speed rotation output + ultra-high-pressure injection propulsion output weight increase.

The large Osprey 7z shown in FIG. 17 is an improved invention of an existing rotary blade / propeller aircraft. The simple gas engine 88m can be selected from compressed air drive + zero fuel cost electric product selection drive. Large material gravity turbine 8U Fuel cost 0 Power generation Extremely inexpensive electricity production Electricity + Liquid air cold heat + High temperature water to superheated steam temperature heat supply equipment 3D, Low oxygen electric product driven theoretical combustion chamber 4Q etc. Liquid oxygen + electricity + By receiving 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 compressed and heated to an ultrahigh pressure such as 24-200 MPa. Then, in the rocket combustion theoretical combustion chamber 4Q in which the on-off valves 1Q at the plurality of inlets are 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 Heating the fuel + oxygen + hot water to superheated steam 50 to the optimum temperature on the Q inner wall, and setting the theoretical air-fuel ratio combustion to 40 times the pressure 40 times the combustion amount of the existing jet combustion, the jet combustion theoretical combustion chamber 4Q 4 of the existing technology As the stoichiometric air-fuel ratio combustion of double fuel combustion, 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 four times the combustion quantity or 40 times pressure injection by exhaust injection or rocket injection Target high-pressure high-temperature combustion chamber 5M injection, large-sized Osprey 7z, which is a greatly improved existing rotor blade / propeller aircraft, exhaust blade + propeller 7A multiple drive vertically rising horizontal flight with rotary output of simple gas engine 88m, exhaust injection + rocket Rotation output + injection propulsion output by injection, rocket injection + jet capable of 40 times pressure injection by driving inner shaft device 60A extension rotor blade and propeller 7A Combustion + rotation output + injection propulsion output, compressed air + liquid oxygen drive theoretical combustion chamber 4Q Combined with multiple combustion chambers, the space arrival cost is 1 / 500,000 months landing return aim, the atmospheric return speed Mach 3 or less Large, large-scale osprey that can fly in the atmosphere with liquid oxygen 0, or fly vertically and horizontally by driving multiple inner shaft device 60A extension rotors and propellers 7A to support increased ultra-high-speed rotation output + ultra-high-pressure jet propulsion output weight 7z.

Compared to the existing pumped-storage power generation, the horizontal full-blade specific material gravity turbine 8U power generation aiming at a resource price of 0 fuel cost of 0 power generation less than 1/2 of the nuclear power generation. Gravity acceleration in a vacuum is added to the water injection speed Mach 3 or higher, and the work rate is proportional to the speed + proportional to the height, so the mercury injection speed Mach 3 or higher + gravity acceleration in the vacuum = Mach 30 limit speed drive The aim is 100 times the speed 1/100 mass vertical mercury drive + all-blade horizontal axis 1h double reversal drive, maximizing the power of 9.8m / second in gravity acceleration in vacuum, 200 in the world's highest building height 828m There is a possibility of extremely low-priced power generation with a horizontal full-blade specific material gravity turbine 8U power generation that has one set of power generation with a set and has the same mercury amount 2710 times as much as the existing pumped storage power generation.

In the process of comparative explanation of gravity turbine 8U power generation with a horizontal full-blade ratio, which is targeted for less than 1/2 of nuclear power generation, with a resource price of 0 fuel costs of 0 power generation, and atmospheric pressure according to Boyle's law The steam of 1,700 times the volume of water at 100 ° C. and 760 mmHg becomes the steam of 43,000 times the volume of water at an exhaust temperature of 29 ° C. and a vacuum pressure of 30 mmHg, and assuming that the existing steam turbine final blade group steam velocity is the sonic velocity, the inlet high pressure blade Since the group steam velocity is 1 / 100th or less of the speed of sound, the work rate is the lowest. When the water drive volume is 1/433000 volume 29 ° C water drive, which is 29 ° C water vapor, the same amount of power is generated by driving the cylindrical turbine blade group 8A, and 200 times power generation is generated by 1/215 volume water drive. If it is calculated by elementary school science, such as the amount of power generation, 271,000 times the power generation of one unit of 100 pairs connected, there is a possibility that extremely low-cost power generation will be an astronomical large power generation amount.

Horizontal type moving blade ratio critical material gravity turbine 8U power generation Extremely cheap power generation, electric product prime, electricity + liquid air cold heat + superheated steam temperature supply facility 3D receives superheated steam, methane hydrate under the seabed or permafrost land Food companies for methane recovery, permafrost land grazing conversion, overheating steam injection in oil sand zone, oil shale zone and old oil extraction zone, vaporization recovery liquefaction preservation etc. Then, it is possible to receive superheated steam at low cost for mass production of cheap food products, etc., and to use it for agriculture, industrial use, industrial use, mining, etc.

Horizontal type moving blade ratio critical material gravity turbine 8U power generation Extremely inexpensive power generation, electric product prime as a prime of electricity + liquid air cold heat + superheated steam temperature supply equipment 3D receives liquid oxygen 5K, liquid oxygen drive and normal drive It is set as a combined driving car, ship, airplane, etc., and liquid oxygen 5K is liquid compressed to 21/60000 volumetric compression work rate of air volume compression work rate, simple gas engine 88m, simple water injection engine 88n, simple injection engine Driving 88o, there is a possibility that the CO2 exhaust and fuel cost will be close to 1/10 in the automobile, the ship may be close to 10 times the speed with the same fuel cost, and the plane will have a space arrival cost 1 / 500,000, etc. As a prime use of space, there is a possibility of making a great revolution in the use of cold energy, such as making a day trip anywhere on the planet.

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・ Various energy coalescing engine and various energy coalescence means that use and save the gravitational energy by ascending device) 1A: storage battery, 1B: pressure engine (oxygen pressure gear engine, oxygen pressure reciprocating engine, water pressure gear engine, water pressure reciprocating engine, etc., to make various pressure engines with a compression work rate of 1/600 by liquid compression) 1C: Alcohol, 1D: Fuel injection pump, 1F: Condensate pump, 1G: 1 to multi-stage heat pump (heat 50 is divided into hot room 3B + cold 28a is divided into cold room 3A, aiming at an infinite rise in pressure after increasing the amount of collected cold heat) 1K: Liquid fuel control valve, 1L: Fuel heating pipe, 1Q: On-off valve, 1Y: Multi-stage combustion chamber, 1b: Fuel (liquid fuel + liquefiable gas fuel) 1b: Fuel pipe (fuel injection temperature becomes optimum temperature) 1c: Liquid fuel, 1d: Mercury, 1g: Gravity acceleration part, 1h: Horizontal axis, 2: Solar heater (collecting sunlight in a straight line with a long lens to heat the hot part forming intake air 2a: Natural phenomenon high speed (A large amount of microorganisms that move to zero near the night when leftover foods with almost no change in the air move to nearby rivers will be used to increase food for humans) 2a: Acceleration of natural phenomena (In power generation, cold 28a is mixed with seawater for power generation) Supplying seawater that has been accelerated in natural phenomena to the seabed Supplying nutrients such as nitrogen, oxygen, and CO2 Increases microorganisms to increase foods such as fish and kombu 2a: Speeding up natural phenomena (in ships, nitrogen, oxygen, and CO2 in the sea) 2b: Low water resistance (air and combustion gas on the bottom of the ship) 2b: Low water resistance (air and combustion gas on the bottom of the ship) 2c: heat insulating material, 2d: long lens (convex lens cross-section is extended to a straight line and multiple lenses are used to achieve the maximum focal length lens width) 2e: water surface, 2A : Heat-resistant material, 2B: heat absorbing material, 2C: 1 to multiple-stage compression heat recovery device (heat energy is air temperature, heat pump is heat-recovered a plurality of times with a compression heat exchanger, and the rest is heated 50 + liquid cold 28a 2E: Specific critical substances (including alloys, platinum balls, gold balls, tungsten alloy powder sintered balls, silver balls, copper balls, tin balls, lead balls, zinc balls, aluminum balls, indium, cadmium, gallium, thallium, bismuth 2E: Specific critical substance (Manufacturing method reduces impact energy for smaller diameters. For example, molten steel is injected into the atmosphere to produce ultra-small diameter steel balls by high-speed collision pulverization and air cooling water cooling) 2E: Specific importance Substances (silicon resin-coated or silicon-resin-coated platinum alloy balls, coated gold alloy balls, coated tungsten alloy powder sintered balls, coated silver alloy balls, coated bismuth alloy balls, coated copper alloy balls, coated tin alloy balls, Lead-coated alloy balls, coated zinc alloy balls, coated aluminum alloy balls) 2F: Specific critical material raising device (gravity energy is increased and stored) 2H: Cold and hot seawater mixer, 2X: Air heat exchanger 2Y: Compressed air heat exchanger ( 2Z: Specific material heat exchanger (used for temperature control of liquid metal below 500 degrees) 3a: Water repellent plating, 3f: Simple multistage compressor, 3h: Simple multistage compressor, 3s : Simple compressor, 3t: Simple multi-stage compressor, 3u: Air turbine, 3A: Water repellent coating, 3B: Water pressure reciprocating engine, 3D: Electricity + liquid air cold heat + superheated steam heat supply equipment (cooling power by gravity power generation + Manufactures heat and supplies liquid oxygen and liquid nitrogen. Drives automobiles, ships and airplanes and supplies with superheated steam. Recovers methane injected into methane hydrate, etc. (Mercury, water, etc., liquid critical substances) 3E: Specific critical substances (low-melting-point alloy liquids up to 500 degrees and stable 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 volume of gas is the best in theory inversely proportional to pressure 3Q: Theoretical expansion engine (best engine + aiming at the maximum acceleration drive in vacuum by Boyle's law) 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 existing pumps in the engine) 3X: compressor engine (uses existing compressors in the engine) 3Y: counter-rotating engine (gas volume is inversely proportional to pressure) 3Z: Oxygen pressure gear engine, 3a: water repellent plating, 3b: water repellent coating, 4C: counter-synchronous gear, 4D: series rotation gear, 4F: combustion gas reciprocating engine, 4H: heat absorption tube (with long lens 2d) 4J: Storage battery drive wheels, 4K: Theoretical expansion engine vehicle, 4Q: Theoretical combustion chamber (superheated steam) Theoretical air-fuel ratio combustion in combustion: combustion chamber aiming for the existing 4-fold combustion amount and 20-fold pressure superheated steam injection, 4W: theoretical compression chamber, 4Y: theoretical combustion chamber (high-temperature combustion in water vapor and water pyrolysis electricity Cracked fuel Target Compound 0 Target Combustion Chamber) 4Z: Combustion gas gear engine, 4X: Turbine blade cross section (cross-sectional area is increased in surface area) 4a: Liquid fuel pump, 4b: Liquid oxygen pump, 4c: Water pump, 4d: Gear device, 4e : Roller, 4f: Rotation support part, 5: Air injection nozzle, 5a: High-pressure high-temperature combustion gas control valve, 5b: Compressed intake air passage, 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 pipe, 5H: high pressure high temperature superheated steam pipe, 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 water Air chamber, 5N: high-pressure and 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 critical material injection nozzle, 6F: water injection nozzle, 6G: stationary blade, 6H: drain pipe, 6L: oxygen injection nozzle, 6W: specific critical material accelerator ( 6X: Fuel injection nozzle, 6X: Afterburner (combustion of fuel injection cold heat 28a and combustion flow 6Y combined with suction air flow and fuel combustion amount) 6Y: Combustion gas injection nozzle (cooling 28a combustion flow) 6Z: Steam injection nozzle, 7A: Propeller, 7B: Rotary blade, 7C: Screw, 7D: Simple gas engine Vehicle, 7E: Simple gas engine ship, 7F: Simple gas engine airplane, 7G: Simple water injection engine ship, 7H: Simple injection engine airplane, 7d: Simple gas engine automobile, 7e: Simple gas engine ship, 7f: Simple gas engine ship Airplane, 7g: simple water injection engine ship, 7h: simple injection engine airplane, 7i: rotary wing airplane, 7j: rotary wing injection airplane, 7k: simple gas engine automobile, 7l: simple gas engine ship, 7m: simple gas engine airplane 7n: simple water injection 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 airplane, 7w: rotary wing airplane, 7x: rotary wing injection airplane, 7y: extra large Osprey, z: Large Osprey, 8c: Turbine blade (a straight long turbine blade is provided on the outer surface of the cylinder to aim for fully automatic machining and weight reduction of the inner and outer circumferences) 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 8A: Cylindrical turbine blade group (Fully automatic machining and precision assembly are possible as a horizontal cylindrical turbine blade group) 8S: Horizontal full blade turbine (opposite full blade impeller turbine series full blade impeller turbine full bite blade Bouncer turbine) 8S: Horizontal full-blade turbine (with straight long turbine blades on the outer surface of the cylinder, aiming for fully automatic machining and weight reduction of the inner and outer circumferences) 8S: Horizontal full-rotor water gravity turbine (existing steam turbine is static) Damping out with wings (8) Mine-type full blades are required to use all blades because the force approaches 0 and the work rate is as small as 1 / 360,000 of platinum spheres. Hydrogravity turbine (6 types of cylindrical turbine blade group fitting assembly + magnetic bearing load close to 0) 8N: Vertical type full blade ratio material gravity turbine (6 types of cylindrical turbine blade group fitting assembly + 8R: Horizontal type full-blade water gravity turbine (cylindrical turbine blade group serially opposed synchronous rotation + magnetic use bearing load close to 0) 8S: Horizontal type full blade ratio material gravity turbine (cylindrical) Turbine blade group series counter synchronous rotation + magnetic utilization bearing load close to 0) 8P: vertical-type all blade hydrogravity turbine (6 types of cylindrical turbine blade group fitting assembly + magnetic utilization bearing load approaching 0 + super high speed outer circumference) 8Q: Vertical type all blade specific gravity Mass Gravity Turbine (6 types of cylindrical turbine blade group fitting assembly + magnetic bearing load approach 0 + super high speed peripheral speed) 8T: Horizontal all blade water gravity turbine (cylindrical turbine blade group series opposed synchronous rotation + magnetism) 8U: Horizontal type full blade ratio material gravity turbine (cylindrical turbine blade group series opposed synchronous rotation + magnetic utilization bearing load 0 approach + super high speed peripheral speed) 9: Wear-resistant annular assembly (fitting assembly method for reducing the weight of specific critical material flow path including 8c with cemented carbide and reducing the weight) 9b: Upper attracting lower repulsion magnet, 9A: Cylindrical annular assembly (wear-resistant cylindrical annular assembly moving blade group 6 types make it simple structure, few parts, fully automatic processing, easy assembly, light weight, etc. 9A: Cylindrical ring assembly (entrance fixed outer blade 60E + outer annular blade 60G + outlet fixed outer blade 60J fitting) so Cylindrical outer blade group 60D, cylindrical portion that forms cylindrical inner blade group 60C by fitting inlet fixed inner blade 60F + inner annular blade 60H + outlet fixed inner blade 60K) 9B: repulsive permanent magnet, 9C: attractive permanent magnet , 9D: Compressed air section, 9E: Vacuum section, 9M: Fitting assembly section, 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 room, 16: Horizontal shaft plate (disc for facilitating precision assembly) 16A: Horizontal shaft, 11D: Gas cooling room, 21: Solar heater (intake air) 24: combustion gas control valve, 24A: compressed air control valve, 25: superheated steam control valve, 25b: fuel control valve, 25c: fuel pipe, 28a: air 28a: cold (empty 28a is compressed by a heat pump and divided into 50 heated superheated steam of compressed air calorie + compressed air 28a cold containing liquid oxygen and liquid nitrogen) 28b: calorie of compressed air, 28A: intake air channel, 28B: air channel inlet, 38: Rotating guide, 38a: Flight trunk, 38b: Flying wing, 38c: Flying tail, 38d: Vertical wing, 38e: Front wing center, 38g: Water wing, 38h: Levitation boat, 38B: Air suction jet ship ( 38S: 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 airplane, 39C: Solar thermal gravity helicopter, 39D: Screw ship, 39G: Solar thermal gravity ship, 3 9H: oxygen coalescence screw ship, 39J: oxygen coalescence injection ship, 39K: oxygen coalescence screw injection ship, 39L: oxygen coalescence injection airplane, 39M: oxygen coalescence propeller airplane, 39N: oxygen coalescence propeller injection airplane, 39P: oxygen coalescence rotor Airplane, 39Q: oxygen coalescence screw ship, 39R: oxygen coalescence injection ship, 39S: oxygen coalescence screw injection ship, 39T: oxygen coalescence injection airplane, 39U: oxygen coalescence propeller airplane, 40A: rudder, 49: combustion gas, 50: superheat Steam: 50: Superheated steam chamber, 50: Warmth (compressed air 28a is compressed by a heat pump and divided into 50 warm heat of compressed air heat + compressed air 28a cold storage) 50A: Steam, 50a: Superheated steam injection pipe, 51 : Air extractor 51: Merged extractor (extractor for joining) 51A: Air Exit 52a: Hot water 52a: Deep sea water 52b: Hot water 52d: Hot (change from 50) 52e: Cold (change from 28a) 55B: Transmission, 60A: Inner shaft device (turbine blade equipped device) 60B: Outer shaft device (equipment with turbine blade) 60C: Cylindrical inner blade group (Wear resistant cylindrical annular assembly fixed moving blade group including fully automatic machining easy assembly) 60D: Cylindrical outer blade group (wear resistance) 60E: Inlet fixed outer blade (inlet blade for annularly fixing the outer blade group) 60F: Inlet fixed inner blade (inner blade group) 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) Assemble the blade group 60K: Outlet fixed inner wing (exit wing for annular assembly fixing inner blade group) 60c: Inner blade, 60d: Outer 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 outer box, 77F: Outer box for injection, 77G: Cylindrical rotating part, 77a: Outer box for turbine, 77b: Outer box for compressor, 80: Bearing (including magnetic bearing + air bearing) 80a: Thrust bearing (including 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 combusted multiple times in 5M, 5N from the inner circumference and inner circumference outer circumference Heat and spray 80Z: Liquid air suction water jet (receives the high pressure / high temperature combustion chamber 5M, high pressure / high temperature steam chamber 5N, and injects and burns the fuel multiple times to 5M to generate 5N for the inner circumference and inner circumference outer circumference) And heated several times to inject, and fuel injection combustion injection to a plurality of locations of air suction flow, air suction injection and water suction injection) 84: Counter-rotating magnetic friction device (inner moving blade with fixed portion) 84Y: Counter-rotating gear device (same for existing technology) 85: Counter-rotating magnetic device (magnet gear using a slight height and no contact, horizontal) 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 : Easy gas machine 88f: Simple injection engine 88e: Simple water injection engine 88g: Liquid oxygen production machine 88l: Liquid oxygen production machine 88i: Simple gas engine 88j: Simple water injection engine 88k: Simple injection engine 88l: Liquid oxygen Manufacturing machine, 88m: Simple gas engine, 88n: Simple water injection engine, 88o: Simple injection engine, 88A: Oxygen combined air injection unit (rocket combustion + jet combustion + steam injection and combined injection) 88B: Oxygen combined air injection unit (Ultrahigh pressure rocket combustion + jet combustion + superheated steam injection suction) 88C: Theoretical air injection part, 88M: Theoretical water injection part, 88K: Oxygen coalescence water injection part (rocket coalescence + jet combustion + steam injection etc. coalescence injection) 88L : Oxygen combined water injection unit (super high pressure rocket combustion + jet combustion + superheated steam injection suction) 95a: combustion gas reservoir, 95b: compressed air reservoir 95c: Superheated steam reservoir, 103: Cold heat recovery device,

Claims (457)

  The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. A horizontal full rotor blade having a series of co-rotating gears (4D) between the horizontal shafts (16A) and rotating in the same direction in the same direction in the vertical direction so that the bearing load is close to 0 and the super-high speed circumferential speed is achieved. Specific energy gravitational turbine (8U) 1-20 sets of power generation electric product drive + both center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) drive coalescence various energy conservation cycle coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. A horizontal full rotor blade having a series of co-rotating gears (4D) between the horizontal shafts (16A) and rotating in the same direction in the same direction in the vertical direction so that the bearing load is close to 0 and the super-high speed circumferential speed is achieved. Specific energy gravitational turbine (8U) 21 to 40 generator electric product drive + both center support bearing load coalescence 0 approach counter rotating production compressed air (28a) drive coalescence various energy conservation cycle coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. A horizontal full rotor blade having a series of co-rotating gears (4D) between the horizontal shafts (16A) and rotating in the same direction in the same direction in the vertical direction so that the bearing load is close to 0 and the super-high speed circumferential speed is achieved. Specific energy gravitational turbine (8U) 41-60 sets of power generation electric product drive + both center support bearing load coalescence 0 approach counter rotating production compressed air (28a) drive coalescence various energy conservation cycle coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. A horizontal full rotor blade having a series of co-rotating gears (4D) between the horizontal shafts (16A) and rotating in the same direction in the same direction in the vertical direction so that the bearing load is close to 0 and the super-high speed circumferential speed is achieved. Specific energy gravitational turbine (8U) 61-80 sets of power generation electric product drive + both center support bearing load coalescence 0 approach counter rotating production compressed air (28a) drive coalescence various energy conservation cycle coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. A horizontal full rotor blade having a series of co-rotating gears (4D) between the horizontal shafts (16A) and rotating in the same direction in the same direction in the vertical direction so that the bearing load is close to 0 and the super-high speed circumferential speed is achieved. Specific energy gravitational turbine (8U) 81 to 100 sets of power generation electric product drive + both center support bearing load coalescence 0 approach counter rotating production compressed air (28a) drive coalescence various coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. A horizontal full rotor blade having a series of co-rotating gears (4D) between the horizontal shafts (16A) and rotating in the same direction in the same direction in the vertical direction so that the bearing load is close to 0 and the super-high speed circumferential speed is achieved. Specific energy gravitational turbine (8U) 101-120 generator electric product drive + both center support bearing load coalescence 0 approach counter rotating production compressed air (28a) drive coalescence various energy conservation cycle coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. A horizontal full rotor blade having a series of co-rotating gears (4D) between the horizontal shafts (16A) and rotating in the same direction in the same direction in the vertical direction so that the bearing load is close to 0 and the super-high speed circumferential speed is achieved. Specific energy gravitational turbine (8U) 121-140 generator power generation electric product drive + both center support bearing load coalescence 0 approach counter rotating production compressed air (28a) drive coalescence various energy conservation cycle coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. A horizontal full rotor blade having a series of co-rotating gears (4D) between the horizontal shafts (16A) and rotating in the same direction in the same direction in the vertical direction so that the bearing load is close to 0 and the super-high speed circumferential speed is achieved. Specific energy gravitational turbine (8U) 141 to 160 sets of power generation electric product drive + both center support bearing load coalescence 0 approach counter rotating production compressed air (28a) drive coalescence various energy conservation cycle coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. A horizontal full rotor blade having a series of co-rotating gears (4D) between the horizontal shafts (16A) and rotating in the same direction in the same direction in the vertical direction so that the bearing load is close to 0 and the super-high speed circumferential speed is achieved. Specific energy gravitational turbine (8U) 161-180 sets of power generation electric product drive + both center support bearing load coalescence 0 approach counter rotating production compressed air (28a) drive coalescence various energy conservation cycle coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. A horizontal full rotor blade having a series of co-rotating gears (4D) between the horizontal shafts (16A) and rotating in the same direction in the same direction in the vertical direction so that the bearing load is close to 0 and the super-high speed circumferential speed is achieved. Specific energy gravitational turbine (8U) 181 to 200 sets of power generation electric product drive + both center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) drive coalescence various coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. Magnetic bearing load that is provided with a series of same rotating gears (4D) between horizontal axes (16A), and is driven by injection with specific material (3E) Mach 1-30 by rotating in the same direction in the same vertical direction. Horizontal approaching blade ratio critical material gravity turbine (8U) 1-20 sets driven with zero approach + super high speed circumferential speed + both sides center support bearing load coalescence 0 approach counter rotating manufactured compressed air (28a) drive Various energy conservation cycle coalescence engines and coalescence methods for coalescence.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. Magnetic bearing load that is provided with a series of same rotating gears (4D) between horizontal axes (16A), and is driven by injection with specific material (3E) Mach 1-30 by rotating in the same direction in the same vertical direction. Horizontal approaching blade ratio critical material gravity turbine (8U) 21 to 40 sets of electric power product drive + close approach + super high speed circumferential speed + both sides center support bearing load coalescence 0 approach counter rotating manufactured compressed air (28a) drive Various energy conservation cycle coalescence engines and coalescence methods for coalescence.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. Magnetic bearing load that is provided with a series of same rotating gears (4D) between horizontal axes (16A), and is driven by injection with specific material (3E) Mach 1-30 by rotating in the same direction in the same vertical direction. Horizontal approaching blade ratio critical material gravity turbine (8U) 41-60 sets driven with zero approach + super high speed circumferential speed + both sides center support bearing load coalescence 0 approach counter rotating manufactured compressed air (28a) drive Various energy conservation cycle coalescence engines and coalescence methods for coalescence.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. Magnetic bearing load that is provided with a series of same rotating gears (4D) between horizontal axes (16A), and is driven by injection with specific material (3E) Mach 1-30 by rotating in the same direction in the same vertical direction. Horizontal all-blade ratio critical material gravity turbine (8U) 61-80 sets of power generation electrical product drive with 0 approach + super-high speed circumferential speed + both sides center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) drive Various energy conservation cycle coalescence engines and coalescence methods for coalescence.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. Magnetic bearing load that is provided with a series of same rotating gears (4D) between horizontal axes (16A), and is driven by injection with specific material (3E) Mach 1-30 by rotating in the same direction in the same vertical direction. Horizontal approaching blade ratio critical material gravity turbine (8U) 81 to 100 sets generating electric product drive with 0 approach + super high speed circumferential speed + both sides center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) drive Various energy conservation cycle coalescence engines and coalescence methods for coalescence.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. Magnetic bearing load that is provided with a series of same rotating gears (4D) between horizontal axes (16A), and is driven by injection with specific material (3E) Mach 1-30 by rotating in the same direction in the same vertical direction. Horizontal approaching blade ratio critical material gravity turbine (8U) 101-120 sets driven by 0 approach + ultra high speed circumferential speed + both sides center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) drive Various energy conservation cycle coalescence engines and coalescence methods for coalescence.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. Magnetic bearing load that is provided with a series of same rotating gears (4D) between horizontal axes (16A), and is driven by injection with specific material (3E) Mach 1-30 by rotating in the same direction in the same vertical direction. Horizontal approaching blade ratio critical material gravity turbine (8U) 121-140 set driven with zero approach + super high speed circumferential speed + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) drive Various energy conservation cycle coalescence engines and coalescence methods for coalescence.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. Magnetic bearing load that is provided with a series of same rotating gears (4D) between horizontal axes (16A), and is driven by injection with specific material (3E) Mach 1-30 by rotating in the same direction in the same vertical direction. Horizontal approaching blade ratio critical material gravity turbine (8U) 141-160 sets driven with zero approach + super high speed circumferential speed + Electric power product drive on both sides + Center support bearing load coalescence 0 approach contra-rotating production compressed air (28a) drive Various energy conservation cycle coalescence engines and coalescence methods for coalescence.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. Magnetic bearing load that is provided with a series of same rotating gears (4D) between horizontal axes (16A), and is driven by injection with specific material (3E) Mach 1-30 by rotating in the same direction in the same vertical direction. Horizontal approaching blade ratio critical material gravity turbine (8U) 161-180 sets driven to zero approach + super high speed circumferential speed + both sides center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) drive Various energy conservation cycle coalescence engines and coalescence methods for coalescence.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. Magnetic bearing load that is provided with a series of same rotating gears (4D) between horizontal axes (16A), and is driven by injection with specific material (3E) Mach 1-30 by rotating in the same direction in the same vertical direction. Horizontal approaching blade ratio critical material gravity turbine (8U) 181 to 200 sets driven by zero approach + super high speed circumferential speed + Electric power product drive of both sides + Double-side center support bearing load coalescence 0 approach counter rotating manufactured compressed air (28a) drive Various energy conservation cycle coalescence engines and coalescence methods for coalescence.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and a pair of vertical rotations in the same direction and rotation at the same speed, aiming at the specific material (3E) Mach 30 and the injection ratio material (2E). Mixed injection acceleration drive using magnetic bearing load 0 approach + ultra-high speed peripheral blade ratio critical material gravity turbine (8U) 1-20 sets generator electric product drive + both sides center support bearing load merge 0 approach 2 Various energy storage cycle coalescence engine and coalescence method for coalescence of heavy inversion manufactured compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and a pair of vertical rotations in the same direction and rotation at the same speed, aiming at the specific material (3E) Mach 30 and the injection ratio material (2E). Magnetically driven bearing load to drive mixed injection acceleration 0 + horizontal type full blade ratio material gravity turbine (8U) 21 to 40 sets driven by super high speed circumferential speed + both-side center support bearing load merge 0 approach 2 Various energy storage cycle coalescence engine and coalescence method for coalescence of heavy inversion manufactured compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and a pair of vertical rotations in the same direction and rotation at the same speed, aiming at the specific material (3E) Mach 30 and the injection ratio material (2E). Mixed magnetic-acceleration driven magnetic bearing load approaching 0 + ultra-high speed peripheral blade ratio critical material gravity turbine (8U) 41-60 sets power generation electric product drive + both sides center support bearing load union approaching 0 approach 2 Various energy storage cycle coalescence engine and coalescence method for coalescence of heavy inversion manufactured compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and a pair of vertical rotations in the same direction and rotation at the same speed, aiming at the specific material (3E) Mach 30 and the injection ratio material (2E). Mixed magnetic-acceleration driven magnetic bearing load approaching 0 + ultra-high speed peripheral blade ratio critical material gravity turbine (8U) 61-80 sets generator electric product drive + both-side center support bearing load combination approaching 0 approach 2 Various energy storage cycle coalescence engine and coalescence method for coalescence of heavy inversion manufactured compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and a pair of vertical rotations in the same direction and rotation at the same speed, aiming at the specific material (3E) Mach 30 and the injection ratio material (2E). Mixed injection acceleration driven magnetically utilized bearing load approaching 0 + ultra-high speed peripheral speed blades critical material gravity turbine (8U) 81-100 sets of power generation electric product drive + both sides center support bearing load combined approach 0 approach 2 Various energy storage cycle coalescence engines and coalescence methods for coalescence of heavy inversion manufactured compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and a pair of vertical rotations in the same direction and rotation at the same speed, aiming at the specific material (3E) Mach 30 and the injection ratio material (2E). Mixed magnetic-acceleration driven magnetic bearing load approaching 0 + ultra-high speed peripheral blade ratio critical material gravity turbine (8U) 101-120 set power generation electric product drive + both sides center support bearing load union approaching 0 approach 2 Various energy storage cycle coalescence engine and coalescence method for coalescence of heavy inversion manufactured compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and a pair of vertical rotations in the same direction and rotation at the same speed, aiming at the specific material (3E) Mach 30 and the injection ratio material (2E). Mixed magnetic-acceleration driven magnetically loaded bearing load approaching 0 + ultra-high speed circumferential speed blade-weighted critical material gravity turbine (8U) 121-140 set generator electric product drive + both sides center support bearing load combined approach 0 approach 2 Various energy storage cycle coalescence engine and coalescence method for coalescence of heavy inversion manufactured compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and a pair of vertical rotations in the same direction and rotation at the same speed, aiming at the specific material (3E) Mach 30 and the injection ratio material (2E). Mixed magnetic-acceleration driven magnetic bearing load approaching 0 + ultra-high speed peripheral blade ratio critical material gravity turbine (8U) 141-160 set generator electric product drive + both sides center support bearing load union approaching 0 approach 2 Various energy storage cycle coalescence engine and coalescence method for coalescence of heavy inversion manufactured compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and a pair of vertical rotations in the same direction and rotation at the same speed, aiming at the specific material (3E) Mach 30 and the injection ratio material (2E). Mixed magnetic-acceleration driven magnetic bearing load approaching 0 + ultra-high speed peripheral blade ratio critical material gravity turbine (8U) 161-180 set generator electric product drive + both-side center support bearing load combination approaching 0 approach 2 Various energy storage cycle coalescence engine and coalescence method for coalescence of heavy inversion manufactured compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and a pair of vertical rotations in the same direction and rotation at the same speed, aiming at the specific material (3E) Mach 30 and the injection ratio material (2E). Mixed magnetic-acceleration driven magnetic bearing load approaching 0 + ultra-high speed peripheral blade ratio critical material gravity turbine (8U) 181 to 200 sets generating electric product drive + both-side center support bearing load combined approach 0 approach 2 Various energy storage cycle coalescence engine and coalescence method for coalescence of heavy inversion manufactured compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , Equipped with a series rotation gear (4D) between the horizontal axes (16A) and rotating in the same direction in the same vertical direction, allowing cutting of the entire inner diameter. Peripheral all-blade ratio critical material gravity turbine (8U) 1 to 20 sets of power generation electric product drive + both center support bearing load coalescence 0 approach counter rotating production compressed air (28a) drive various energy Storage cycle coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , Equipped with a series rotation gear (4D) between the horizontal axes (16A) and rotating in the same direction in the same vertical direction, allowing cutting of the entire inner diameter. Horizontal full-blade ratio critical material gravity turbine (8U) 21 to 40 sets of power generation electric product drive + both sides center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) drive various energy Storage cycle coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , Equipped with a series rotation gear (4D) between the horizontal axes (16A) and rotating in the same direction in the same vertical direction, allowing cutting of the entire inner diameter. Horizontal full-blade ratio critical material gravity turbine (8U) 41-60 sets generating electric product drive + both sides center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) drive Storage cycle coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , Equipped with a series rotation gear (4D) between the horizontal axes (16A) and rotating in the same direction in the same vertical direction, allowing cutting of the entire inner diameter. Horizontal full-blade ratio critical material gravity turbine (8U) 61-80 sets generating electric product drive + both sides center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) drive various energy Storage cycle coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , Equipped with a series rotation gear (4D) between the horizontal axes (16A) and rotating in the same direction in the same vertical direction, allowing cutting of the entire inner diameter. Horizontal full-blade ratio critical material gravity turbine (8U) 81 to 100 sets of power generation electric product drive + both center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) drive Storage cycle coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , Equipped with a series rotation gear (4D) between the horizontal axes (16A) and rotating in the same direction in the same vertical direction, allowing cutting of the entire inner diameter. Horizontal full-blade ratio critical material gravity turbine (8U) 101-120 sets of peripheral electrical speeds Driven electric product drive + Double-sided center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) drive energy Storage cycle coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , Equipped with a series rotation gear (4D) between the horizontal axes (16A) and rotating in the same direction in the same vertical direction, allowing cutting of the entire inner diameter. Horizontal full-blade ratio critical material gravity turbine (8U) 121-140 sets driven by electric power product + both-side center support bearing load coalescence 0 approach counter rotating production compressed air (28a) drive various energy Storage cycle coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , Equipped with a series rotation gear (4D) between the horizontal axes (16A) and rotating in the same direction in the same vertical direction, allowing cutting of the entire inner diameter. Horizontal full-blade ratio critical material gravity turbine (8U) 141-160 sets of peripheral electric speeds Driven electric product drive + both center support bearing load coalescence 0 approach counter rotating production compressed air (28a) drive various energy Storage cycle coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , Equipped with a series rotation gear (4D) between the horizontal axes (16A) and rotating in the same direction in the same vertical direction, allowing cutting of the entire inner diameter. Horizontal all-blade ratio critical material gravity turbine (8U) 161-180 sets of peripheral electrical speeds Driven electric product drive + both sides center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) drive energy Storage cycle coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , Equipped with a series rotation gear (4D) between the horizontal axes (16A) and rotating in the same direction in the same vertical direction, allowing cutting of the entire inner diameter. Horizontal all-blade ratio critical material gravity turbine (8U) 181 to 200 sets of generator electric product drive + both sides center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) drive various energy Storage cycle coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , Equipped with a series rotation gear (4D) between the horizontal axes (16A), rotating in the same direction in the same vertical direction and rotating at the same speed, and cutting the entire inner diameter by spraying with specific material (3E) Mach 1-30 Largest experimental diameter using magnetic bearing load approaching 0 + ultra-high speed peripheral blade ratio critical material gravity turbine (8U) 1-20 sets generator electric product drive + double-sided center support bearing load combination 0 approaching double Various energy storage cycle merging engines and merging methods for merging driven inverted compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronized rotation , Equipped with a series rotation gear (4D) between the horizontal axes (16A), rotating in the same direction in the same vertical direction and rotating at the same speed, and cutting the entire inner diameter by spraying with specific material (3E) Mach 1-30 The maximum diameter of the magnetically utilized bearing load approaching zero + the horizontal full blade ratio critical material gravity turbine (8U) 21-40 sets driven by super high speed circumferential speed + both sides center support bearing load coalescence 0 approach double Various energy storage cycle merging engines and merging methods for merging driven inverted compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , Equipped with a series rotation gear (4D) between the horizontal axes (16A), rotating in the same direction in the same vertical direction and rotating at the same speed, and cutting the entire inner diameter by spraying with specific material (3E) Mach 1-30 The maximum diameter of the magnetic bearing used in the experiment is approaching zero + the super-high-speed circumferential speed of the full blade ratio critical material gravity turbine (8U) 41 to 60 sets of power generation electric product drive + both sides center support bearing combined load 0 approach double Various energy storage cycle merging engines and merging methods for merging driven inverted compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , Equipped with a series rotation gear (4D) between the horizontal axes (16A), rotating in the same direction in the same vertical direction and rotating at the same speed, and cutting the entire inner diameter by spraying with specific material (3E) Mach 1-30 Largest experimental diameter magnetic bearing load approaching 0 + ultra-high speed peripheral speed blades critical material gravity turbine (8U) 61-80 sets of power generation electric product drive + both sides center support bearing combined 0 approach double Various energy storage cycle merging engines and merging methods for merging driven inverted compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , Equipped with a series rotation gear (4D) between the horizontal axes (16A), rotating in the same direction in the same vertical direction and rotating at the same speed, and cutting the entire inner diameter by spraying with specific material (3E) Mach 1-30 Largest experimental diameter bearing using magnetic force 0 approach + ultra-high speed peripheral blade ratio critical material gravity turbine (8U) 81-100 sets of power generation electric product drive + both sides center support bearing load merge 0 approach double Various energy storage cycle merging engines and merging methods for merging driven inverted compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , Equipped with a series rotation gear (4D) between the horizontal axes (16A), rotating in the same direction in the same vertical direction and rotating at the same speed, and cutting the entire inner diameter by spraying with specific material (3E) Mach 1-30 Largest experimental diameter magnetic bearing load approaching 0 + ultra-high speed peripheral speed blades critical material gravity turbine (8U) 101-120 generator power generation electric product drive + double-sided center support bearing load coalescence 0 approach double Various energy storage cycle merging engines and merging methods for merging driven inverted compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , Equipped with a series rotation gear (4D) between the horizontal axes (16A), rotating in the same direction in the same vertical direction and rotating at the same speed, and cutting the entire inner diameter by spraying with specific material (3E) Mach 1-30 Largest experimental diameter magnetic bearing load approaching 0 + ultra-high speed peripheral speed blades critical material gravity turbine (8U) 121-140 set generator electric product drive + both sides center support bearing load coalescence 0 approach double Various energy storage cycle coalescing engines and coalescence methods for coalescence of inverted manufacturing compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , Equipped with a series rotation gear (4D) between the horizontal axes (16A), rotating in the same direction in the same vertical direction and rotating at the same speed, and cutting the entire inner diameter by spraying with specific material (3E) Mach 1-30 Largest experimentally used magnetic bearing load of 0 approach + horizontal full blade ratio critical material gravity turbine (8U) 141-160 sets driven by super high speed circumferential speed + both-side center support bearing load merge 0 approach double Various energy storage cycle merging engines and merging methods for merging driven inverted compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , Equipped with a series rotation gear (4D) between the horizontal axes (16A), rotating in the same direction in the same vertical direction and rotating at the same speed, and cutting the entire inner diameter by spraying with specific material (3E) Mach 1-30 Largest experimentally used magnetic bearing load of 0 approach + horizontal full-blade ratio critical material gravity turbine (8U) 161-180 sets driven by super high speed circumferential speed + both-side center support bearing load merge 0 approach double Various energy storage cycle merging engines and merging methods for merging driven inverted compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , Equipped with a series rotation gear (4D) between the horizontal axes (16A), rotating in the same direction in the same vertical direction and rotating at the same speed, and cutting the entire inner diameter by spraying with specific material (3E) Mach 1-30 The maximum diameter of the magnetically utilized bearing load approaching zero + the horizontal full blade ratio critical material gravity turbine (8U) 181 to 200 sets driven by super high speed circumferential speed + both sides center support bearing load coalescence 0 approach double Various energy storage cycle merging engines and merging methods for merging driven inverted compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and a pair of vertical rotations in the same direction and rotation at the same speed, aiming at the specific material (3E) Mach 30 and the injection ratio material (2E). Mixed injection acceleration driven inside diameter can be cut all the way Experiment using the maximum diameter magnetic bearing load close to 0 + ultra-high speed peripheral blade ratio critical material gravity turbine (8U) 1 to 20 sets of power generation electric product drive + both sides Center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) drive coalescence of various energy conservation cycle coalescence engines and coalescence methods.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and a pair of vertical rotations in the same direction and rotation at the same speed, aiming at the specific material (3E) Mach 30 and the injection ratio material (2E). Mixed jet acceleration driven inside diameter can be cut all the way Experiment using the maximum diameter magnetic bearing load close to 0 + ultra-high speed circumferential speed of all blades critical material gravity turbine (8U) 21 to 40 sets Driven electric product drive + both sides Center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) drive coalescence of various energy conservation cycle coalescence engines and coalescence methods.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and a pair of vertical rotations in the same direction and rotation at the same speed, aiming at the specific material (3E) Mach 30 and the injection ratio material (2E). Mixed injection acceleration driven inside diameter can be cut all the way Experiment using the maximum diameter magnetic bearing load close to 0 + ultra-high speed circumferential speed of all blades critical material gravity turbine (8U) 41-60 sets drive electric power product drive + both sides Center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) drive coalescence of various energy conservation cycle coalescence engines and coalescence methods.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and a pair of vertical rotations in the same direction and rotation at the same speed, aiming at the specific material (3E) Mach 30 and the injection ratio material (2E). Mixed injection acceleration driven inside diameter can be cut all the way Experiment using the maximum diameter magnetic bearing load close to 0 + ultra-high speed circumferential speed of all moving blade ratio critical material gravity turbine (8U) 61-80 sets power generation electric product drive + both sides Center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) drive coalescence of various energy conservation cycle coalescence engines and coalescence methods.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and a pair of vertical rotations in the same direction and rotation at the same speed, aiming at the specific material (3E) Mach 30 and the injection ratio material (2E). Mixed injection acceleration drive possible to cut the entire inner surface of the experiment. Use of the maximum diameter magnetic bearing load approaching 0 + ultra-high speed peripheral blade ratio critical material gravity turbine (8U) 81 to 100 sets of power generation electric product drive + both sides Center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) drive coalescence of various energy conservation cycle coalescence engines and coalescence methods.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and a pair of vertical rotations in the same direction and rotation at the same speed, aiming at the specific material (3E) Mach 30 and the injection ratio material (2E). Mixed injection acceleration driven inside diameter can be cut all the way Experiment using the maximum diameter magnetic bearing load approaching 0 + ultra-high speed peripheral blade ratio critical material gravity turbine (8U) 101-120 set generator electric product drive + both sides Center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) drive coalescence of various energy conservation cycle coalescence engines and coalescence methods.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and the same rotation speed in the same vertical direction in each pair, and the injection ratio critical substance (2E) with the aim of the specific critical substance (3E) Mach 30 Mixed injection acceleration driven inside diameter can be cut all the way Experiment using the maximum diameter magnetic bearing load approaching 0 + super high speed circumferential speed ratio of all blades critical gravity gravity turbine (8U) 121-140 set power generation electric product drive + both sides Center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) drive coalescence of various energy conservation cycle coalescence engines and coalescence methods.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and a pair of vertical rotations in the same direction and rotation at the same speed, aiming at the specific material (3E) Mach 30 and the injection ratio material (2E). Mixed injection acceleration drive possible to cut the entire inner diameter of the experiment. Use of the maximum diameter magnetic bearing load approaching 0 + ultra-high speed circumferential speed of all moving blades ratio critical material gravity turbine (8U) 141-160 set power generation electric product drive + both sides Center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) drive coalescence of various energy conservation cycle coalescence engines and coalescence methods.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and a pair of vertical rotations in the same direction and rotation at the same speed, aiming at the specific material (3E) Mach 30 and the injection ratio material (2E). Mixed injection acceleration driven inside diameter can be cut all-around Experiment using the maximum diameter magnetic bearing load close to 0 + ultra-high speed circumferential speed of all blades critical material gravity turbine (8U) 161-180 set power generation electric product drive + both sides Center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) drive coalescence of various energy conservation cycle coalescence engines and coalescence methods.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and a pair of vertical rotations in the same direction and rotation at the same speed, aiming at the specific material (3E) Mach 30 and the injection ratio material (2E). Mixed injection acceleration driven inside diameter can be cut all the way Experiment using the largest diameter magnetic bearing load close to 0 + ultra-high speed circumferential speed of all blades critical material gravity turbine (8U) 181 to 200 sets Driven electric product drive + both sides Center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) drive coalescence of various energy conservation cycle coalescence engines and coalescence methods.   Cylindrical turbine blade group (8A) with a horizontal shaft (16A) fixed on both sides by a horizontal shaft plate (16) as one set, and an opposed series full blade impeller turbine. Horizontal all-blade ratio critical material gravity turbine (8U) 1-20 sets of power generation electric product drive + double-sided center support bearing load coalescence 0 approach counter rotating production compressed air (28a) drive various energy conservation cycles Merger engine and merger method.   Cylindrical turbine blade group (8A) with a horizontal shaft (16A) fixed on both sides by a horizontal shaft plate (16) as one set, and an opposed series full blade impeller turbine. Horizontal all-blade ratio critical material gravity turbine (8U) 21 to 40 sets of power generation electrical product drive + double-sided center support bearing load coalescence 0 approach counter rotating production compressed air (28a) drive various energy conservation cycles Merger engine and merger method.   Cylindrical turbine blade group (8A) with a horizontal shaft (16A) fixed on both sides by a horizontal shaft plate (16) as one set, and an opposed series full blade impeller turbine. Horizontal all-blade ratio critical material gravity turbine (8U) 41-60 sets of power generation electric product drive + both center support bearing load coalescence 0 approach counter rotating production compressed air (28a) drive various energy conservation cycles Merger engine and merger method.   Cylindrical turbine blade group (8A) with a horizontal shaft (16A) fixed on both sides by a horizontal shaft plate (16) as one set, and an opposed series full blade impeller turbine. Horizontal all-blade ratio critical material gravity turbine (8U) 61-80 sets of power generation electric product drive + double-sided center support bearing load coalescence 0 approach counter rotating production compressed air (28a) drive various energy conservation cycles Merger engine and merger method.   Cylindrical turbine blade group (8A) with a horizontal shaft (16A) fixed on both sides by a horizontal shaft plate (16) as one set, and an opposed series full blade impeller turbine. Horizontal all-blade ratio critical material gravity turbine (8U) 81-100 sets of power generation electric product drive + double-sided center support bearing load coalescence 0 approach counter rotating production compressed air (28a) drive various energy conservation cycles Merger engine and merger method.   Cylindrical turbine blade group (8A) with a horizontal shaft (16A) fixed on both sides by a horizontal shaft plate (16) as one set, and an opposed series full blade impeller turbine. Horizontal all-blade ratio critical material gravity turbine (8U) 101-120 sets of power generation electrical product drive + double-sided center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) drive various energy conservation cycles Merger engine and merger method.   Cylindrical turbine blade group (8A) with a horizontal shaft (16A) fixed on both sides by a horizontal shaft plate (16) as one set, and an opposed series full blade impeller turbine. Horizontal all blade ratio material gravity turbine (8U) 121-140 sets of power generation electric product drive + double-sided center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) coalescence of various energy conservation cycles Merger engine and merger method.   Cylindrical turbine blade group (8A) with a horizontal shaft (16A) fixed on both sides by a horizontal shaft plate (16) as one set, and an opposed series full blade impeller turbine. Horizontal all-blade ratio critical material gravity turbine (8U) 141 to 160 sets of power generation electrical product drive + double-sided center support bearing load coalescence 0 approach counter rotating production compressed air (28a) drive various energy conservation cycles Merger engine and merger method.   Cylindrical turbine blade group (8A) with a horizontal shaft (16A) fixed on both sides by a horizontal shaft plate (16) as one set, and an opposed series full blade impeller turbine. Horizontal all-blade ratio critical material gravity turbine (8U) 161-180 sets of power generation electric product drive + double-sided center support bearing load coalescence 0 approach counter rotating production compressed air (28a) drive various energy conservation cycles Merger engine and merger method.   Cylindrical turbine blade group (8A) with a horizontal shaft (16A) fixed on both sides by a horizontal shaft plate (16) as one set, and an opposed series full blade impeller turbine. Horizontal type blade ratio critical material gravity turbine (8U) 181 to 200 sets of power generation electric product drive + double-sided center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) coalescence of various energy conservation cycles Merger engine and merger method.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a series full blade impeller turbine is used. Combined various energy conservation cycle to combine 1 to 20 sets of power generation electric product drive + both sides center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) drive Organization and coalescence method.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a series full blade impeller turbine is used. Horizontal full blade ratio critical material gravity turbine (8U) 21-40 sets of power generation electric product drive + double-sided center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) drive coalescence Organization and coalescence method.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a series full blade impeller turbine is used. Horizontal full blade ratio critical material gravity turbine (8U) 41-60 sets power generation electric product drive + both center support bearing load coalescence 0 approach counter rotating production compressed air (28a) drive coalescence various energy conservation cycle coalescence Organization and coalescence method.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a series full blade impeller turbine is used. Horizontal full blade ratio critical material gravity turbine (8U) 61-80 sets of power generation electric product drive + both center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) drive coalescence Organization and coalescence method.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a series full blade impeller turbine is used. Horizontal full blade ratio critical material gravity turbine (8U) 81-100 sets of power generation electrical product drive + double-sided center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) drive coalescence Organization and coalescence method.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a series full blade impeller turbine is used. Combined with various types of energy conservation cycle to combine the combined full-blade blade ratio critical material gravity turbine (8U) 101-120 generator electric product drive + double-side center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) drive Organization and coalescence method.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a series full blade impeller turbine is used. Horizontal full blade ratio critical material gravity turbine (8U) 121-140 set generator electric product drive + both center support bearing load coalescence 0 approach counter rotating production compressed air (28a) drive coalescence Organization and coalescence method.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a series full blade impeller turbine is used. Horizontal full blade ratio material gravity turbine (8U) 141-160 generator power generation electric product drive + both center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) drive coalescence Organization and coalescence method.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a series full blade impeller turbine is used. Horizontal full blade ratio material gravity turbine (8U) 161-180 sets of power generation electrical product drive + double-sided center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) drive coalescence Organization and coalescence method.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a series full blade impeller turbine is used. Horizontal full blade ratio critical material gravity turbine (8U) 181 to 200 sets of power generation electric product drive + both center support bearing load coalescence 0 approach counter rotating production compressed air (28a) drive coalescence Organization and coalescence method.   Cylindrical turbine blade group (8A) horizontal shaft (16A) fixed on both sides with horizontal shaft plate (16), one set of two, using a bite series full blade impeller turbine, approaching magnetic bearing load 0 approach + super high speed circumference Horizontal full-blade ratio critical material gravity turbine (8U) 1 to 20 sets of power generation electric product drive + double-side center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) drive various energy conservation Cycle coalescence engine and coalescence method.   Cylindrical turbine blade group (8A) horizontal shaft (16A) fixed on both sides with horizontal shaft plate (16), one set of two, using a bite series full blade impeller turbine, approaching magnetic bearing load 0 approach + super high speed circumference Horizontal full-blade ratio critical material gravity turbine (8U) 21 to 40 sets of power generation electrical product drive + double-sided center support bearing load coalescence 0 approach counter-rotating production Compressed air (28a) drive various energy conservation Cycle coalescence engine and coalescence method.   Cylindrical turbine blade group (8A) horizontal shaft (16A) fixed on both sides with horizontal shaft plate (16), one set of two, using a bite series full blade impeller turbine, approaching magnetic bearing load 0 approach + super high speed circumference Horizontal full-blade ratio critical material gravity turbine (8U) 41-60 sets of power generation electric product drive + double-sided center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) drive coalescence Cycle coalescence engine and coalescence method.   Cylindrical turbine blade group (8A) horizontal shaft (16A) fixed on both sides with horizontal shaft plate (16), one set of two, using a bite series full blade impeller turbine, approaching magnetic bearing load 0 approach + super high speed circumference Horizontal all-blade ratio critical material gravity turbine (8U) 61-80 sets of power generation electrical product drive + double-sided center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) drive various energy conservation Cycle coalescence engine and coalescence method.   Cylindrical turbine blade group (8A) horizontal shaft (16A) fixed on both sides with horizontal shaft plate (16), one set of two, using a bite series full blade impeller turbine, approaching magnetic bearing load 0 approach + super high speed circumference Various types of energy storage to combine the speed of the horizontal full-blade ratio critical material gravity turbine (8U) 81 to 100 sets of power generation electric product drive + double side center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) drive Cycle coalescence engine and coalescence method.   Cylindrical turbine blade group (8A) horizontal shaft (16A) fixed on both sides with horizontal shaft plate (16), one set of two, using a bite series full blade impeller turbine, approaching magnetic bearing load 0 approach + super high speed circumference Horizontal full-blade ratio critical material gravity turbine (8U) 101-120 sets of power generation electrical product drive + double-side center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) drive coalescence Cycle coalescence engine and coalescence method.   Cylindrical turbine blade group (8A) horizontal shaft (16A) fixed on both sides with horizontal shaft plate (16), one set of two, using a bite series full blade impeller turbine, approaching magnetic bearing load 0 approach + super high speed circumference Horizontal full-blade ratio critical material gravity turbine (8U) 121-140 sets generator electric product drive + double-sided center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) drive coalescence Cycle coalescence engine and coalescence method.   Cylindrical turbine blade group (8A) horizontal shaft (16A) fixed on both sides with horizontal shaft plate (16), one set of two, using a bite series full blade impeller turbine, approaching magnetic bearing load 0 approach + super high speed circumference Horizontal full-blade ratio critical material gravity turbine (8U) 141-160 sets of power generation electric product drive + double-sided center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) drive coalescence Cycle coalescence engine and coalescence method.   Cylindrical turbine blade group (8A) horizontal shaft (16A) fixed on both sides with horizontal shaft plate (16), one set of two, using a bite series full blade impeller turbine, approaching magnetic bearing load 0 approach + super high speed circumference Horizontal full-blade ratio critical material gravity turbine (8U) 161-180 sets of power generation electrical product drive + double-sided center support bearing load coalescence 0 approach counter-rotating production Compressed air (28a) drive various energy conservation Cycle coalescence engine and coalescence method.   Cylindrical turbine blade group (8A) horizontal shaft (16A) fixed on both sides with horizontal shaft plate (16), one set of two, using a bite series full blade impeller turbine, approaching magnetic bearing load 0 approach + super high speed circumference Horizontal full-blade ratio critical material gravity turbine (8U) 181 to 200 sets of power generation electrical product drive + double-side center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) drive coalescence Cycle coalescence engine and coalescence method.   Horizontally-moving blade ratio critical material gravity turbine (8U) extreme with solar heater (21) provided with buoyancy on the water surface and solar heated air with magnetic bearing load approaching 0 + super high speed circumferential speed Compressed one or more times with a simple compressor (3 s) driven by low-cost power generation, and heat-recovered liquid oxygen production machine (88 l) with a high-pressure high-temperature water heating pipe (5H) for each compression, Liquid energy cold heat + hot water to superheated steam heat supply equipment (3D) feed drive + double-sided center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) drive coalescence and various energy conservation cycle coalescence engines and coalescence methods.   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. Horizontally moving blade ratio critical material gravity turbine (8U) with zero approach + super high speed circumferential speed (8U) Compressed one or more times with a simple compressor (3s) of extremely inexpensive power generation electric drive, high pressure hot water for each compression Heat recovery liquid oxygen production machine (88 l) heat production with heating pipe (5H), electricity + liquid air cold heat + hot water to superheated steam temperature heat supply equipment (3D) feed drive + both sides center support bearing load coalescence approach 0 Various energy storage cycle coalescing engine and coalescence method for driving counter rotating manufactured compressed air (28a) drive coalescence.   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), a device for controlling rotation of sunlight at a right angle in the vertical direction, and a horizontal full-blade ratio critical material gravity with solar-heated air approaching a magnetic bearing load of 0 and an ultra-high speed circumferential speed. Turbine (8U) Extremely inexpensive power generation electric drive, simple compressor (3s) compressed one or more times, and at each compression heat recovery liquid oxygen production machine (88l) heat production with high pressure high temperature water heating pipe (5H) Electricity + Liquid air cooling + High temperature water to superheated steam temperature supply equipment (3D) Feed drive + Both sides center support bearing load coalescence 0 approaching counter-rotating manufactured compressed air (28a) drive coalescence Organization and coalescence method.   The solar heater (21) is provided with buoyancy on the water surface, and includes a rotation support part (4f) that controls rotation of the sunlight at a right angle from east to west, and includes a gear device (4d) and a roller (4e). ) As a cylindrical rotating part (77G), as a device for controlling rotation of the sunlight at a right angle in the vertical direction and as a device for controlling rotation at a right angle in the east-west direction by using buoyancy, the sunlight is linearly irradiated around the center of the heat absorption tube (4H). Horizontal type full blade ratio material gravity turbine (8U) with air (28a) maximum temperature, magnetic bearing load approaching 0 + super high speed circumferential speed Extremely inexpensive power generation Electric drive, simple compressor (3s) Compressed one or more times, and at each compression, heat recovery liquid oxygen production machine (88l) with a high-pressure high-temperature water heating pipe (5H) to produce electricity, electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D ) Feed drive + center support shaft on both sides Various energy saving cycles combined engine and coalescence process for the load coalesce 0 close counterrotating producing compressed air (28a) driven coalescence.   The solar heater (21) is provided with buoyancy on the water surface, and includes a rotation support part (4f) that controls rotation of the sunlight at a right angle from east to west, and includes a gear device (4d) and a roller (4e). ) As a cylindrical rotating part (77G), as a device for controlling rotation of the sunlight at a right angle in the vertical direction and as a device for controlling rotation at a right angle in the east-west direction by using buoyancy, the sunlight is linearly irradiated around the center of the heat absorption tube (4H). The air (28a) temperature is maximized, and the external air (28a) is also heated. Each air passage (28A) is a high temperature selective suction. Gravity turbine (8U) Extremely inexpensive power generation electric drive, compressed by simple compressor (3s) one or more times, heat recovery liquid oxygen production machine (88l) heat production by high pressure high temperature water heating pipe (5H) for each compression Electric + liquid air Hot + hot water - superheated steam heat supply facilities (3D) feed drive + sides center support bearing load united 0 close counterrotating producing compressed air (28a) various energy conservation cycle combined engine and coalescence process for the driving coalesce.   A horizontal full blade ratio gravity material gravity turbine (8U) with a solar heater (21) provided with a circular railroad on a flat ground and solar heated air with a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed Compressed one or more times with a simple compressor (3 s) of extremely inexpensive power generation electric drive, and heat-recovered liquid oxygen production machine (88 l) with a high-pressure high-temperature water heating pipe (5H) for each compression, + Liquid air cold heat + High temperature water to superheated steam heat supply equipment (3D) feed drive + Both-side center support bearing load coalescence 0 approaching counter-rotating manufactured compressed air (28a) drive coalescence and various energy conservation cycle coalescence engines and coalescence methods .   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. Horizontal all-blade ratio critical material gravity turbine (8U) with zero load approach + super high speed circumferential speed (8U) Compressed one or more times with a simple compressor (3s) of extremely inexpensive power generation electric drive, high pressure and high temperature for each compression Heat recovery liquid oxygen production machine (88l) heat production with water heating pipe (5H), electricity + liquid air cold heat + hot water to superheated steam temperature heat supply equipment (3D) feed drive + both sides center support bearing load combination 0 Various energy storage cycle coalescing engines and coalescence methods for close-inversion manufacturing compressed air (28a) drive coalescence.   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), it is a device that controls the rotation of sunlight at a right angle in the vertical direction. Gravity turbine (8U) Extremely inexpensive power generation electric drive, compressed by simple compressor (3s) one or more times, heat recovery liquid oxygen production machine (88l) heat production by high pressure high temperature water heating pipe (5H) for each compression Electricity + liquid air cooling + hot water to superheated steam temperature supply equipment (3D) feed drive + both sides center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) drive coalescence various energy storage cycles Merger engine and merger method.   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). Irradiated internal air (28a) maximum temperature, magnetically utilized bearing load approaching 0 + super-high speed circumferential speed horizontal full blade ratio critical material gravity turbine (8U) extremely low cost electric drive, simple compressor (3s ) 1 to several times, and at each compression, a heat recovery liquid oxygen production machine (88 l) is produced with a high-pressure high-temperature water heating pipe (5H), and electricity + liquid air cold heat + high-temperature water to superheated steam heat supply equipment (3D) Feed drive + both sides Various energy saving cycles combined engine and coalescence process for the support bearing load united 0 close counterrotating producing compressed air (28a) driven coalescence.   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 all-blade specific gravity with maximum magnetic bearing load approaching 0 + super high speed circumferential speed, with the highest temperature of the irradiated internal air (28a), and the external air (28a) also heating each air passage (28A) high temperature selective suction Large material gravity turbine (8U) Compressed one or more times with a simple compressor (3s) of extremely inexpensive power generation electric drive, heat recovery liquid oxygen production machine (88l) with high pressure high temperature water heating pipe (5H) for each compression Thermal production, electricity + Body air cold + hot water - superheated steam heat supply facilities (3D) feed drive + sides center support bearing load united 0 close counterrotating producing compressed air (28a) various energy conservation cycle combined engine and coalescence process for the driving coalesce.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Liquid oxygen (5K) receiving drive + both center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) driven various energy storage cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Liquid oxygen (5K) superheated steam (50) receiving drive + both center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) driven various energy storage cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Liquid oxygen (5K) superheated steam (50) is driven to receive a plurality of theoretical combustion chambers (4Q) + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) and various energy storage cycle coalescence engines Merge method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Liquid oxygen (5K) superheated steam (50) is supplied to multiple theoretical combustion chambers (4Q) combined drive + double-side center support bearing load combined 0 approaching counter-rotating manufactured compressed air (28a) combined energy storage cycle combined engine And coalescing method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Liquid oxygen (5K) superheated steam (50) is supplied to a plurality of theoretical combustion chambers (4Q) combined rocket combustion drive + both center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) various energy storage cycles Merger engine and merger method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Liquid oxygen (5K) superheated steam (50) is supplied to multiple theoretical combustion chambers (4Q) Combined rocket combustion additional drive + Both-side center support bearing load coalescence 0 approaching counter-rotating manufactured compressed air (28a) Various energy storage Cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Liquid oxygen (5K) superheated steam (50) is supplied to a plurality of theoretical combustion chambers (4Q) combined rocket combustion + jet combustion drive + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) drive Energy conservation cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Liquid oxygen (5K) superheated steam (50) is received by multiple rockets in the theoretical combustion chamber (4Q), and the others are jet-fired + both-side center support bearing load coalescence 0 approach counter-rotating manufactured compressed air (28a) is combusted Various energy storage cycle coalescence engines and coalescence methods.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Liquid oxygen (5K) superheated steam (50) is received in multiple theoretical combustion chambers (4Q) by rocket combustion, and other theoretical combustion chambers (4Q) are jet combustion + both-side center support bearing load coalescence 0 approach counter-rotating production Various energy storage cycle coalescence engine and coalescence method for burning compressed air (28a).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Liquid oxygen (5K) superheated steam (50) is received in multiple theoretical combustion chambers (4Q) by rocket combustion, and the other theoretical combustion chambers (4Q) are jet combustion driven + both-side center support bearing load merge 0 approach double reversal Manufacturing compressed air (28a) various energy storage cycle coalescing engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression (4Q) ultra high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air ( 28a) Various energy storage cycle coalescence engines and coalescence methods in which a simple gas engine (88m) is driven as a combustion to drive an automobile.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) super high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) combustion as simple gas engine (88m ) Various energy storage cycle coalescence engines and coalescence methods for driving and driving an automobile.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 approaching counter-rotating manufactured compressed air (28a) combustion as simple gas Various energy storage cycle coalescence engine and coalescence method for driving an engine (88m) and driving an automobile.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression (4Q) ultra high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air ( 28a) A simple gas engine (88m) drive generator (1) as a combustion, (1) Drive energy storage battery (1A), storage battery drive wheel (4J) rotating simple gas engine automobile (7r) various energy storage cycle coalescence engine and coalescence method .   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) super high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) combustion as simple gas engine (88m ) Drive generator (1) Various energy storage cycle coalescence engine and coalescence method for accumulating in the drive battery (1A) and driving the battery drive wheel (4J) rotating simple gas engine vehicle (7r).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 approaching counter-rotating manufactured compressed air (28a) combustion as simple gas Engine (88m) drive generator (1) Various energy storage cycle coalescence engine and coalescence method for accumulating power in the drive battery (1A) and driving the battery drive wheel (4J) rotating simple gas engine vehicle (7r).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression (4Q) ultra high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air ( 28a) A simple gas engine (88m) drive generator as combustion (1) Various energy to drive a simple gas engine car (7r) that can be stored in the drive storage battery (1A) and rotate the storage battery drive wheel (4J) and normal wheel Storage cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) super high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) combustion as simple gas engine (88m ) Drive generator (1) Various energy storage cycle coalescence engine and coalescence method for driving a simple gas engine vehicle (7r) capable of rotating in the battery drive wheel (4J) and normal wheel by accumulating in the drive battery (1A).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 approaching counter-rotating manufactured compressed air (28a) combustion as simple gas Engine (88m) drive generator (1) Various energy storage cycle coalescence engine and coalescence that drive in a storage battery (1A) and drive a simple gas engine vehicle (7r) capable of rotating the battery drive wheel (4J) and normal wheel Method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression (4Q) ultra high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air ( 28a) Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88m) as combustion and driving a simple gas engine automobile (7r).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression (4Q) ultra high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air ( 28a) Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88m) as combustion and driving a screw (7C) rotating ship.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) super high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) combustion as simple gas engine (88m ) Various energy storage cycle coalescence engine and coalescence method for driving and driving a screw (7C) rotating ship.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 approaching counter-rotating manufactured compressed air (28a) combustion as simple gas Various energy storage cycle coalescence engine and coalescence method for driving the engine (88m) and driving the screw (7C) rotating ship.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression (4Q) ultra high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air ( 28a) Various energy storage cycle coalescing engines and coalescence methods for driving a simple gas engine (88m) 1 to plural and driving a screw (7C) plural rotations as a combustion as a combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) super high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) combustion as simple gas engine (88m ) Various energy storage cycle coalescing engine and coalescence method for driving 1 to a plurality of screws and driving a screw (7C) a plurality of rotations.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 approaching counter-rotating manufactured compressed air (28a) combustion as simple gas Engines (88m) 1 to multiple energy storage cycle coalescing engines and coalescing methods for driving a plurality of screws and driving a screw (7C) for multiple rotations.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression (4Q) ultra high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air ( 28a) Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88m) 1 to a plurality of cylinders as combustion and driving a screw (7C) multiple rotation simple gas engine ship (7s).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) super high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) combustion as simple gas engine (88m ) Various energy storage cycle coalescing engine and coalescence method for driving 1 to plural and driving screw (7C) multi-turn simple gas engine ship (7s).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 approaching counter-rotating manufactured compressed air (28a) combustion as simple gas Engines (88m) 1 to multiple energy storage cycle coalescing engines and coalescence methods for driving a plurality of screws (7C) and a multi-turn simple gas engine ship (7s).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression (4Q) ultra high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air ( 28a) Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88m) as combustion and driving a simple gas engine ship (7s).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression (4Q) ultra high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air ( 28a) Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88m) as combustion and driving an injection propulsion ship such as a screw (7C) rotating simple water injection engine (88n).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) super high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) combustion as simple gas engine (88m ) Various energy storage cycle coalescence engines and coalescence methods for driving and driving propulsion vessels such as screw (7C) rotating simple water injection engine (88n).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 approaching counter-rotating manufactured compressed air (28a) combustion as simple gas Various energy storage cycle coalescence engine and coalescence method for driving the engine (88m) and driving the propulsion vessel such as screw (7C) rotating simple water injection engine (88n).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression (4Q) ultra high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air ( 28a) Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88m) 1 to a plurality of combustion and driving an injection propulsion ship such as a screw (7C) multiple rotation simple water injection engine (88n).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) super high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) combustion as simple gas engine (88m 1) Various energy storage cycle coalescence engines and coalescence methods that drive one or more and drive a propulsion vessel such as a screw (7C) multiple rotation simple water injection engine (88n).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 approaching counter-rotating manufactured compressed air (28a) combustion as simple gas Various energy storage cycle coalescing engines and coalescence methods for driving the engine (88m) 1 to plural and driving the propulsion vessel such as a screw (7C) multi-turn simple water injection engine (88n).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression (4Q) ultra high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air ( 28a) Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88m) 1 to a plurality of combustion and driving an injection propulsion screw injection vessel such as a screw (7C) multiple rotation simple water injection engine (88n).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) super high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) combustion as simple gas engine (88m 1) Various energy storage cycle coalescence engines and coalescence methods that drive one or more and drive a screw (7C) multiple rotation simple water injection engine (88n), etc.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 approaching counter-rotating manufactured compressed air (28a) combustion as simple gas Various energy storage cycle coalescence engines and coalescence methods for driving the engine (88m) 1 to plural and driving the screw (7C) multi-turn simple water injection engine (88n), etc.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression (4Q) ultra high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air ( 28a) Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88m) as combustion and driving an injection propulsion screw injection ship such as a simple water injection engine (88n).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression. Multi-high pressure fuel combustion injection propulsion + Double-sided center support bearing load coalescence 0 approaching counter-rotating production Various energy storage cycle coalescing engine and coalescence method for driving a propulsion propulsion ship such as a simple water injection engine (88n) combusted with compressed air (28a).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Easy to receive cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) multiple ultra high pressure fuel combustion injection propulsion + both sides center support bearing load coalescence 0 approaching counter-rotating manufactured compressed air (28a) combustion Various energy storage cycle coalescence engine and coalescence method for driving an injection propulsion ship such as a water injection engine (88n).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) multiple ultra high pressure fuel combustion injection propulsion + both sides center support bearing load coalescence 0 approach counter-rotating manufactured compressed air (28a) combustion Various energy storage cycle coalescence engines and coalescence methods for driving an injection propulsion ship such as a simple water injection engine (88n).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression. Various energy storage cycle coalescence engines and coalescence methods for driving an injection propulsion ship such as a simple water injection engine (88n) with zero-commutated counter-rotating manufactured compressed air (28a) combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Received cheaper liquid oxygen (5K) + electricity, equipped with theoretical combustion chamber (4Q) air suction channel, multiple ultra-high pressure fuel combustion injection propulsion + both-side center support bearing load coalescence 0 approach counter-rotating manufactured compressed air ( 28a) Various energy storage cycle coalescence engines and coalescence methods for driving an injection propulsion ship such as a simple water injection engine (88n) as a combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) equipped with air suction flow path, multiple ultra high pressure fuel combustion injection propulsion + both sides center support bearing load coalescence 0 approach double reversal manufacturing Various energy storage cycle coalescing engine and coalescence method for driving a propulsion propulsion ship such as a simple water injection engine (88n) combusted with compressed air (28a).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression. Various energy storage cycle coalescing engines and coalescence methods for driving a simple water injection engine (88n), such as a simple water injection engine (88n) combustion (0u), and a ship (7u) with 0 approaching counter-rotating production compressed air (28a).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Received cheaper liquid oxygen (5K) + electricity, equipped with theoretical combustion chamber (4Q) air suction channel, multiple ultra-high pressure fuel combustion injection propulsion + both-side center support bearing load coalescence 0 approach counter-rotating manufactured compressed air ( 28a) A simple water injection engine (88n), such as a combustion, and an injection propulsion simple water injection engine ship (7u).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) equipped with air suction flow path, multiple ultra high pressure fuel combustion injection propulsion + both sides center support bearing load coalescence 0 approach double reversal manufacturing Various energy storage cycle coalescing engine and coalescence method for driving a simple water injection engine (88n), such as a compressed water (28a) combustion, and a simple water injection engine ship (7u).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression + both sides center support bearing load coalescence 0 approach counter-rotating manufactured compressed air (28a) combustion Various energy storage cycle coalescence engines and coalescence methods for driving a simple water injection engine (88n), etc., and a simple water injection engine ship (7u).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression. Multi-high pressure fuel combustion injection propulsion + Double-sided center support bearing load coalescence 0 approaching counter-rotating production Various energy storage cycle coalescing engines and coalescence methods for making a simple injection engine (88o) injection propulsion airplane with compressed air (28a) combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Easy to receive cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) multiple ultra high pressure fuel combustion injection propulsion + both sides center support bearing load coalescence 0 approaching counter-rotating manufactured compressed air (28a) combustion Various energy conservation cycle coalescence engine and coalescence method for making an injection engine (88o) jet propulsion airplane.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) multiple ultra high pressure fuel combustion injection propulsion + both sides center support bearing load coalescence 0 approach counter-rotating manufactured compressed air (28a) combustion Various energy storage cycle coalescing engine and coalescence method to make a simple injection engine (88o) injection propulsion airplane.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression. Various energy storage cycle coalescing engine and coalescence method to make a simple injection engine (88o) injection propulsion airplane with zero approaching counter-rotating manufactured compressed air (28a) combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Received cheaper liquid oxygen (5K) + electricity, equipped with theoretical combustion chamber (4Q) air suction channel, multiple ultra-high pressure fuel combustion injection propulsion + both-side center support bearing load coalescence 0 approach counter-rotating manufactured compressed air ( 28a) Combustion simple injection engine (88o) Various energy storage cycle coalescence engine and coalescence method for making an injection propulsion airplane.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) equipped with air suction flow path, multiple ultra high pressure fuel combustion injection propulsion + both sides center support bearing load coalescence 0 approach double reversal manufacturing Various energy storage cycle coalescing engines and coalescence methods for making a simple injection engine (88o) injection propulsion airplane with compressed air (28a) combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression. Various energy storage cycle coalescence engine and coalescence method for driving a simple injection engine (88o) injection propelled simple injection engine airplane (7v) with zero approaching counter-rotating production compressed air (28a) combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Received cheaper liquid oxygen (5K) + electricity, equipped with theoretical combustion chamber (4Q) air suction channel, multiple ultra-high pressure fuel combustion injection propulsion + both-side center support bearing load coalescence 0 approach counter-rotating manufactured compressed air ( 28a) Combustion simple injection engine (88o) injection propulsion simple injection engine airplane (7v) various energy storage cycle coalescence engine and coalescence method to drive.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) equipped with air suction flow path, multiple ultra high pressure fuel combustion injection propulsion + both sides center support bearing load coalescence 0 approach double reversal manufacturing A simple injection engine (88o) that uses compressed air (28a) combustion, a simple injection engine, a plane (7v), and various energy storage cycle combination engines and a combination method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression + both sides center support bearing load coalescence 0 approach counter-rotating manufactured compressed air (28a) combustion The simple injection engine (88o) injection propulsion simple injection engine airplane (7v) various energy storage cycle coalescence engine and the coalescence method to drive.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression (4Q) ultra high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air ( 28a) Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88m) as combustion and driving a propeller (7A) rotating airplane.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) super high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) combustion as simple gas engine (88m ) Various energy storage cycle merging engines and merging methods for driving and propeller (7A) rotating airplane drive.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 approaching counter-rotating manufactured compressed air (28a) combustion as simple gas Various energy storage cycle coalescing engine and coalescence method for driving the engine (88m) and driving the propeller (7A) rotating airplane.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression (4Q) ultra high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air ( 28a) Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88m) 1 to multiple propellers (7A) to drive a multi-turn airplane as combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) super high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) combustion as simple gas engine (88m 1) Various energy storage cycle coalescing engine and coalescence method for driving 1 to plural and propeller (7A) plural rotating airplanes.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 approaching counter-rotating manufactured compressed air (28a) combustion as simple gas Various energy storage cycle coalescence engines and coalescence methods for driving a plurality of engines (88m) 1 to propellers (7A) to drive a plurality of rotating airplanes.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression (4Q) ultra high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air ( 28a) Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88m) 1 to a plurality of combustion propellers (7A) and a multi-turn simple gas engine airplane (7t) as combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) super high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) combustion as simple gas engine (88m 1) Various energy storage cycle coalescing engine and coalescence method for driving 1 to plural and propeller (7A) plural rotation simple gas engine airplane (7t).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 approaching counter-rotating manufactured compressed air (28a) combustion as simple gas Various energy storage cycle coalescing engine and coalescence method for driving the engine (88m) 1 to plural and driving the propeller (7A) multiple rotation simple gas engine airplane (7t).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression (4Q) ultra high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air ( 28a) Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88m) as combustion and driving a propeller (7A) rotating simple gas engine airplane (7t).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression (4Q) ultra high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air ( 28a) A simple gas engine (88m) driven rotor blade (7B) for combustion and various energy storage cycle coalescing engines and coalescence methods that rotate and drive an airplane.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) super high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) combustion as simple gas engine (88m ) Driven rotary blade (7B) Various energy storage cycle coalescing engine and coalescence method for rotating and driving an airplane.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 approaching counter-rotating manufactured compressed air (28a) combustion as simple gas Engine (88m) driven rotor blade (7B) Various energy storage cycle coalescing engine and coalescence method for rotating and driving an airplane.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression (4Q) ultra high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air ( 28a) A simple gas engine (88m) 1 to a plurality of driving rotor blades (7B) as combustion, and various energy storage cycle coalescing engines and coalescence methods for driving the airplane by plural revolutions.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) super high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) combustion as simple gas engine (88m 1) Multiple drive rotor blades (7B) Various energy storage cycle coalescence engines and coalescence methods that drive the aircraft by multiple revolutions.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 approaching counter-rotating manufactured compressed air (28a) combustion as simple gas Engine (88m) 1-Plural drive rotor blades (7B) Various energy storage cycle coalescing engine and coalescence method for driving an airplane by plural revolutions.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression (4Q) ultra high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air ( 28a) Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88m) 1 to a multi-drive rotor blade (7B) and driving a rotor-wing airplane (7w) as a combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) super high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) combustion as simple gas engine (88m ) 1 to multiple drive rotor blades (7B) various energy storage cycle coalescing engines and coalescence methods for driving the rotor blade airplane (7w) with multiple rotations.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 approaching counter-rotating manufactured compressed air (28a) combustion as simple gas Engines (88m) 1 to multiple drive rotor blades (7B) various energy storage cycle coalescence engines and coalescence methods for driving the rotor blade airplane (7w) by multiple rotations.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression (4Q) ultra high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air ( 28a) Various energy storage cycle coalescence engines and coalescence methods for rotating a simple gas engine (88m) driving rotor blade (7B) and driving a rotor blade airplane (7w) as combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression (4Q) ultra high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air ( 28a) A simple gas engine (88m) drive propeller (7A) as a combustion, and a simple injection engine (88o) injection propulsion airplane driving various energy storage cycle coalescence engines and coalescence methods.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) super high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) combustion as simple gas engine (88m ) Driving propeller (7A) Rotating and simple injection engine (88o) Injection propulsion airplane driving various energy storage cycle merging engine and merging method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 approaching counter-rotating manufactured compressed air (28a) combustion as simple gas Engine (88m) driven propeller (7A), simple injection engine (88o) various types of energy storage cycle coalescence engine and coalescence method for driving an injection propulsion airplane.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression (4Q) ultra high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air ( 28a) A simple gas engine (88m) 1 to a multiple drive propeller (7A) as a combustion, a simple injection engine (88o) various propulsion engines and a combination method for driving an injection propulsion airplane.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) super high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) combustion as simple gas engine (88m 1) Multi-drive propeller (7A) Multi-rotation simple injection engine (88o) Various energy storage cycle coalescence engine and coalescence method for driving an injection propulsion airplane.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 approaching counter-rotating manufactured compressed air (28a) combustion as simple gas Engine (88m) 1 -multiple drive propeller (7A) various rotations simple energy injection engine (88o) various types of energy storage cycle coalescence engine and coalescence method for driving a propulsion airplane.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression (4Q) ultra high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air ( 28a) Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88m) 1 to a multiple drive propeller (7A) as a combustion and driving a simple injection engine (88o) injection propulsion simple gas engine airplane (7t) and the like.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) super high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) combustion as simple gas engine (88m 1) Plural drive propellers (7A) Simple rotation engine (88o) Injection propulsion simple gas engine airplane (7t) and other various energy storage cycle coalescence engines and coalescence methods.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 approaching counter-rotating manufactured compressed air (28a) combustion as simple gas Engine (88m) 1-Plural drive propeller (7A) Various energy storage cycle coalescence engine and coalescence method for driving a plurality of rotations and driving simple injection engine (88o) injection propulsion simple gas engine airplane (7t) and the like.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression (4Q) ultra high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air ( 28a) Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88m) driving propeller (7A) as combustion and driving a simple injection engine (88o) injection propulsion simple gas engine airplane (7t) and the like.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression (4Q) ultra high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air ( 28a) Various energy storage cycle coalescence engines and coalescence methods in which combustion is performed and high pressure high temperature combustion gas (5M) is injected to drive a simple gas engine (88m).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double side center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) combustion, high pressure high temperature combustion gas Various energy storage cycle coalescence engines and coalescence methods for injecting (5M) and driving a simple gas engine (88 m).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) combustion, high pressure Various energy storage cycle coalescence engine and coalescence method for driving a simple gas engine (88m) by injecting high-temperature combustion gas (5M).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression (4Q) ultra high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air ( 28a) Various energy storage cycle coalescence engines and coalescence methods driven by a simple gas engine (88m) that injects high pressure and high temperature combustion gas (5M) and inverts the horizontal axis (1h).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double side center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) combustion, high pressure high temperature combustion gas Various energy storage cycle coalescing engine and coalescence method driven by a simple gas engine (88m) that injects (5M) and inverts horizontally (1h).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) combustion, high pressure Various energy storage cycle coalescence engine and coalescence method driven by a simple gas engine (88m) in which high temperature combustion gas (5M) is injected and the horizontal axis (1h) is double-reversed.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression (4Q) ultra high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air ( 28a) Various energy storage cycle coalescence engines and coalescence methods in which combustion is performed and high-pressure high-temperature combustion gas (5M) is injected and the horizontal axis (1h) is driven by a plurality of contra-rotating simple gas engines (88m).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double side center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) combustion, high pressure high temperature combustion gas Various energy storage cycle coalescence engine and coalescence method in which (5M) is injected to drive a horizontal gas (1h) double inversion multiple simple gas engines (88m).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) combustion, high pressure Various energy storage cycle coalescence engine and coalescence method in which high temperature combustion gas (5M) is injected to drive a plurality of simple gas engines (88m) with a horizontal axis (1h) counter-rotating.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression (4Q) ultra high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air ( 28a) Various energy storage cycle coalescence engines and coalescence methods in which combustion is performed and high-pressure high-temperature combustion gas (5M) is injected and the horizontal axis (1h) is driven by a plurality of contra-rotating simple gas engines (88m).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression (4Q) ultra high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air ( 28a) Various energy storage cycle coalescing engines and coalescence methods for making a simple gas engine (88m) as combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) super high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) combustion as simple gas engine (88m ) Various energy conservation cycle coalescence engines and coalescence methods.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 approaching counter-rotating manufactured compressed air (28a) combustion as simple gas Various energy conservation cycle coalescing engines and coalescence methods for an engine (88 m).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression (4Q) ultra high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air ( 28a) Various energy storage cycle coalescing engines and coalescing methods for a simple gas engine (88m) that maximizes combustion speed.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Easy to receive cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) combustion to maximum speed Various energy storage cycle coalescence engine and coalescence method for gas engine (88m).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) super high pressure fuel combustion + both sides center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) combustion maximum speed Various energy storage cycle coalescence engine and coalescence method to make a simple gas engine (88m).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression (4Q) ultra high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air ( 28a) Various energy storage cycle coalescing engines and coalescing methods for a simple gas engine (88m) with maximum driving speed for combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) combustion to maximum driving speed Various energy storage cycle coalescence engine and coalescence method to make simple gas engine (88m).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double-sided center support bearing load coalescence 0 approaching counter-rotating manufactured compressed air (28a) maximum drive Various energy storage cycle coalescence engine and coalescence method to make the speed simple gas engine (88m).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression (4Q) ultra high pressure fuel combustion + both-side center support bearing load coalescence 0 approach counter-rotating production compressed air ( 28a) Various energy storage cycle coalescing engines and coalescing methods for a simple gas engine (88m) that achieves the highest speed for combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion that receives cheaper liquid oxygen (5K), compresses liquid fuel (1c) and water (52a) with liquid, and compresses the compressed volume with air compression 21/60000 volume, etc. Chamber (4Q) + both center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) Combustion various energy storage cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, liquid fuel (1c) and water (52a) are compressed with liquid, and the compression volume is burned by ultra high pressure compression fuel injection with air compression of 21/60000 volume, etc. Theoretical combustion chamber (4Q) + both center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) combustion, various energy storage cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, liquid fuel (1c) and water (52a) are compressed with liquid, compression volume is 21/60000 volume of air compression, etc. Ultra high pressure compressed fuel Theoretical combustion chamber (4Q) for injection combustion + both center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) Combustion engine for various energy storage cycles and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K), liquid fuel (1c) and water (52a) are compressed with liquid and heated to the optimum temperature on the inner wall of the theoretical combustion chamber (4Q) Various energy storage cycle coalescing engine and coalescence method for burning counter-rotating manufactured compressed air (28a).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Less expensive liquid oxygen (5K) + electricity is received, liquid fuel (1c) and water (52a) are compressed with liquid and heated to the optimum temperature on the inner wall of the theoretical combustion chamber (4Q) Various energy storage cycle coalescing engine and coalescence method for burning 0 approaching counter-rotating manufactured compressed air (28a).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, compressing liquid fuel (1c) and water (52a) with liquid and heating them to the optimum temperature on the inner wall of the theoretical combustion chamber (4Q) + center support on both sides Bearing load coalescence 0 approaching counter-rotating production compressed air (28a) burning various energy storage cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K), liquid fuel (1c) and water (52a) are compressed with liquid and heated to the optimum temperature on the inner wall of the theoretical combustion chamber (4Q) Various energy storage cycle coalescence engines and coalescence methods that open the contra-rotating manufactured compressed air (28a) combustion oxygen injection nozzle (6L) + fuel injection nozzle (6X) + superheated steam injection nozzle (6A).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Less expensive liquid oxygen (5K) + electricity is received, liquid fuel (1c) and water (52a) are compressed with liquid and heated to the optimum temperature on the inner wall of the theoretical combustion chamber (4Q) Various energy storage cycle coalescence engines and coalescence methods that open zero approaching counter-rotating manufactured compressed air (28a) combustion oxygen injection nozzle (6L) + fuel injection nozzle (6X) + superheated steam injection nozzle (6A).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, compressing liquid fuel (1c) and water (52a) with liquid and heating them to the optimum temperature on the inner wall of the theoretical combustion chamber (4Q) + center support on both sides Bearing load coalescence 0 approaching counter-rotating production 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.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) + hot water, compress liquid fuel (1c) and water (52a) with liquid and heat them to the optimum temperature on the inner wall of the theoretical combustion chamber (4Q) + Both-side center support bearing load Combined zero approaching counter-rotating production Compressed air (28a) Combustion oxygen injection nozzle (6L) + Fuel injection nozzle (6X) + Superheated steam injection nozzle (6A) together with open received superheated steam Method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K), open heated oxygen injection nozzle (6L) + fuel injection nozzle (6X) + superheated steam injection nozzle (6A) to the optimum temperature + heat superheated steam (50) + both sides Center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) Two types of theoretical combustion chambers (4Q) to burn various energy storage cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) + electricity, open heated oxygen injection nozzle (6L) + fuel injection nozzle (6X) + superheated steam injection nozzle (6A) to the optimum temperature + heat superheated steam (50) + Both-side center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) Various energy storage cycle coalescence engine and coalescence method to make two kinds of theoretical combustion chambers (4Q) to burn.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) + electricity + hot water, open heated oxygen injection nozzle (6L) + fuel injection nozzle (6X) + superheated steam injection nozzle (6A) to the optimum temperature + superheated steam (50 ) Is heated + both-side center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) Two kinds of theoretical combustion chambers (4Q) to burn various energy storage cycle coalescence engines and coalescence methods.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K), open heated oxygen injection nozzle (6L) + fuel injection nozzle (6X) + superheated steam injection nozzle (6A) to the optimum temperature + heated superheated steam (50) to high temperature + Double-sided center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) Combustion 2 types of theoretical combustion chamber (4Q) Various energy conservation cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) + electricity, open heated oxygen injection nozzle (6L) + fuel injection nozzle (6X) + superheated steam injection nozzle (6A) to the optimum temperature + heat superheated steam (50) High temperature + Both sides center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) Combustion 2 types of theoretical combustion chamber (4Q) Various energy storage cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) + electricity + hot water, open heated oxygen injection nozzle (6L) + fuel injection nozzle (6X) + superheated steam injection nozzle (6A) to the optimum temperature + superheated steam (50 ) Is heated to high temperature + both-side center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) combustion 2 types of theoretical combustion chamber (4Q) various energy storage cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K), open heated oxygen injection nozzle (6L) + fuel injection nozzle (6X) + superheated steam injection nozzle (6A) to the optimum temperature + heat superheated steam (50) + Both-side center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) Combustion 2 types of theoretical combustion chamber (4Q) Various energy storage cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) + electricity, open heated oxygen injection nozzle (6L) + fuel injection nozzle (6X) + superheated steam injection nozzle (6A) to the optimum temperature + heat superheated steam (50) + Double-sided center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) Combustion 2 types of theoretical combustion chamber (4Q) Various energy conservation cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) + electricity + hot water, open heated oxygen injection nozzle (6L) + fuel injection nozzle (6X) + superheated steam injection nozzle (6A) to the optimum temperature + superheated steam (50 ) + Both sides center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) Combustion 2 types of theoretical combustion chamber (4Q) various energy storage cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + hot water, open heated oxygen injection nozzle (6L) + fuel injection nozzle (6X) + superheated steam injection nozzle (6A) to the optimum temperature. Heating the peripheral superheated steam (50) including the received superheated steam by combustion at ℃ or more + Double-sided center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) Combustion 2 types of theoretical combustion chamber (4Q) Merger engine and merger method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K), high-pressure high-temperature combustion gas (5M) with a plurality of theoretical combustion chambers (4Q) injection acceleration injection + both center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a ) Various energy storage cycle coalescing engines and coalescing methods in a simple water injection engine (88n) for combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Received cheaper liquid oxygen (5K) + electricity, high pressure high temperature combustion gas (5M) injection accelerated injection with multiple theoretical combustion chambers (4Q) + both sides center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) Various energy storage cycle coalescing engines and coalescing methods in a simple water injection engine (88n) for combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, high-pressure high-temperature combustion gas (5M) injection acceleration injection with multiple theoretical combustion chambers (4Q) + double-side center support bearing load coalescence 0 approach double reversal Various energy storage cycle coalescing engine and coalescence method in a simple water injection engine (88n) for combustion of compressed air (28a) manufactured.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) and use high pressure high temperature combustion gas (5M) with multiple theoretical combustion chambers (4Q) (4Q) oxygen + fuel + superheated steam on the inner wall + Both energy saving cycle coalescence engine and coalescence method for a simple water injection engine (88n) that burns compressed air (28a) burning on both sides center support bearing load coalescence 0 approaching counter-rotating production.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, and heating the oxygen + fuel + superheated steam on the inner wall (4Q) with high pressure and high temperature combustion gas (5M) with multiple theoretical combustion chambers (4Q) Use + both center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) various energy storage cycle coalescing engine and coalescence method for burning simple water injection engine (88n).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, high pressure high temperature combustion gas (5M) with multiple theoretical combustion chambers (4Q) (4Q) inner wall oxygen + fuel + superheated steam at optimum temperature Heating and use + both center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) various energy storage cycle coalescence engine and coalescence method for simple water injection engine (88n) burning.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K), (4Q) oxygen + fuel + superheated steam on the inner wall with high pressure high temperature combustion gas (5M) with multiple theoretical combustion chambers (4Q) Various energy storage cycle coalescence engines and coalescence methods in the form of a simple water injection engine (88n) for theoretical combustion chamber (4Q) combustion + both center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, and heating the oxygen + fuel + superheated steam on the inner wall (4Q) with high pressure and high temperature combustion gas (5M) with multiple theoretical combustion chambers (4Q) Various energy storage cycle coalescence engines and coalescence methods in the form of a simple water injection engine (88n) for theoretical combustion chamber (4Q) combustion + both center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, high pressure high temperature combustion gas (5M) with multiple theoretical combustion chambers (4Q) (4Q) inner wall oxygen + fuel + superheated steam at optimum temperature Various energy storage cycle coalescence engines and coalescence methods that are heated to a theoretical combustion chamber (4Q) combustion + both center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) combustion into a simple water injection engine (88n).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Superheated steam that receives low-priced liquid oxygen (5K) + high-temperature water, and includes high-pressure high-temperature combustion gas (5M) having a plurality of theoretical combustion chambers (4Q) (4Q) oxygen + fuel on the inner wall + received high-temperature water Various energy storage cycle coalescence engines, which are made into a simple water injection engine (88n) that is heated to an optimum temperature to make theoretical combustion chamber (4Q) combustion + both center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) combustion, and Merge method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K), heat oxygen + fuel + superheated steam at the inner wall at the optimum temperature, theoretical combustion chamber (4Q) combustion + both sides center support bearing load coalescence 0 approaching counter-rotating production compressed air ( 28a) Various energy storage cycle coalescing engines and coalescence methods in a simple water injection engine (88n) for combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) + electricity, heat oxygen + fuel + superheated steam on the inner wall at the optimum temperature, theoretical combustion chamber (4Q) combustion + both sides center support bearing load coalescence 0 approach double reversal manufacturing compression Various energy storage cycle coalescing engines and coalescing methods in a simple water injection engine (88n) for air (28a) combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, heating oxygen + fuel + superheated steam on the inner wall at the optimum temperature, theoretical combustion chamber (4Q) combustion + double-sided center support bearing combined load 0 approach double Various energy storage cycle coalescing engine and coalescence method in a simple water injection engine (88n) for combustion with inverted manufactured compressed air (28a).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K), heat oxygen + fuel + superheated steam on the inner wall at the optimum temperature and burn the theoretical combustion chamber (4Q) + both sides center support bearing load coalescence 0 approaching counter-rotating manufactured compressed air (28a) Various energy storage cycle coalescing engines and coalescing methods in a simple water injection engine (88n) for combustion.   Magnet type bearing load approaching 0 + ultra high speed circumferential speed horizontal type + both sides center support bearing load coalescence 0 approaching counter-rotating manufactured compressed air (28a) combustion blade ratio critical material gravity turbine (8U) extremely inexpensive generator electricity Manufactures electricity + liquid air cold heat + hot water to superheated steam temperature heat supply equipment (3D), receives cheap liquid oxygen (5K) + electricity, and heats oxygen + fuel + superheated steam at the optimum temperature on the inner wall and theoretical combustion Combustion chamber (4Q) + both center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) combustion simple water injection engine (88n) various energy storage cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, heating oxygen + fuel + superheated steam on the inner wall at the optimum temperature and burning in the theoretical combustion chamber (4Q) Various energy storage cycle coalescing engine and coalescence method in the form of a simple water injection engine (88n) of heavy inversion manufactured compressed air (28a) combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K), heat oxygen + fuel + superheated steam at the optimal temperature on the inner wall, and heat superheated steam (50) in the high-temperature water heating pipe (5H) by theoretical combustion chamber (4Q) combustion Injection + both center support bearing load coalescence 0 approaching counter-rotating manufactured compressed air (28a) Various energy storage cycle coalescing engine and coalescence method for burning simple water injection engine (88n).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Received cheaper liquid oxygen (5K) + electricity, heated oxygen + fuel + superheated steam at the inner wall at the optimum temperature, and heated superheated steam (50) in the hot water heating pipe (5H) in the theoretical combustion chamber (4Q) combustion Various energy storage cycle coalescence engines and coalescence methods, which are made into a simple water injection engine (88n) that burns heated injection + both center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) + electricity + hot water, heat oxygen + fuel + superheated steam at the inner wall at the optimum temperature, and heat the hot water heated pipe (5H) in the theoretical combustion chamber (4Q) combustion Various energy storage cycle coalescence engine and coalescence method (50), which is heating injection + both center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) burning simple water injection engine (88n).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) + hot water, heat oxygen + fuel + superheated steam on the inner wall at the optimum temperature, and receive hotheat steam received in the hot water heating pipe (5H) in the theoretical combustion chamber (4Q) combustion Various energy storage cycle coalescence engines and coalescence methods comprising a simple water injection engine (88n) that burns superheated steam (50) including heated injection + both center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K), air (28a) suction injection flow at the optimal location, multiple theoretical combustion chambers (4Q) as well as combustion injection + both-side center support bearing load coalescence 0 approach double reversal manufacturing Various energy storage cycle coalescing engines and coalescing methods in a simple water injection engine (88n) that burns with compressed air (28a).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, the air (28a) suction injection flow at the optimal location is also equipped with a plurality of theoretical combustion chambers (4Q) combustion injection + double-sided center support bearing load coalescence 0 approach double Various energy storage cycle coalescing engine and coalescence method in a simple water injection engine (88n) that burns with inverted manufactured compressed air (28a).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, the air (28a) suction injection flow at the optimum location also with a plurality of theoretical combustion chambers (4Q) combustion injection + both-side center support bearing load combination 0 Various energy storage cycle coalescing engine and coalescence method in the form of a simple water injection engine (88n) that burns near-inverted manufacturing compressed air (28a).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K), making it a simple water injection engine (88n), forward air inlet + both sides center support bearing load coalescence 0 approaching counter-rotating manufactured compressed air (28a) burning various energy storage Cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Cheaper liquid oxygen (5K) + receiving electricity + both sides center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) burned to make a simple water injection engine (88n), various front-facing air inlets Energy conservation cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Cheaper liquid oxygen (5K) + Electricity + High temperature water received + Both sides center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) burns to make a simple water injection engine (88n) and front air inlet Various energy conservation cycle coalescence engines and coalescence methods.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) + Both sides center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) burns to make a simple water injection engine (88n), straight forward with air inlet Various energy storage cycle coalescing engine and coalescence method for injecting maximum bubbles to the bottom of the ship.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Cheaper liquid oxygen (5K) + receiving electricity + both sides center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) burned to make a simple water injection engine (88n) forward air inlet Various energy storage cycle coalescing engine and coalescence method for approaching a straight line and injecting the maximum amount of bubbles to the ship bottom.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Cheaper liquid oxygen (5K) + Electricity + High temperature water received + Both sides center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) burns to make a simple water injection engine (88n) and front air inlet Various energy storage cycle coalescing engine and coalescence method for injecting the maximum amount of air bubbles toward the bottom of the ship.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + hot water + both sides center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) burns to make a simple water injection engine (88n) forward air inlet Various energy storage cycle coalescing engine and coalescence method in which a bubble is jetted to the bottom of a ship close to a straight line.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) + Both sides center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) burned, high-pressure high-temperature combustion gas (5M) equipped with two kinds of theoretical combustion chambers (4Q) ) Various energy storage cycle coalescing engines and coalescence methods that are simple injection engines (88o) for injection acceleration injection.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Cheaper liquid oxygen (5K) + receiving electricity + both sides center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) burned, high pressure high temperature combustion gas equipped with two kinds of theoretical combustion chambers (4Q) (5M) Various energy storage cycle coalescing engines and coalescence methods that are simple injection engines (88o) for injection acceleration injection.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Less expensive liquid oxygen (5K) + Electricity + High temperature water received + Both sides center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) burned, high pressure equipped with two kinds of theoretical combustion chambers (4Q) Various energy storage cycle coalescing engines and coalescence methods that are simple injection engines (88o) for high-temperature combustion gas (5M) injection acceleration injection.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) + Both sides center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) burned, high-pressure high-temperature combustion gas (5M) equipped with two kinds of theoretical combustion chambers (4Q) ) (4Q) Various energy storage cycle coalescing engines and coalescing methods in a simple injection engine (88o) that uses oxygen + fuel + superheated steam on the inner wall at the optimum temperature.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Cheaper liquid oxygen (5K) + receiving electricity + both sides center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) burned, high pressure high temperature combustion gas equipped with two kinds of theoretical combustion chambers (4Q) In (5M), (4Q) various energy storage cycle coalescing engines and coalescing methods, which are simple injection engines (88o) that use oxygen + fuel + superheated steam on the inner wall at an optimum temperature.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Less expensive liquid oxygen (5K) + Electricity + High temperature water received + Both sides center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) burned, high pressure equipped with two kinds of theoretical combustion chambers (4Q) Various energy storage cycle coalescence engines and coalescence methods, which are simple injection engines (88o) that use (4Q) oxygen + fuel + superheated steam on the inner wall with high-temperature combustion gas (5M) at the optimum temperature.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) + Both sides center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) burned, high-pressure high-temperature combustion gas (5M) equipped with two kinds of theoretical combustion chambers (4Q) ) (4Q) Various energy storage cycle coalescing engines and coalescence methods, which are made into a simple injection engine (88o) in which the oxygen + fuel + superheated steam on the inner wall is heated at an optimum temperature to make two kinds of theoretical combustion chambers (4Q) combustion, etc.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Cheaper liquid oxygen (5K) + receiving electricity + both sides center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) burned, high pressure high temperature combustion gas equipped with two kinds of theoretical combustion chambers (4Q) Various energy storage cycle coalescence engine and coalescence method in (5M) (4Q) a simple injection engine (88o) in which oxygen + fuel + superheated steam on the inner wall is heated at the optimum temperature to make two types of theoretical combustion chamber (4Q) combustion, etc. .   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Less expensive liquid oxygen (5K) + Electricity + High temperature water received + Both sides center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) burned, high pressure equipped with two kinds of theoretical combustion chambers (4Q) Various energy conservation cycle coalescence engine which made simple injection engine (88o) to make 2 kinds of theoretical combustion chambers (4Q) combustion etc. by heating the optimum temperature of oxygen + fuel + superheated steam of (4Q) inner wall with high temperature combustion gas (5M) And coalescing method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + high temperature water + both center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) combustion, high pressure high temperature combustion equipped with two kinds of theoretical combustion chambers (4Q) Various types of energy storage in a simple injection engine (88o) that uses gas (5M) and (4Q) inner wall oxygen + fuel + superheated steam containing received high-temperature water to achieve optimum temperature heating to make two types of theoretical combustion chamber (4Q) combustion, etc. Cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) + Both sides center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) combustion, oxygen + fuel + superheated steam heated at the optimum temperature on one kind of inner wall 2 Various energy storage cycle coalescing engine and coalescence method in a simple injection engine (88o) of type theoretical combustion chamber (4Q) combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Cheaper liquid oxygen (5K) + receiving electricity + both sides center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) is burned, and oxygen + fuel + superheated steam is heated at the optimum temperature on one kind of inner wall 2 types of theoretical combustion chamber (4Q) various energy storage cycle coalescing engine and coalescence method made into a simple injection engine (88o) for combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Cheaper liquid oxygen (5K) + Electricity + High temperature water received + Both sides center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) burns and optimizes oxygen + fuel + superheated steam on one kind of inner wall Various energy storage cycle coalescing engines and coalescence methods that have been heated to two types of theoretical combustion chamber (4Q) combustion simple injection engine (88o).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) + Both sides center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) combustion, oxygen + fuel + superheated steam heated at the optimum temperature on one kind of inner wall 2 Type Theoretical Combustion Chamber (4Q) Various energy storage cycle coalescing engine and coalescing method in a simple injection engine (88o) for combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Cheaper liquid oxygen (5K) + receiving electricity + both sides center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) is burned, and oxygen + fuel + superheated steam is heated at the optimum temperature on one kind of inner wall 2 types of theoretical combustion chambers (4Q), various energy storage cycle coalescing engines and coalescence methods made into a simple injection engine (88o) that burns.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Cheaper liquid oxygen (5K) + Electricity + High temperature water received + Both sides center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) burns and optimizes oxygen + fuel + superheated steam on one kind of inner wall Various energy storage cycle coalescing engine and coalescence method in a simple injection engine (88o) that heats and heats two types of theoretical combustion chambers (4Q).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) + Both sides center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) combustion, oxygen + fuel + superheated steam heated at the optimum temperature on one kind of inner wall 2 Various energy storage cycle coalescence engines and coalescence methods that are simple injection engines (88o) that heat and inject superheated steam (50) of a high-temperature water heating pipe (5H) by combustion in a type theoretical combustion chamber (4Q).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Cheaper liquid oxygen (5K) + receiving electricity + both sides center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) is burned, and oxygen + fuel + superheated steam is heated at the optimum temperature on one kind of inner wall Various energy storage cycle coalescence engines and coalescence methods, which are simple injection engines (88o) that heat and inject superheated steam (50) of a high-temperature water heating pipe (5H) in two types of theoretical combustion chamber (4Q) combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Cheaper liquid oxygen (5K) + Electricity + High temperature water received + Both sides center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) burns and optimizes oxygen + fuel + superheated steam on one kind of inner wall Various energy storage cycle coalescence engines and coalescence methods that are a simple injection engine (88o) that heats and injects the superheated steam (50) of the high-temperature water heating pipe (5H) in two types of theoretical combustion chamber (4Q) combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + hot water + both sides center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) burning, oxygen + fuel + superheated steam at one kind of inner wall at optimum temperature heating Various energy storage cycle coalescing engines and coalesced in a simple injection engine (88o) that heats and injects superheated steam (50) including superheated steam received in the high-temperature water heating pipe (5H) in two types of theoretical combustion chamber (4Q) combustion Method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + both center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) burns, and air (28a) a plurality of two types of theoretical combustion at the optimum place of suction jet flow Chamber (4Q) Various energy storage cycle coalescing engine and coalescence method, which is a simple injection engine (88o) that performs combustion injection in the same manner as the injection unit.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Cheaper liquid oxygen (5K) + Receive electricity + Both sides center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) burned, and air (28a) suction injection flow at the optimal location Various energy storage cycle coalescing engine and coalescence method, which is a simple injection engine (88o) that performs combustion injection in the same manner as the theoretical combustion chamber (4Q) injection unit.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Cheaper liquid oxygen (5K) + Electricity + High temperature water received + Both sides center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) burned, and air (28a) suction injection flow at the optimal location Various energy storage cycle coalescing engines and coalescence methods in the form of a simple injection engine (88o) in which two types of theoretical combustion chamber (4Q) injectors are provided and combustion-injected similarly.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + both center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) burned and rotated with simple injection engine (88o) to allow vertical ascent and descent Energy conservation cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Cheaper liquid oxygen (5K) + receiving electricity + both sides center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) burns and rotates with simple injection engine (88o) to allow vertical rise and fall Various energy storage cycle coalescence engines and coalescence methods.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Cheaper liquid oxygen (5K) + Electricity + High temperature water received + Both sides center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) burns, rotates with simple injection engine (88o) and rises and falls vertically Various energy storage cycle coalescence engines and coalescence methods that make possible.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + Both sides center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) burns and rotates with simple injection engine (88o) to enable reverse injection Storage cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Cheaper liquid oxygen (5K) + electricity received + both sides center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) burned and rotated with simple injection engine (88o) to enable reverse injection Various energy storage cycle coalescence engines and coalescence methods.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Cheaper liquid oxygen (5K) + Electricity + High temperature water received + Both sides center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) burns, rotates with simple injection engine (88o) and reverse injection Various energy storage cycle coalescence engines and coalescence methods made possible.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + high temperature water + both center support bearings load combined 0 approaching counter-rotating production compressed air (28a) burning, rotating with simple injection engine (88o), enabling reverse injection Various energy storage cycle coalescence engines and coalescence methods.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Supplying electricity + hot water (52b) as liquid oxygen production, easy aiming to maximize suction speed, both sides of the center drive bearing load combined with electric drive 0 approach simple multistage compressor (3h) + liquid oxygen production machine (88l) Various energy storage cycle coalescence engines and coalescence methods.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Supplying electricity to produce liquid oxygen, easy aiming to maximize suction speed, both sides of electric drive center support bearing load coalescence 0 approach easy multistage compressor (3h) + liquid oxygen production machine (88l) various energy storage cycle coalescence Organization and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Electric + superheated steam supply liquid oxygen production, easy aiming to maximize suction speed Electric drive both sides center support bearing load coalescence 0 approach easy multistage compressor (3h) + liquid oxygen production machine (88l) Storage cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) As an electric + hot water (52b) supply liquid oxygen production, easy aiming to maximize the suction speed, both sides of the electric drive center support bearing load coalescence 0 approach simple multistage compressor (3h) + liquid oxygen production machine (88l) Various energy storage cycle coalescence engine and coalescence method for producing liquid oxygen.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Supplying electricity to produce liquid oxygen, easy aiming to maximize suction speed Electric drive both sides center support bearing load coalescence 0 approach easy multistage compressor (3h) + liquid oxygen production machine (88l) various energy to produce liquid oxygen Storage cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Supplying electricity + superheated steam to produce liquid oxygen, easy aiming to maximize suction speed, both sides of electric drive center support bearing load coalescence 0 approach easy multistage compressor (3h) + liquid oxygen production machine (88l) as liquid oxygen production Various energy storage cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) As an electric + hot water (52b) supply liquid oxygen production, easy aiming to maximize the suction speed, both sides of the electric drive center support bearing load coalescence 0 approach simple multistage compressor (3h) + liquid oxygen production machine (88l) Various energy storage cycle coalescence engine and coalescence method for producing compressed heat exchange superheated steam by sucking air.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Supplying electricity as liquid oxygen production, easy aiming to maximize suction speed Electric drive both sides center support bearing load coalescence 0 approach simple multistage compressor (3h) + liquid oxygen production machine (88l) as intake air compression heat exchange Various energy storage cycle coalescence engine and coalescence method for producing superheated steam.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Supplying electricity + superheated steam to produce liquid oxygen, easily aiming to maximize suction speed, both sides of electric drive center support bearing combined load 0 approaching easy multistage compressor (3h) + liquid oxygen producing machine (88l) sucking air Various energy storage cycle coalescence engine and coalescence method for producing compressed heat exchange superheated steam.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Electric + hot water (52b) + superheated steam supply liquid oxygen production, easy aiming to maximize suction speed, both sides center support bearing combined load of electric drive 0 approach simple multistage compressor (3h) + liquid oxygen production machine ( 88l), various energy storage cycle coalescence engines and coalescence methods for producing compressed heat exchange superheated steam that sucks air.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) As an electric + hot water (52b) supply liquid oxygen production, easy aiming to maximize the suction speed, both sides of the electric drive center support bearing load coalescence 0 approach simple multistage compressor (3h) + liquid oxygen production machine (88l) Various energy storage cycle coalescence engines and coalescence methods for producing liquid nitrogen.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Supplying electricity to produce liquid oxygen, easy aiming to maximize suction speed, both sides of electric drive center support bearing load coalescence 0 approach easy multistage compressor (3h) + liquid oxygen production machine (88l) to produce liquid nitrogen Energy conservation cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Supplying electricity + superheated steam to produce liquid oxygen, easy aiming to maximize suction speed, both sides of electric drive center support bearing load coalescence 0 approach easy multistage compressor (3h) + liquid oxygen production machine (88l) as liquid nitrogen Various energy storage cycle coalescence engines and coalescence methods to be manufactured.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) As an electric + hot water (52b) supply liquid oxygen production, easy aiming to maximize the suction speed, both sides of the electric drive center support bearing load coalescence 0 approach simple multistage compressor (3h) + liquid oxygen production machine (88l) Various energy storage cycle coalescence engine and coalescence method for supplying liquid nitrogen to manufacturing and supply equipment (3D).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Supplying electricity as liquid oxygen production, easy aiming to maximize the suction speed Electric drive both sides center support bearing load coalescence 0 approach easy multistage compressor (3h) + liquid oxygen production machine (88l) as production and supply equipment of liquid nitrogen Various energy storage cycle coalescence engines and coalescence methods supplied to (3D).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Supplying electricity + superheated steam to produce liquid oxygen, easy aiming to maximize suction speed, both sides of electric drive center support bearing load coalescence 0 approach easy multistage compressor (3h) + liquid oxygen production machine (88l) as liquid nitrogen Various energy storage cycle coalescence engine and coalescence method to be supplied to the production supply facility (3D).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) As an electric + hot water (52b) supply liquid oxygen production, easy aiming to maximize the suction speed, both sides of the electric drive center support bearing load coalescence 0 approach simple multistage compressor (3h) + liquid oxygen production machine (88l) Various energy storage cycle coalescence engine and coalescence method for supplying liquid nitrogen + liquid oxygen + superheated steam to the production supply facility (3D).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Supplying electricity as liquid oxygen production, easy aiming to maximize suction speed, both sides center support bearing load coalescence of electric drive 0 approach simple multistage compressor (3h) + liquid oxygen production machine (88l) as liquid nitrogen + liquid oxygen + Various energy storage cycle coalescence engines and coalescence methods for supplying superheated steam to the production and supply equipment (3D).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) As an electric + superheated steam supply liquid oxygen production, easy aiming to maximize suction speed both sides center support bearing load combination of electric drive 0 approach easy multistage compressor (3h) + liquid oxygen production machine (88l) liquid nitrogen + Various energy storage cycle coalescence engine and coalescence method for supplying liquid oxygen + superheated steam to the production supply facility (3D).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Electric + hot water (52b) + superheated steam supply liquid oxygen production, easy aiming to maximize suction speed, both sides center support bearing combined load of electric drive 0 approach simple multistage compressor (3h) + liquid oxygen production machine ( 88l) Various energy storage cycle coalescence engines and coalescence methods for supplying liquid nitrogen + liquid oxygen + superheated steam to the production supply facility (3D).   Horizontally-moving blade ratio critical material gravity turbine (8U) with extremely high speed circumferential speed with magnetic bearing load approaching 0 + double-sided center support bearing load combined 0 approaching simple multistage compressor (3h) + Various energy storage cycle coalescence engines and coalescence methods configured to simplify the liquid oxygen production machine (88l) and maximize the suction speed.   Horizontally-moving blade ratio critical material gravity turbine (8U) with extremely high speed circumferential speed with magnetic bearing load approaching 0 + double-sided center support bearing load combined 0 approaching simple multistage compressor (3h) + Various energy storage cycle coalescence engines and coalescence methods that compress air as a configuration that simplifies the liquid oxygen producing machine (88l) and maximizes the suction speed.   Horizontally-moving blade ratio critical material gravity turbine (8U) with extremely high speed circumferential speed with magnetic bearing load approaching 0 + double-sided center support bearing load combined 0 approaching simple multistage compressor (3h) + Various energy storage cycle coalescence engines and coalescence methods that compress air (28a) as a configuration that simplifies the liquid oxygen production machine (88l) to maximize the suction speed.   Horizontally-moving blade ratio critical material gravity turbine (8U) with extremely high speed circumferential speed with magnetic bearing load approaching 0 + double-sided center support bearing load combined 0 approaching simple multistage compressor (3h) + Various energy storage cycle coalescing engines and coalescence methods for compressing one or more stages as a configuration that maximizes the suction speed by simplifying the liquid oxygen production machine (88l).   Horizontally-moving blade ratio critical material gravity turbine (8U) with extremely high speed circumferential speed with magnetic bearing load approaching 0 + double-sided center support bearing load combined 0 approaching simple multistage compressor (3h) + Various energy storage cycle coalescence engines and coalescence methods for heating 1 to multi-stage compressed water as a configuration that makes the liquid oxygen production machine (88l) simple and maximizes the suction speed.   Horizontally-moving blade ratio critical material gravity turbine (8U) with extremely high speed circumferential speed with magnetic bearing load approaching 0 + double-sided center support bearing load combined 0 approaching simple multistage compressor (3h) + Various energy storage cycle coalescence engines and coalescence methods for heating 1 to multi-stage compressed high-temperature water as a configuration that simplifies the liquid oxygen production machine (88l) and maximizes the suction speed.   Horizontally-moving blade ratio critical material gravity turbine (8U) with extremely high speed circumferential speed with magnetic bearing load approaching 0 + double-sided center support bearing load combined 0 approaching simple multistage compressor (3h) + Various energy storage cycle coalescence engines and coalescence methods for heating 1 to multi-stage compressed superheated steam as a configuration that makes the liquid oxygen production machine (88l) simple and maximizes the suction speed.   Horizontally-moving blade ratio critical material gravity turbine (8U) with extremely high speed circumferential speed with magnetic bearing load approaching 0 + double-sided center support bearing load combined 0 approaching simple multistage compressor (3h) + Various energy storage cycle coalescence engines and coalescence methods that heat the water by 1 to multi-stage compression as a configuration that simplifies the liquid oxygen production machine (88l) and maximizes the suction speed.   Horizontally-moving blade ratio critical material gravity turbine (8U) with extremely high speed circumferential speed with magnetic bearing load approaching 0 + double-sided center support bearing load combined 0 approaching simple multistage compressor (3h) + Various energy storage cycle coalescence engines and coalescence methods for heating high-temperature water by 1 to multi-stage compression as a configuration that makes the liquid oxygen production machine (88l) simple and maximizes the suction speed.   Horizontally-moving blade ratio critical material gravity turbine (8U) with extremely high speed circumferential speed with magnetic bearing load approaching 0 + double-sided center support bearing load combined 0 approaching simple multistage compressor (3h) + Various energy storage cycle coalescence engines and coalescence methods for heating superheated steam by 1 to multi-stage compression as a configuration that makes the liquid oxygen production machine (88l) simple and maximizes the suction speed.   Horizontally-moving blade ratio critical material gravity turbine (8U) with extremely high speed circumferential speed with magnetic bearing load approaching 0 + double-sided center support bearing load combined 0 approaching simple multistage compressor (3h) + Various energy storage cycle coalescence engines and coalescence methods for producing superheated steam by compression as a configuration that makes the liquid oxygen production machine (88l) simple and maximizes the suction speed.   Horizontally-moving blade ratio critical material gravity turbine (8U) with extremely high speed circumferential speed with magnetic bearing load approaching 0 + double-sided center support bearing load combined 0 approaching simple multistage compressor (3h) + Various energy storage cycle coalescence engines and coalescence methods for producing liquid oxygen + superheated steam by compression as a configuration that maximizes the suction speed by simplifying the liquid oxygen production machine (88l).   Horizontally-moving blade ratio critical material gravity turbine (8U) with extremely high speed circumferential speed with magnetic bearing load approaching 0 + double-sided center support bearing load combined 0 approaching simple multistage compressor (3h) + Various energy storage cycle coalescence engine and coalescence method for producing liquid oxygen + liquid nitrogen + superheated steam by compression as a configuration that makes the liquid oxygen production machine (88l) simple and maximizes the suction speed.   Horizontally-moving blade ratio critical material gravity turbine (8U) with extremely high speed circumferential speed with magnetic bearing load approaching 0 + double-sided center support bearing load combined 0 approaching simple multistage compressor (3h) + Various energy storage cycle coalescence engines and coalescence methods for producing liquid oxygen + liquid nitrogen + high temperature water by compression as a configuration that makes the liquid oxygen production machine (88l) simple and maximizes the suction speed.   Horizontally-moving blade ratio critical material gravity turbine (8U) with extremely high speed circumferential speed with magnetic bearing load approaching 0 + double-sided center support bearing load combined 0 approaching simple multistage compressor (3h) + Various energy storage cycle coalescence engines and coalescence methods for supplying the liquid oxygen + superheated steam production / supply facility (3D) by compression as a configuration that simplifies the liquid oxygen production machine (88l) and maximizes the suction speed.   Horizontally-moving blade ratio critical material gravity turbine (8U) with extremely high speed circumferential speed with magnetic bearing load approaching 0 + double-sided center support bearing load combined 0 approaching simple multistage compressor (3h) + Various energy storage cycle coalescence engine and coalescence method for supplying liquid oxygen + liquid nitrogen + high pressure superheated steam production / supply facility (3D) by compression as a configuration that simplifies the liquid oxygen production machine (88l) and maximizes the suction speed.   Horizontally-moving blade ratio critical material gravity turbine (8U) with extremely high speed circumferential speed with magnetic bearing load approaching 0 + double-sided center support bearing load combined 0 approaching simple multistage compressor (3h) + Various energy storage cycle coalescence engine and coalescence method for supplying liquid oxygen + liquid nitrogen + super high pressure superheated steam production and supply equipment (3D) by compression as a configuration that maximizes the suction speed by simplifying the liquid oxygen production machine (88l).   Horizontally-moving blade ratio critical material gravity turbine (8U) with extremely high speed circumferential speed with magnetic bearing load approaching 0 + double-sided center support bearing load combined 0 approaching simple multistage compressor (3h) + Various energy storage cycle coalescence engines and coalescence methods for supplying the liquid oxygen + superhigh pressure superheated steam production / supply facility (3D) by compression as a configuration that simplifies the liquid oxygen production machine (88l) and maximizes the suction speed.   Horizontally-moving blade ratio critical material gravity turbine (8U) with extremely high speed circumferential speed with magnetic bearing load approaching 0 + double-sided center support bearing load combined 0 approaching simple multistage compressor (3h) + Various energy storage cycle coalescence engine and coalescence method for supplying liquid oxygen + liquid nitrogen + super high pressure superheated steam production and supply equipment (3D) by compression as a configuration that maximizes the suction speed by simplifying the liquid oxygen production machine (88l).   Horizontally-moving blade ratio critical material gravity turbine (8U) with extremely high speed circumferential speed with magnetic bearing load approaching 0 + double-sided center support bearing load combined 0 approaching simple multistage compressor (3h) + Various energy storage cycle coalescence engines and coalescence methods for supplying the electric oxygen + liquid oxygen + liquid nitrogen + super high pressure superheated steam production and supply equipment (3D) by compression as a configuration that maximizes the suction speed by simplifying the liquid oxygen production machine (88l).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Various energy storage cycle coalescence engines and coalescence methods, in which low-cost liquid oxygen (5K) is received into a simple gas engine (88 m) on both side center support bearing load coalescence, and fuel injection combustion is performed in compressed air.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Various energy storage cycle coalescence engines and coalescence methods that make the two-sided center support bearing load coalescence zero approach simple injection engine (88o) receive low-cost liquid oxygen (5K) and receive fuel injection combustion + compressed air fuel injection combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) More energy storage cycle coalescence engine with two types of theoretical combustion chambers: fuel injection combustion + compressed air fuel injection combustion + low-cost liquid oxygen (5K) received from both sides center support bearing load coalescence 0 approach simple water injection engine (88n) And coalescing method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) More energy storage cycle with two types of theoretical combustion chambers (4Q): low-cost liquid oxygen (5K) received in a simple gas engine (88m) on both side center support bearings combined, and fuel injection combustion with compressed air + fuel injection combustion Merger engine and merger method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) From both sides center support bearing load coalescence 0 approach easy injection engine (88o) receives cheap liquid oxygen (5K) fuel injection combustion + compressed air fuel injection combustion into two types of theoretical combustion chamber (4Q) and opens and closes at one type inlet Various energy storage cycle coalescence engine and coalescence method provided in the valve (1Q).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) From both sides center support bearing load coalescence 0 approach simple water injection engine (88n) received cheap liquid oxygen (5K) fuel injection combustion + compressed air fuel injection combustion into two types of theoretical combustion chamber (4Q) and one type inlet Various energy storage cycle coalescence engine and coalescence method provided with on-off valve (1Q) oxygen injection nozzle (6L).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) From both sides center support bearing load coalescence 0 approach Easy gas engine (88m) receives cheap liquid oxygen (5K) Fuel injection combustion + Compressed air fuel injection combustion 2 types of theoretical combustion chamber (4Q) open and close to 1 type inlet Various energy storage cycle coalescence engines and coalescence methods comprising a valve (1Q), an oxygen injection nozzle (6L), and a fuel injection nozzle (6X).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) From both sides center support bearing load coalescence 0 approach easy injection engine (88o) receives cheap liquid oxygen (5K) fuel injection combustion + compressed air fuel injection combustion into two types of theoretical combustion chamber (4Q) and opens and closes at one type inlet Valves (1Q), oxygen injection nozzles (6L), fuel injection nozzles (6X), on-off valves (1Q), various energy storage cycle coalescing engines and coalescence methods.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) From both sides center support bearing load coalescence 0 approach simple water injection engine (88n) received cheap liquid oxygen (5K) fuel injection combustion + compressed air fuel injection combustion into two types of theoretical combustion chamber (4Q) and one type inlet On-off valve (1Q) Oxygen injection nozzle (6L) Fuel injection nozzle (6X) Equipped with on-off valve (1Q) closed oxygen fuel injection Combustion engine and combination method for various energy storage cycles.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) From both sides center support bearing load coalescence 0 approach Easy gas engine (88m) receives cheap liquid oxygen (5K) Fuel injection combustion + Compressed air fuel injection combustion 2 types of theoretical combustion chamber (4Q) open and close to 1 type inlet Valve (1Q) Oxygen injection nozzle (6L) Fuel injection nozzle (6X) Equipped with on-off valve (1Q) Closed oxygen fuel injection Combustion rotational output Increases various energy storage cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) From both sides center support bearing load coalescence 0 approach easy injection engine (88o) receives cheap liquid oxygen (5K) fuel injection combustion + compressed air fuel injection combustion into two types of theoretical combustion chamber (4Q) and opens and closes at one type inlet Valve (1Q) Oxygen injection nozzle (6L) Fuel injection nozzle (6X) Open / close valve (1Q) Closed oxygen fuel injection Combustion rotation output increase 2 types (4Q) Superheated steam (50) Various energy storage cycle coalescence engine and coalescence Method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) From both sides center support bearing load coalescence 0 approach simple water injection engine (88n) received cheap liquid oxygen (5K) fuel injection combustion + compressed air fuel injection combustion into two types of theoretical combustion chamber (4Q) and one 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 2 types (4Q) Superheated steam (50) injection sucks combustion gas (49) Various energy storage cycle coalescence engines and coalescence methods for injection.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) From both sides center support bearing load coalescence 0 approach Easy gas engine (88m) receives cheap liquid oxygen (5K) Fuel injection combustion + Compressed air fuel injection combustion 2 types of theoretical combustion chamber (4Q) open and close to 1 type inlet Valve (1Q) Oxygen injection nozzle (6L) Fuel injection nozzle (6X) Open / close valve (1Q) Closed oxygen fuel injection Combustion rotation output increase 2 types (4Q) Superheated steam (50) injection and combustion gas (49) suction injection Various energy storage cycle coalescing engine and coalescence method for increasing injection propulsion output.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) From both sides center support bearing load coalescence 0 approaching simple injection engine (88o) receiving cheap liquid oxygen (5K) fuel injection combustion + compressed air fuel injection combustion into two types of theoretical combustion chamber (4Q) at one type inlet and outlet Various energy storage cycle coalescence engines and coalescence methods comprising an on-off valve (1Q), an oxygen injection nozzle (6L), and a fuel injection nozzle (6X).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Both side center support bearing load coalescence 0 approach Easy water injection engine (88n) receive cheap liquid oxygen (5K) Fuel injection combustion + Compressed air fuel injection combustion 2 types of theoretical combustion chamber (4Q) 1 type inlet and outlet On-off valve (1Q), oxygen injection nozzle (6L), fuel injection nozzle (6X), and on-off valve (1Q) to close various energy storage cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Both sides center support bearing load combined 0 approaching simple gas engine (88m) receiving cheap liquid oxygen (5K) fuel injection combustion + compressed air fuel injection combustion into two types of theoretical combustion chamber (4Q) and one type at inlet and outlet On-off valve (1Q) Oxygen injection nozzle (6L) Fuel injection nozzle (6X) Equipped with on-off valve (1Q) closed oxygen fuel injection Combustion engine and combination method for various energy storage cycles.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) From both sides center support bearing load coalescence 0 approaching simple injection engine (88o) receiving cheap liquid oxygen (5K) fuel injection combustion + compressed air fuel injection combustion into two types of theoretical combustion chamber (4Q) at one type inlet and outlet Open / close valve (1Q) Oxygen injection nozzle (6L) Fuel injection nozzle (6X) Open / close valve (1Q) Closed oxygen fuel injection combustion High pressure high temperature combustion gas (5M) various energy storage cycle coalescence engine and coalescence Method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) From both sides center support bearing load coalescence 0 approach simple water injection engine (88n) low cost liquid oxygen (5K) received fuel injection combustion + compressed air fuel injection combustion into two types of theoretical combustion chamber (4Q) at one type inlet and 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) Injection superheated steam (50) also outer periphery (6A ) Various energy storage cycle coalescence engines and coalescence methods to be injected.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Both sides center support bearing load coalescence 0 approach simple injection engine (88o) low-cost liquid oxygen (5K) received fuel injection combustion + compressed air fuel injection combustion into two types of theoretical combustion chamber (4Q) open and close at one type inlet and outlet Valve (1Q) Oxygen injection nozzle (6L) Fuel injection nozzle (6X) Open / close 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 ) Various energy conservation cycle coalescing engine and coalescence method that increase rocket injection injection propulsion output.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) From both sides center support bearing load coalescence 0 approach simple water injection engine (88n) low cost liquid oxygen (5K) received fuel injection combustion + compressed air fuel injection combustion into two types of theoretical combustion chamber (4Q) at one type inlet and 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) Various energy storage cycle coalescing engines and coalescence methods that increase rocket-injected water in front and sucking-injection propulsion output.   Cylindrical turbine blade group with a gravity-accelerated acceleration of gravitational acceleration (mixed injection under ultra-high pressure vertically under vacuum) 8A) Horizontal shaft (16A) Opposite synchronous gear (4C) In-line co-rotating gear (4D) Electric drive solar heater (21) for power generation by multiple turbines and double-sided center support bearing combined load 0 approach simple multistage compressor (3h) + various energy storage cycle coalescence engine and coalescence method to make liquid oxygen production machine (88l).   Cylindrical turbine blade group with a gravity-accelerated acceleration of gravitational acceleration (mixed injection under ultra-high pressure vertically under vacuum) 8A) Horizontal shaft (16A) Series rotating gear (4D) Electric power driven solar heater (21) rotating on multiple turbines and generating electricity with multiple turbines + Both sides center support bearing load coalescence 0 approaching simple multistage compressor (3h) + liquid oxygen Various energy storage cycle coalescing engine and coalescence method for manufacturing machine (88l).   Horizontally moving blade ratio critical material gravity turbine (8U) with a magnetic bearing load approaching 0 and super high speed circumferential speed. Ultra-high pressure vertically below the vacuum in the vacuum, accelerating gravitational acceleration and cylindrical turbine blade group (8A) horizontal Rotating shaft (16A) and cylindrical turbine blade group (8A) Electric drive solar heater (21) for multiple power generation + Both sides center support bearing load coalescence 0 approach easy multistage compressor (3h) + Liquid oxygen production machine (88l) Various energy storage cycle coalescence engines and coalescence methods.   Horizontally moving blade ratio critical material gravity turbine (8U) with a magnetic bearing load approaching 0 and super high speed circumferential speed. Ultra-high pressure vertically below the vacuum in the vacuum, accelerating gravitational acceleration and cylindrical turbine blade group (8A) horizontal Rotating shaft (16A) and cylindrical turbine blade group (8A) 20 sets of electric drive solar heater (21) + both sides center support bearing load coalescence 0 approach easy multistage compressor (3h) + liquid oxygen production machine (88l ) Various energy conservation cycle coalescence engines and coalescence methods.   Horizontally moving blade ratio critical material gravity turbine (8U) with a magnetic bearing load approaching 0 and super high speed circumferential speed. Ultra-high pressure vertically below the vacuum in the vacuum, accelerating gravitational acceleration and cylindrical turbine blade group (8A) horizontal Rotating shaft (16A) and cylindrical turbine blade group (8A) 40 sets of electric drive solar heater (21) + both sides center support bearing load coalescence 0 approach easy multistage compressor (3h) + liquid oxygen production machine (88l ) Various energy conservation cycle coalescence engines and coalescence methods.   Horizontally moving blade ratio critical material gravity turbine (8U) with a magnetic bearing load approaching 0 and super high speed circumferential speed. Ultra-high pressure vertically below the vacuum in the vacuum, accelerating gravitational acceleration and cylindrical turbine blade group (8A) horizontal Rotating shaft (16A) and cylindrical turbine blade group (8A) 80 sets of electric drive solar heater (21) + both sides center support bearing load coalescence 0 approach easy multistage compressor (3h) + liquid oxygen production machine (88l ) Various energy conservation cycle coalescence engines and coalescence methods.   Horizontally moving blade ratio critical material gravity turbine (8U) with a magnetic bearing load approaching 0 and super high speed circumferential speed. Ultra-high pressure vertically below the vacuum in the vacuum, accelerating gravitational acceleration and cylindrical turbine blade group (8A) horizontal Rotating shaft (16A) and cylindrical turbine blade group (8A) 100 sets of electric drive solar heater (21) + both sides center support bearing load coalescence 0 approach simple multistage compressor (3h) + liquid oxygen production machine (88l ) Various energy conservation cycle coalescence engines and coalescence methods.   Horizontally moving blade ratio critical material gravity turbine (8U) with a magnetic bearing load approaching 0 and super high speed circumferential speed. Ultra-high pressure vertically below the vacuum in the vacuum, accelerating gravitational acceleration and cylindrical turbine blade group (8A) horizontal Rotating shaft (16A) and cylindrical turbine blade group (8A) 150 sets of electric drive solar heater (21) + both sides center support bearing load coalescence 0 approach easy multistage compressor (3h) + liquid oxygen production machine (88l ) Various energy conservation cycle coalescence engines and coalescence methods.   Horizontally moving blade ratio critical material gravity turbine (8U) with a magnetic bearing load approaching 0 and super high speed circumferential speed. Ultra-high pressure vertically below the vacuum in the vacuum, accelerating gravitational acceleration and cylindrical turbine blade group (8A) horizontal Rotating shaft (16A) and cylindrical turbine blade group (8A) 200 sets of electric drive solar heater (21) + both sides center support bearing load coalescence 0 approach easy multistage compressor (3h) + liquid oxygen production machine (88l ) Various energy conservation cycle coalescence engines and coalescence methods.   Horizontally moving blade ratio critical material gravity turbine (8U) power generation electric product + rocket combustion + jet combustion both sides center support bearing combined 0 approach simple water injection engine (magnetic approach bearing load 0 approach + super high speed circumferential speed) ( 88n) Various energy storage cycle coalescence engines and coalescence methods that are driven in equality.   Magnetically-applied bearing load approaching 0 + ultra-high-speed circumferential speed with full blade ratio critical material gravity turbine (8U) power generation electrical product + rocket combustion 2 locations + jet combustion 2 locations on both sides center support bearing combined 0 approach easy Various energy storage cycle coalescence engine and coalescence method for driving water injection engine (88n) and the like.   Magnetically-applied bearing load approaching 0 + super high speed circumferential speed with full blade ratio critical material gravity turbine (8U) power generation electrical product + rocket combustion 3 locations + jet combustion 3 locations on both sides center support bearing combined 0 approach easy Various energy storage cycle coalescence engine and coalescence method for driving water injection engine (88n) and the like.   Magnetically utilized bearing load approaching 0 + ultra-high speed circumferential speed with full blade ratio critical material gravity turbine (8U) power generation electrical product + rocket combustion 4 locations + jet combustion 4 locations on both sides center support bearing combined 0 approach easy Various energy storage cycle coalescence engine and coalescence method for driving water injection engine (88n) and the like.   Magnetically-applied bearing load approaching 0 + ultra-high speed circumferential speed with full blade ratio critical material gravity turbine (8U) power generation electrical product + rocket combustion 5 locations + jet combustion 5 locations on both sides center support bearing combined 0 approach easy Various energy storage cycle coalescence engine and coalescence method for driving water injection engine (88n) and the like.   Magnetically-applied bearing load approaching 0 + ultra-high speed peripheral blade ratio critical material gravity turbine (8U) power generation electrical product + rocket combustion 6 locations + jet combustion 6 locations on both sides center support bearings combined 0 approach easy Various energy storage cycle coalescence engine and coalescence method for driving water injection engine (88n) and the like.   Horizontally moving blade ratio critical material gravity turbine (8U) power generation electric product + rocket combustion + jet combustion both sides center support bearing combined 0 approach simple injection engine (88o) ) Various energy storage cycle coalescence engines and coalescence methods to be driven.   Magnetically-applied bearing load approaching 0 + ultra-high-speed circumferential speed with full blade ratio critical material gravity turbine (8U) power generation electrical product + rocket combustion 2 locations + jet combustion 2 locations on both sides center support bearing combined 0 approach easy Various energy storage cycle coalescence engine and coalescence method for driving an injection engine (88o).   Magnetically-applied bearing load approaching 0 + super high speed circumferential speed with full blade ratio critical material gravity turbine (8U) power generation electrical product + rocket combustion 3 locations + jet combustion 3 locations on both sides center support bearing combined 0 approach easy Various energy storage cycle coalescence engine and coalescence method for driving an injection engine (88o).   Magnetically utilized bearing load approaching 0 + ultra-high speed circumferential speed with full blade ratio critical material gravity turbine (8U) power generation electrical product + rocket combustion 4 locations + jet combustion 4 locations on both sides center support bearing combined 0 approach easy Various energy storage cycle coalescence engine and coalescence method for driving an injection engine (88o).   Magnetically-applied bearing load approaching 0 + ultra-high speed circumferential speed with full blade ratio critical material gravity turbine (8U) power generation electrical product + rocket combustion 5 locations + jet combustion 5 locations on both sides center support bearing combined 0 approach easy Various energy storage cycle coalescence engine and coalescence method for driving an injection engine (88o).   Magnetically-applied bearing load approaching 0 + ultra-high speed peripheral blade ratio critical material gravity turbine (8U) power generation electrical product + rocket combustion 6 locations + jet combustion 6 locations on both sides center support bearings combined 0 approach easy Various energy storage cycle coalescence engine and coalescence method for driving an injection engine (88o).   Horizontal type full blade ratio material gravity turbine (8U) Receives low-priced liquid oxygen (5K) from electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D), extremely low-priced electricity production, supports both sides center Various energy storage cycle coalescence engines and coalescence methods for driving the maximum load of bubbles into the bottom vertical parallel plate (9Q) using a simple water jet engine (88n) driven simple water jet engine such as a bearing load coalescence (88n).   Horizontal type full blade ratio material gravity turbine (8U) Receives low-priced liquid oxygen (5K) from electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D), extremely low-priced electricity production, supports both sides center Various energy storage cycle coalescence engine and coalescence method for making a maximum load of bubbles into a ship bottom vertical parallel plate (9Q) by using a screw injection ship such as a bearing water coalescence 0 approach simple water injection engine (88n).   Horizontal type full blade ratio material gravity turbine (8U) Receives low-priced liquid oxygen (5K) from electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D), extremely low-priced electricity production, supports both sides centrally Combined bearing load coalescence 0 approach simple water injection engine (88n), etc. Driven simple water injection engine ship (7u) wide bottom bottom parallel plate (9Q) wide and various energy conservation cycle coalescence engine and coalescence method to maximize air floating amount .   Horizontal type full blade ratio material gravity turbine (8U) Receives low-priced liquid oxygen (5K) from electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D), extremely low-priced electricity production, supports both sides centrally Various energy storage cycle coalescence engines and coalescence methods that make the bearing load coalescence 0 approach simple water injection engine (88n), etc. drive screw injection ship, and have a wide bottom vertical parallel plate (9Q) to maximize the air floating amount.   Horizontal type full blade ratio material gravity turbine (8U) Receives low-priced liquid oxygen (5K) from electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D), extremely low-priced electricity production, supports both sides centrally Combined bearing load coalescence 0 approach simple water injection engine (88n), etc. Drive simple water injection engine ship (7u) wide bottom bottom parallel plate (9Q) wide and various energy conservation cycle coalescence engine and coalescence method to maximize friction reduction amount .   Horizontal type full blade ratio material gravity turbine (8U) Receives low-priced liquid oxygen (5K) from electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D), extremely low-priced electricity production, supports both sides center Various energy storage cycle coalescence engines and coalescence methods that make the bearing load coalescence 0 approach simple water injection engine (88n), etc., drive screw injection ship, wide bottom bottom parallel plate (9Q) and maximize friction reduction.   Horizontal all-blade ratio critical material gravity turbine (8U) power generation electricity production theoretical fluid chamber (4Q) multiple ultra high pressure fuel combustion injection that receives liquid oxygen (5K) and makes the compression volume 21/60000 of air compression Various energy storage cycle coalescence engines and coalescence methods that make a simple injection engine (88o) rotary blade injection airplane (7x) with propulsion + both center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) combustion.   Horizontal full-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) multiple ultra high pressure fuel combustion injection propulsion + both sides center support bearing load coalescence 0 Various energy conservation cycle coalescing engine and coalescence method to make a simple injection engine (88o) rotary blade injection airplane (7x) with combustion in close counter-rotating manufactured compressed air (28a).   Horizontal all-blade ratio critical material gravity turbine (8U) power generation electric manufacturing, receiving liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) multiple ultra high pressure fuel combustion propulsion + both sides center support bearing Various energy storage cycle coalescing engine and coalescence method to make a simple injection engine (88o) rotary blade injection airplane (7x) with a load coalescence 0 approaching counter-rotating manufactured compressed air (28a) combustion.   Includes a theoretical combustion chamber (4Q) air suction flow path that receives liquid oxygen (5K) and produces a compression volume of 21/60000 of air compression, produced by a horizontal full blade ratio critical material gravity turbine (8U) generator Plural super high pressure fuel combustion injection propulsion + both center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) combustion simple injection engine (88o) rotary blade injection plane (7x) various energy storage cycle coalescence engine and Merge method.   Horizontal full-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity, equipped with theoretical combustion chamber (4Q) air suction channel, multiple ultra high pressure fuel combustion injection propulsion + both sides Center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) combustion simple engine (88o) rotary blade injection plane (7x) various energy storage cycle coalescence engine and coalescence method.   Horizontal all blade ratio critical material gravity turbine (8U) power generation electric manufacturing, receiving liquid oxygen (5K) + electricity + high temperature water, and equipped with theoretical combustion chamber (4Q) air suction channel, multiple ultra high pressure fuel combustion injection Various energy storage cycle coalescence engines and coalescence methods that make a simple injection engine (88o) rotary blade injection airplane (7x) with propulsion + both center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) combustion.   Includes a theoretical combustion chamber (4Q) air suction flow path that receives liquid oxygen (5K) and produces a compression volume of 21/60000 of air compression, produced by a horizontal full blade ratio critical material gravity turbine (8U) generator Multiple ultra-high pressure fuel combustion injection propulsion + both center support bearing load coalescence 0 approach double reversal production compressed air (28a) combustion simple injection engine (88o) rotary blade injection airplane (7x) driven various energy conservation cycle coalescence engine, Merge method.   Horizontal full-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity, equipped with theoretical combustion chamber (4Q) air suction channel, multiple ultra high pressure fuel combustion injection propulsion + both sides Center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) combustion simple engine (88o) rotary blade jet airplane (7x) driven various energy storage cycle coalescence engine and coalescence method.   Horizontal all blade ratio critical material gravity turbine (8U) power generation electric manufacturing, receiving liquid oxygen (5K) + electricity + high temperature water, and equipped with theoretical combustion chamber (4Q) air suction channel, multiple ultra high pressure fuel combustion injection Various energy storage cycle coalescence engines and coalescence methods driven by simple injection engine (88o) rotating blade injection airplane (7x) driven by propulsion + both center support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) combustion.   Horizontal all-blade ratio critical material gravity turbine (8U) power generation electrical production, receiving liquid oxygen (5K) and making the compression volume 21/60000 of air compression multiple theoretical combustion chambers (4Q) + both sides center support bearing Various energy storage cycle coalescence engines and coalescence methods driven by a simple injection engine (88o) rotary blade injection airplane (7x) with load coalescence 0 approaching counter-rotating manufactured compressed air (28a) combustion.   Theoretical combustion chamber (4Q) with high pressure fuel combustion + both sides receiving liquid oxygen (5K) and making compression volume 21/60000 Center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) Combustion engine and coalescence method for various energy storage cycle to drive simple gas engine (88m) rotor blade airplane (7w).   Horizontal all-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double-sided center support bearing load coalescence 0 approach double Various energy storage cycle coalescing engine and coalescence method for driving a simple gas engine (88m) rotor blade airplane (7w) as inversion manufactured compressed air (28a) combustion.   Horizontal full-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 Various energy storage cycle coalescing engine and coalescence method for driving a simple gas engine (88m) rotary wing airplane (7w) as combusted counter-rotating manufactured compressed air (28a) combustion.   Theoretical combustion chamber (4Q) with high pressure fuel combustion + both sides receiving liquid oxygen (5K) and making compression volume 21/60000 Center support bearing load coalescence 0 approach counter-rotating production Compressed air (28a) Combustion engine and various energy conservation cycle coalescence engines and multiple rotors (7w) driven by simple gas engine (88m) 1 to plural driving.   Horizontal all-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double-sided center support bearing load coalescence 0 approach double Various energy storage cycle coalescence engine and coalescence method for driving a rotary blade airplane (7w) by driving a plurality of simple gas engines (88m) 1 as combustion of inverted production compressed air (28a).   Horizontal full-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 Various energy storage cycle coalescing engines and coalescence methods for driving a rotating wing airplane (7w) by driving a simple gas engine (88m) 1 to plural as combusted counter-rotating manufactured compressed air (28a) combustion.   Theoretical combustion chamber (4Q) with high pressure fuel combustion + both sides receiving liquid oxygen (5K) and making compression volume 21/60000 Center support bearing load coalescence 0 approach counter-rotating production Compressed air (28a) Combustion engine and various energy conservation cycle coalescence engines and multiple rotors (7w) driven by simple gas engine (88m) 1 to plural driving.   Horizontal all-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double-sided center support bearing load coalescence 0 approach double Various energy storage cycle coalescence engine and coalescence method for driving a rotary blade airplane (7w) by driving a plurality of simple gas engines (88m) 1 as combustion of inverted production compressed air (28a).   Horizontal full-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 Various energy storage cycle coalescing engines and coalescence methods for driving a rotating wing airplane (7w) by driving a simple gas engine (88m) 1 to plural as combusted counter-rotating manufactured compressed air (28a) combustion.   Theoretical combustion chamber (4Q) with high pressure fuel combustion + both sides receiving liquid oxygen (5K) and making compression volume 21/60000 Center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) combustion as simple gas engine (88m) driving and rotary blade airplane (7w) driving various energy storage cycle coalescence engine and coalescence method.   Theoretical combustion chamber (4Q) with high pressure fuel combustion + both sides receiving liquid oxygen (5K) and making compression volume 21/60000 Center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) combustion as simple gas engine (88m) driving rotor blade (7B) rotating and rotating blade airplane (7w) driving various energy conservation cycle coalescence engine and coalescence method .   Horizontal all-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double-sided center support bearing load coalescence 0 approach double Various energy storage cycle coalescence engines and coalescence methods for rotating a simple gas engine (88m) driven rotor blade (7B) and driving a rotor blade airplane (7w) as inversion manufactured compressed air (28a) combustion.   Horizontal full-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 Various energy storage cycle coalescence engines and coalescence methods for rotating a simple gas engine (88m) driving rotor blade (7B) and driving a rotorcraft airplane (7w) as compressed air (28a) combustion.   Theoretical combustion chamber (4Q) with high pressure fuel combustion + both sides receiving liquid oxygen (5K) and making compression volume 21/60000 Center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) Combustion of simple gas engine (88m) 1-multiple drive rotor blade (7B) multiple rotations to drive rotor blade airplane (7w) Organization and coalescence method.   Horizontal all-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double-sided center support bearing load coalescence 0 approach double Various energy storage cycle coalescence engines and coalescence methods for driving a rotary blade airplane (7w) by rotating a simple gas engine (88m) 1 to a plurality of rotor blades (7B) as a reverse combustion compressed air (28a) combustion.   Horizontal full-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 Various energy storage cycle coalescence engines and coalescence methods for driving a rotating blade airplane (7w) by rotating a simple gas engine (88m) 1 to a plurality of driving rotor blades (7B) as combusted counter-rotating manufactured compressed air (28a) combustion.   Theoretical combustion chamber (4Q) with high pressure fuel combustion + both sides receiving liquid oxygen (5K) and making compression volume 21/60000 Center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) Combustion of simple gas engine (88m) 1-multiple drive rotor blade (7B) multiple rotations to drive rotor blade airplane (7w) Organization and coalescence method.   Horizontal all-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double-sided center support bearing load coalescence 0 approach double Various energy storage cycle coalescence engines and coalescence methods for driving a rotary blade airplane (7w) by rotating a simple gas engine (88m) 1 to a plurality of rotor blades (7B) as a reverse combustion compressed air (28a) combustion.   Horizontal full-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 Various energy storage cycle coalescence engines and coalescence methods for driving a rotating blade airplane (7w) by rotating a simple gas engine (88m) 1 to a plurality of driving rotor blades (7B) as combusted counter-rotating manufactured compressed air (28a) combustion.   Theoretical combustion chamber (4Q) with high pressure fuel combustion + both sides receiving liquid oxygen (5K) and making compression volume 21/60000 Center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) combustion as simple gas engine (88m) driving rotor blade (7B) rotating and rotating blade airplane (7w) driving various energy conservation cycle coalescence engine and coalescence method .   Theoretical combustion chamber (4Q) with high pressure fuel combustion + both sides receiving liquid oxygen (5K) and making compression volume 21/60000 Center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) Combustion engine and various energy storage cycle coalescence engine and simple gas engine (88m) driven simple injection engine (88o).   Horizontal all-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double-sided center support bearing load coalescence 0 approach double Various energy storage cycle coalescing engine and coalescence method for driving simple gas engine (88m) driving simple injection engine (88o) as inversion manufactured compressed air (28a) combustion.   Horizontal full-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 Various energy storage cycle coalescing engine and coalescence method for driving a simple gas engine (88m) driving simple injection engine (88o) as a close counter-rotating manufactured compressed air (28a) combustion.   Theoretical combustion chamber (4Q) with high pressure fuel combustion + both sides receiving liquid oxygen (5K) and making compression volume 21/60000 Center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) Combustion engine and various energy storage cycle coalescence engines and simple gas engine (88m) 1 to multiple drive simple injection engine (88o) drive.   Horizontal all-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double-sided center support bearing load coalescence 0 approach double Various energy storage cycle coalescence engine and coalescence method for driving simple gas engine (88m) 1 to multiple drive simple injection engine (88o) as inversion manufactured compressed air (28a) combustion.   Horizontal full-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88m) 1 to a multi-drive simple injection engine (88o) as combustion in the close counter-rotating manufactured compressed air (28a).   Theoretical combustion chamber (4Q) with high pressure fuel combustion + both sides receiving liquid oxygen (5K) and making compression volume 21/60000 Center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) Combustion engine and various energy storage cycle coalescence engines and simple gas engine (88m) 1 to multiple drive simple injection engine (88o) drive.   Horizontal all-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double-sided center support bearing load coalescence 0 approach double Various energy storage cycle coalescence engine and coalescence method for driving simple gas engine (88m) 1 to multiple drive simple injection engine (88o) as inversion manufactured compressed air (28a) combustion.   Horizontal full-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88m) 1 to a multi-drive simple injection engine (88o) as combustion in the close counter-rotating manufactured compressed air (28a).   Theoretical combustion chamber (4Q) with high pressure fuel combustion + both sides receiving liquid oxygen (5K) and making compression volume 21/60000 Center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) Simple gas engine (88m) drive Simple injection engine (88o) Various energy storage cycle coalescence engine and coalescence method for multiple driving.   Theoretical combustion blade water gravity turbine (8V) power generation and electricity production, receiving theoretical oxygen (5K) and making the compression volume 21/60000 of the air compression theoretical combustion chamber (4Q) multiple ultra high pressure fuel combustion injection propulsion + Both-side center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) Combustion simple engine (88o) Oversized osprey (7y) Various energy storage cycle coalescence engine and coalescence method.   Received liquid oxygen (5K) + electricity from vertical all blade hydrogravity turbine (8V) power generation electricity production, theoretical combustion chamber (4Q) multiple ultra high pressure fuel combustion injection propulsion + both sides center support bearing load coalescence approach 0 Various energy storage cycle coalescing engine and coalescence method to make simple injection engine (88o) oversized osprey (7y) with counter-rotating manufactured compressed air (28a) combustion.   Vertical full-blade hydrogravity turbine (8V) power generation electricity production, receiving liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) multiple ultra high pressure fuel combustion injection propulsion + both sides center support bearing load Combined zero approaching counter-rotating production Compressed air (28a) Combustion simple injection engine (88o) Oversized Osprey (7y) Various energy storage cycle coalescing engine and coalescence method.   A plurality of vertical combustion blade hydrogravity turbine (8V) generators and electric generators that receive liquid oxygen (5K) and have a compression volume of 21/60000 of air compression. Super high-pressure fuel combustion injection propulsion + Both-side center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) Combustion simple engine (88o) Oversized osprey (7y) Various energy storage cycle coalescence engines and coalescence methods.   Multi-high pressure fuel combustion injection propulsion including a theoretical combustion chamber (4Q) air suction channel that receives liquid oxygen (5K) + electricity and is manufactured by vertical all blade hydrogravity turbine (8V) power generation electricity production center + both sides Various types of energy storage cycle coalescence engine and coalescence method to make a simple injection engine (88o) oversized osprey (7y) with support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) combustion.   Multi-high pressure fuel combustion injection propulsion that receives liquid oxygen (5K) + electricity + high-temperature water and is equipped with a theoretical combustion chamber (4Q) air suction channel, which is a vertical all blade water gravity turbine (8V) generator + Both-side center support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) Combustion simple engine (88o) Oversized osprey (7y) Various energy storage cycle coalescence engine and coalescence method.   A plurality of vertical combustion blade hydrogravity turbine (8V) generators and electric generators that receive liquid oxygen (5K) and have a compression volume of 21/60000 of air compression. Super high-pressure fuel combustion injection propulsion + both center support bearing load coalescence 0 approach double reversal production compressed air (28a) combustion simple injection engine (88o) extra large Osprey (7y) driven various energy storage cycle coalescence engine and coalescence method.   Multi-high pressure fuel combustion injection propulsion including a theoretical combustion chamber (4Q) air suction channel that receives liquid oxygen (5K) + electricity and is manufactured by vertical all blade hydrogravity turbine (8V) power generation electricity production center + both sides A simple injection engine (88o) and an extra-large osprey (7y) driven by a support bearing load coalescence 0 approaching counter-rotating manufactured compressed air (28a) combustion, and various energy storage cycle coalescence engines and coalescence methods.   Multi-high pressure fuel combustion injection propulsion that receives liquid oxygen (5K) + electricity + high-temperature water and is equipped with a theoretical combustion chamber (4Q) air suction channel, which is a vertical all blade water gravity turbine (8V) generator + Both-side center support bearing load coalescence 0 approach counter-rotating production compressed air (28a) combustion simple injection engine (88o) extra large Osprey (7y) driven various energy storage cycle coalescence engine and coalescence method.   Theoretical combustion blade hydrogravity turbine (8V) power generation electricity production, receiving liquid oxygen (5K) and making the compression volume 21/60000 of the air compression multiple theoretical combustion chambers (4Q) + both sides center support bearing load Combined zero approaching counter-rotating manufactured compressed air (28a) combustion simple engine (88o) oversized Osprey (7y) driven various energy storage cycle coalescing engine and coalescence method.   Theoretical combustion blade (4Q) super high-pressure fuel combustion + center of both sides, receiving liquid oxygen (5K) and making the compression volume 21/60000 of the air compression of vertical type moving blade water gravity turbine (8V) power generation electricity production Various types of energy storage cycle coalescence engines and coalescence methods that drive a simple gas engine (88m) large osprey (7z) as compressed air (28a) combustion with support bearing load coalescence 0 approaching counter-rotating production.   Vertical all-blade hydrogravity turbine (8V) power generation electricity production, receiving liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 approach double reversal Various energy storage cycle coalescing engine and coalescence method for driving a simple gas engine (88m) large osprey (7z) as a compressed air (28a) combustion.   Received liquid oxygen (5K) + electricity + high temperature water, vertical combustion chamber (4Q) ultra high pressure fuel combustion + double-sided center support bearing combined load 0 approach of vertical-type all-bladed water gravity turbine (8V) power generation electricity production Various energy storage cycle coalescence engine and coalescence method driven by simple gas engine (88m) large osprey (7z) as counter-rotating manufactured compressed air (28a) combustion.   Theoretical combustion blade (4Q) super high-pressure fuel combustion + center of both sides, receiving liquid oxygen (5K) and making the compression volume 21/60000 of the air compression of vertical type moving blade water gravity turbine (8V) power generation electricity production Various types of energy storage cycle coalescence engines and coalescence methods for driving a large gas spray (7z) by driving a plurality of simple gas engines (88m) 1 as combustion of compressed air (28a) with support bearing load coalescence.   Vertical all-blade hydrogravity turbine (8V) power generation electricity production, receiving liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 approach double reversal Various energy storage cycle coalescing engines and coalescence methods for driving a large gas spray (7z) by driving one or more simple gas engines (88m) as combustion of compressed air (28a).   Received liquid oxygen (5K) + electricity + high temperature water, vertical combustion chamber (4Q) ultra high pressure fuel combustion + double-sided center support bearing combined load 0 approach of vertical-type all-bladed water gravity turbine (8V) power generation electricity production Various energy storage cycle coalescence engine and coalescence method for driving a large osprey (7z) by driving one or more simple gas engines (88m) as a counter-rotating manufactured compressed air (28a) combustion.   Theoretical combustion blade (4Q) super high-pressure fuel combustion + center of both sides, receiving liquid oxygen (5K) and making the compression volume 21/60000 of the air compression of vertical type moving blade water gravity turbine (8V) power generation electricity production Various types of energy storage cycle coalescence engines and coalescence methods for driving a large gas spray (7z) by driving a plurality of simple gas engines (88m) 1 as combustion of compressed air (28a) with support bearing load coalescence.   Vertical all-blade hydrogravity turbine (8V) power generation electricity production, receiving liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 approach double reversal Various energy storage cycle coalescing engines and coalescence methods for driving a large gas spray (7z) by driving one or more simple gas engines (88m) as combustion of compressed air (28a).   Received liquid oxygen (5K) + electricity + high temperature water, vertical combustion chamber (4Q) ultra high pressure fuel combustion + double-sided center support bearing combined load 0 approach of vertical-type all-bladed water gravity turbine (8V) power generation electricity production Various energy storage cycle coalescence engine and coalescence method for driving a large osprey (7z) by driving one or more simple gas engines (88m) as a counter-rotating manufactured compressed air (28a) combustion.   Theoretical combustion blade (4Q) super high-pressure fuel combustion + center of both sides, receiving liquid oxygen (5K) and making the compression volume 21/60000 of the air compression of vertical type moving blade water gravity turbine (8V) power generation electricity production Various types of energy storage cycle coalescence engine and coalescence method for driving a simple gas engine (88m) and driving a large osprey (7z) as combustion in compressed air (28a) combustion with support bearing load coalescence 0 approach.   Theoretical combustion blade (4Q) super high-pressure fuel combustion + center of both sides, receiving liquid oxygen (5K) and making the compression volume 21/60000 of the air compression of vertical type moving blade water gravity turbine (8V) power generation electricity production Various types of energy storage cycle coalescence engines and coalescence methods for rotating a simple gas engine (88m) drive propeller (7A) and driving a large osprey (7z) as combustion in compressed air (28a) combustion with support bearing load coalescence 0 approaching counter-rotating production.   Vertical all-blade hydrogravity turbine (8V) power generation electricity production, receiving liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 approach double reversal Various energy storage cycle coalescing engine and coalescence method for rotating a simple gas engine (88m) drive propeller (7A) and driving a large osprey (7z) as a compressed air (28a) combustion.   Received liquid oxygen (5K) + electricity + high temperature water, vertical combustion chamber (4Q) ultra high pressure fuel combustion + double-sided center support bearing combined load 0 approach of vertical-type all-bladed water gravity turbine (8V) power generation electricity production Various energy storage cycle coalescence engines and coalescence methods for rotating a simple gas engine (88m) drive propeller (7A) and driving a large osprey (7z) as counter-rotating manufactured compressed air (28a) combustion.   Theoretical combustion blade (4Q) super high-pressure fuel combustion + center of both sides, receiving liquid oxygen (5K) and making the compression volume 21/60000 of the air compression of vertical type moving blade water gravity turbine (8V) power generation electricity production Support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) Combustion with simple gas engine (88m) 1-multiple drive propeller (7A) multiple energy storage cycle coalescence engine and coalescence driven multiple rotations (7z) Method.   Vertical all-blade hydrogravity turbine (8V) power generation electricity production, receiving liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 approach double reversal Various energy storage cycle coalescing engines and coalescence methods for producing simple compressed air (28a) combustion as simple gas engine (88m) 1 -multiple drive propeller (7A) and driving large osprey (7z).   Received liquid oxygen (5K) + electricity + high temperature water, vertical combustion chamber (4Q) ultra high pressure fuel combustion + double-sided center support bearing combined load 0 approach of vertical-type all-bladed water gravity turbine (8V) power generation electricity production Various energy storage cycle coalescence engines and coalescence methods for driving a large gas spray (7z) by rotating a simple gas engine (88m) 1 to a multiple drive propeller (7A) as counter-rotating manufactured compressed air (28a) combustion.   Theoretical combustion blade (4Q) super high-pressure fuel combustion + center of both sides, receiving liquid oxygen (5K) and making the compression volume 21/60000 of the air compression of vertical type moving blade water gravity turbine (8V) power generation electricity production Support bearing load coalescence 0 approaching counter-rotating production Compressed air (28a) Combustion with simple gas engine (88m) 1-multiple drive propeller (7A) multiple energy storage cycle coalescence engine and coalescence driven multiple rotations (7z) Method.   Vertical all-blade hydrogravity turbine (8V) power generation electricity production, receiving liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 approach double reversal Various energy storage cycle coalescing engines and coalescence methods for producing simple compressed air (28a) combustion as simple gas engine (88m) 1 -multiple drive propeller (7A) and driving large osprey (7z).   Received liquid oxygen (5K) + electricity + high temperature water, vertical combustion chamber (4Q) ultra high pressure fuel combustion + double-sided center support bearing combined load 0 approach of vertical-type all-bladed water gravity turbine (8V) power generation electricity production Various energy storage cycle coalescence engines and coalescence methods for driving a large gas spray (7z) by rotating a simple gas engine (88m) 1 to a multiple drive propeller (7A) as counter-rotating manufactured compressed air (28a) combustion.   Theoretical combustion blade (4Q) super high-pressure fuel combustion + center of both sides, receiving liquid oxygen (5K) and making the compression volume 21/60000 of the air compression of vertical type moving blade water gravity turbine (8V) power generation electricity production Various types of energy storage cycle coalescence engines and coalescence methods for rotating a simple gas engine (88m) drive propeller (7A) and driving a large osprey (7z) as combustion in compressed air (28a) combustion with support bearing load coalescence 0 approaching counter-rotating production.   Theoretical combustion blade (4Q) super high-pressure fuel combustion + center of both sides, receiving liquid oxygen (5K) and making the compression volume 21/60000 of the air compression of vertical type moving blade water gravity turbine (8V) power generation electricity production Various types of energy storage cycle coalescence engine and coalescence method for driving a simple gas engine (88m) driven simple injection engine (88o) extra large osprey (7y) as compressed air (28a) combustion with support bearing load coalescence 0 approaching counter-rotating production.   Vertical all-blade hydrogravity turbine (8V) power generation electricity production, receiving liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 approach double reversal Various energy storage cycle coalescing engine and coalescence method for driving simple gas engine (88m) driving simple injection engine (88o) extra large Osprey (7y) as manufactured compressed air (28a) combustion.   Received liquid oxygen (5K) + electricity + high temperature water, vertical combustion chamber (4Q) ultra high pressure fuel combustion + double-sided center support bearing combined load 0 approach of vertical-type all-bladed water gravity turbine (8V) power generation electricity production Various energy storage cycle coalescence engine and coalescence method for driving a simple gas engine (88m) driving simple injection engine (88o) extra large Osprey (7y) as counter-rotating manufactured compressed air (28a) combustion.   Theoretical combustion blade (4Q) super high-pressure fuel combustion + center of both sides, receiving liquid oxygen (5K) and making the compression volume 21/60000 of the air compression of vertical type moving blade water gravity turbine (8V) power generation electricity production Support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) combustion as simple gas engine (88m) 1 to plural driving 1 to plural simple injection engine (88o) extra large Osprey (7y) driving various energy storage cycle coalescing engine and Merge method.   Vertical all-blade hydrogravity turbine (8V) power generation electricity production, receiving liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 approach double reversal Various energy storage cycle coalescence engines and coalescence methods that drive simple gas engine (88m) 1-multiple drive 1-multiple simple injection engine (88o) extra large osprey (7y) as production compressed air (28a) combustion.   Received liquid oxygen (5K) + electricity + high temperature water, vertical combustion chamber (4Q) ultra high pressure fuel combustion + double-sided center support bearing combined load 0 approach of vertical-type all-bladed water gravity turbine (8V) power generation electricity production Various energy storage cycle coalescence engine and coalescence method for driving a simple gas engine (88m) 1 to multiple drives 1 to multiple simple injection engines (88o) extra large Osprey (7y) as counter-rotating manufactured compressed air (28a) combustion.   Theoretical combustion blade (4Q) super high-pressure fuel combustion + center of both sides, receiving liquid oxygen (5K) and making the compression volume 21/60000 of the air compression of vertical type moving blade water gravity turbine (8V) power generation electricity production Support bearing load coalescence 0 approaching counter-rotating production compressed air (28a) combustion as simple gas engine (88m) 1 to plural driving 1 to plural simple injection engine (88o) extra large Osprey (7y) driving various energy storage cycle coalescing engine and Merge method.   Vertical all-blade hydrogravity turbine (8V) power generation electricity production, receiving liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load coalescence 0 approach double reversal Various energy storage cycle coalescence engines and coalescence methods that drive simple gas engine (88m) 1-multiple drive 1-multiple simple injection engine (88o) extra large osprey (7y) as production compressed air (28a) combustion.   Received liquid oxygen (5K) + electricity + high temperature water, vertical combustion chamber (4Q) ultra high pressure fuel combustion + double-sided center support bearing combined load 0 approach of vertical-type all-bladed water gravity turbine (8V) power generation electricity production Various energy storage cycle coalescence engine and coalescence method for driving a simple gas engine (88m) 1 to multiple drives 1 to multiple simple injection engines (88o) extra large Osprey (7y) as counter-rotating manufactured compressed air (28a) combustion.   Theoretical combustion blade (4Q) super high-pressure fuel combustion + center of both sides, receiving liquid oxygen (5K) and making the compression volume 21/60000 of the air compression of vertical type moving blade water gravity turbine (8V) power generation electricity production Various types of energy storage cycle coalescence engine and coalescence method for driving a simple gas engine (88m) driving simple injection engine (88o) and multiple extra large osprey (7y) as combustion of compressed air (28a) combustion with support bearing coalescence 0 approaching counter-rotating production.

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