JP2014005753A - 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 100 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. Gravity acceleration in vacuum, and turbines with heads of 500-828m 10000 times the existing pumped-storage power generation Horizontal power blade specific material gravity turbine 8U power generation electric drive simple multistage compressor as a power generation that requires zero fuel cost experiment of boiler and nuclear reactor abolition aiming at power generation amount The t + liquid oxygen production machine 88g, the simple gas engine 88d, the simple water injection engine 88e, the simple injection engine 88f, and the simple multistage compressor 3t are driven. Manufactured and divided and stored in 24 to 200 MPa superheated steam 50 heat + liquid air 28a cold heat, as electricity + liquid air cold heat + superheated steam heat supply equipment 3D, various heat utilization + liquid use infinite application, ships and vehicles For example, ships, vehicles, airplanes, etc. receive liquid oxygen, make the compression volume work rate 21/20000 volume work of air compression, and make the compression pressure of liquid oxygen or water 20 times easier, etc. Rotational force drive of simple gas engine 88d, combined injection propulsion of simple injection engine 88f and simple water injection engine 88e Nitrogen, oxygen, and CO2 are supplied to the plant. Microorganisms and seaweeds are increased, and food such as fish is greatly increased in the food chain. CO2 emissions are reduced to 1/10 and fuel costs are reduced to 1/10 and 1 / 500,000 when driven by airplanes and automobiles. The present invention relates to the technology of the space space aiming, planes and ships aiming at 10 times speed, various energy conservation cycle coalescence engines and various energy conservation coalescence methods.

  The most existing car-driven reciprocating engine in the world consumes enormous amount of fuel by compressing air. Horizontal type rotor blade specific material gravity turbine 8U vacuum specific material gravity acceleration power generation Electricity + liquid air cold heat + superheated steam Supply from thermal supply equipment 3D, for example, superheated steam is injected into methane hydrate under permafrost and underwater, methane and water are divided into methane and liquid nitrogen cooled liquid methane, and liquid oxygen chamber 5K receives liquid oxygen 5K. Compression of liquid oxygen 5K, compression volume work rate is 21/60000 volume work of air compression, 24-200MPa ultra high pressure compression injection, liquid oxygen 5K + liquid fuel 1b + high temperature water 52a is compressed theoretical combustion to ultra high pressure The fuel is injected and burned in the process of injecting each into the theoretical combustion chamber 4Q by heating at the inner periphery of the chamber 4Q, etc. The superheated steam 50 is heated by the high-pressure high-temperature water heating pipe 5H in the high-temperature combustion, and the two-way center support high-speed double reversal including the driving of the simple gas engine 88d etc. is performed with the liquid oxygen 0. The combustion gas 49 + superheated steam 50 is injected from the high-pressure / high-temperature combustion gas control valve 5a and the combustion gas injection nozzle 6Y, and the simple gas engine 88d is driven to drive various vehicles such as automobiles and tillers, propellers 7A and rotor blades. Driving 7B and screw 7C, driving various vehicles, propeller airplanes and screw ships, aiming at fuel cost 1/10 and 10 times speed by using liquid oxygen 5K of electricity generation electricity generation, excellent operating profit rate The present invention relates to a technology for combining various energy conservation cycle coalescence engines and coalescence methods in the world.

  The existing jets are also blocked by stationary blades and consume a huge amount of fuel by air compression, such as zero output, and the rotational output and propulsion propulsion output are very small. As the aim of propulsion injection of liquid compression simple injection engine 88f combined with a horizontal type, all-blade ratio critical material gravity turbine 8U power generation electric drive many 1 to multiple stage simple multistage compressor 3t etc. heat pump 1G + solar heater 21 heat production Is divided into 24 to 200 MPa high-temperature water to superheated steam temperature 50 + liquid air cold heat 28a, and as an electric + liquid air cold heat + superheated steam temperature supply facility 3D, the propulsion of the airplane is liquid oxygen 5K + liquid fuel 1c + high-pressure high-temperature water Receiving at 52a, the compression volumetric power is compressed by liquid oxygen compression and compressed by ultra-high pressure at 21/60000 volumetric power of air compression, and each is a simple injection engine 8f Theoretical combustion chamber 4Q is not shown in the inner peripheral view of the fuel heating pipe 1L water heating pipe 5H oxygen heating pipe 5F, the heating optimum temperature is set, and the fuel control valve 25b + oxygen control valve 24D + superheated steam control valve 25 not shown is opened. Then, each of them is injected and burned into a theoretical combustion chamber 4Q aiming at one or more theoretical air-fuel ratio ultra-high pressure combustion, and as an oxygen injection nozzle 6L fuel injection nozzle 6X multiple combustion, superheated steam 50 heat recovery rocket injection + rocket combustion combustion gas injection nozzle 6Y In the injection, the forward air is aimed at coalescence such as suction injection, the high-speed counter-rotating compressed air 28a is combusted and added in the both-side center support, and the theoretical combustion chamber 4Q superheated steam injection nozzle 6A superheated steam 50 is combusted by 200 MPa target injection. In the rocket combustion that sucks and injects gas 49, the space arrival cost is aimed at 1 / 500,000, and the earth travels 16 times a day by space flight close to zero fuel cost. Anywhere on the planet to allow a day trip, aimed at profit margins preeminent world in a variety of space shuttle airplane class, relates to a technology of various energy conservation cycle combined institutions and coalescence method.

  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, the air compressor of the liquid oxygen production machine 88g is also added the use of simple multi-stage compressor 3t that is simple in theory, horizontal type full blade ratio material gravity turbine 8U power generation electric drive 1 to multi-stage simple As a heat pump 1G compression such as multistage compressor 3t, solar heater 21 solar heating air is compressed to high temperature, high pressure high temperature water heating pipe 5H heat recovery divided and stored, 24 to 200 MPa high temperature water 52a to superheat Steam 50 hot + liquid air 28a cold and stored separately, as electricity + liquid air cold + superheated steam hot water supply equipment 3D, liquid oxygen 5K + liquid fuel 1c + hot water 52a in the process of receiving Aiming at compression of 200 MPa, the liquid oxygen control valve 5T + liquid fuel control valve 1K + water control valve 5Q (not shown) are opened and heated to the optimum temperature in the inner periphery of the simple water injection engine 88e theoretical combustion chamber 4Q, respectively. 88e and the simple gas engine 88d are driven to make the water suction injection propulsion of the simple water injection engine 88e and the screw 7C rotation propulsion of the simple gas engine 88d. The screw propulsion simple gas engine 88d exhaust is the bottom bottom exhaust injection propulsion, which accelerates natural phenomena in the process of friction reduction injection propulsion and supplies oxygen, nitrogen, CO2 etc. into the sea, microbes, phytoplankton, seaweeds, corals, The present invention relates to technologies for various energy conservation cycle coalescence engines and coalescence methods that aim to increase the food of breeding human beings and increase the food of human beings and aim at the world's best profit rate.

  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 it impossible for natural phenomena to rise in the temperature of the entire sea surface, 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 From the electric + liquid air cold heat + superheated steam temperature heat supply equipment 3D, which is compressed and recovered multiple times with a heat pump 1G such as a machine 3t and divided and stored in 24-200 MPa high-temperature water 52a-superheated steam heat 50 + liquid air cold heat 28a Supply it to the liquid oxygen chamber 5K, storage battery, etc., make the liquid air driven car, airplane or ship a short time 1/10 fuel cost drive or 10 times speed drive, space flight, air flotation ship, etc. There are backgrounds in which extremely low-cost power generation battery drive and electric drive, and prevention of global warming with little CO2 emissions can be obtained.

  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 a fuel cost 0 power generation electric drive 1 to multiple-stage simple multistage compressor 3t + liquid oxygen production machine 88g. The recovered heat is recovered, divided into 5 L of cold liquid oxygen and 5 L of liquid nitrogen + hot high-temperature water 52a to superheated steam 50, and in the process of infinite use of heat, for example, superheated steam 50 is applied to methane hydrate under permafrost. Divide into injected methane and water, recover methane with liquid nitrogen-cooled liquid methane, continue superheated steam injection forever, make the methane recovery enclosure grazing at a suitable temperature and with many water droplets, and increase human food use heat Infinitely, aiming to reach 1 / 500,000 in space as a liquid air coalesced car, ship and spacecraft, and speeding up natural phenomena in the ship driving process 2a, microbes, seaweeds and coral The increase the food of fish such as the human race in the growth the food chain, etc., to prevent the heavy rain of sea water there is a background that can put off the human race extinct. Revolution of employment growth that will increase the employment by making the manufacturing operation monopolized 100% worldwide, with the operating profit rate becoming 10 times larger than the existing operational profit ratio, as the ship revolution and airplane revolution aiming at 10 times speed with low fuel cost There is a background that can be.

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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 are 31 applications including PCT until May 30, 2012, the filing date of Japanese Patent Application No. 2012-122750.

  In the existing thermal power plants in the world, the total heat generation is 7 degrees Celsius, and the seawater temperature rise is 1000 times in 100 years, and the downdrafts and updrafts are increased as much as possible. As the number of storms, torrential rains, heat waves, cold waves, etc. increases without limit, typhoons, seasonal winds, tornadoes, etc., around 100 years in the sea near Japan, salt water on the land due to concentrated heavy rains, etc. Covering increases the danger of human land food loss, making it impossible for the natural phenomenon of supplying nutrients to the sea-cooled seabed in winter, dramatically reducing microorganisms, phytoplankton, seaweeds, corals, etc., fish through food chains, etc. The number of human underwater foods has been reduced as much as 1/100, and droughts, torrential rains, typhoons and seasonal winds have increased 10 times in 100 years. For example, typhoons and seasonal winds have an upper limit such as 300m / sec. weather Giant seafloor rock expansion earthquake and tsunami 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 low cost electric drive all, heat production by solar heater 21 + 1 to multistage simple multistage compressor 3t + liquid oxygen production machine 88g, electricity + liquid air cold heat + As the high temperature water to superheated steam temperature supply facility 3D, the received liquid oxygen 5K is compressed to a 21/60000 volumetric compression work rate of air compression, and the superheated steam is used as the theoretical combustion chamber 4Q that can easily perform ultrahigh pressure combustion or ultrahigh temperature combustion. Heating 50 allows theoretical air-fuel ratio combustion, combined with existing technical improvement invention as rocket combustion, simple gas engine 88d, simple water injection engine 88e and simple injection engine 88f driven by theoretical combustion chamber 4Q, Vehicles, ships, and airplanes are driven by rotational force and propulsion propulsion, and ship propulsion propulsion drives rapid levitation and speeds up natural phenomena with short rocket injection. a. Supply oxygen, nitrogen, CO2, etc. into the sea, increase microorganisms, phytoplankton, seaweeds, corals, fish, etc. As a power generator, ship, airplane, car, etc. that operates 100% of the world's monopoly and operates in a top-secret manner, it is an excellent profit margin. Make it the world's number one, the best in the world for new employment, prevent droughts, torrential rains, typhoons, seasonal winds, heavy rains in seawater, and huge earthquakes and tsunamis to prevent 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 = Mach 30 aiming for 30 times power generation target, and mercury injection aiming for 406 times power generation target, but experiments are necessary, but the power generation cost will be greatly reduced to 1/10 etc. to increase the employment of electrical products infinitely effective.

The green earth is a miracle product and has a high risk of approaching other stars. For example, if China continues to grow 10% for 100 years, the temperature rise in the sea near China will exceed 1000 times due to thermal power generation and nuclear power generation. There is a strong possibility that the extinction of mankind will rapidly approach within 100 years, such as the increase in guerrilla heavy rain in Japan is 1000 times the heavy rain in seawater, the current drastic decrease in fish is close to 0, etc. Electric power drive is required. Therefore, the fuel cost is 0. Electricity generated by power generation + liquid air cold heat + high temperature water to superheated steam temperature heat supply equipment 3D receives liquid oxygen 5K, etc., and the compression work rate of combustion oxygen is 21/60000 volumetric compression work of air compression The theoretical combustion chamber 4Q can drive the simple gas engine 88d, the simple water injection engine 88e, and the simple injection engine 88f most efficiently as the increase of the super high pressure superheated steam 50 by the super high pressure high temperature combustion near the center of the theoretical combustion chamber 4Q. In addition to the effect that the fuel cost can be aimed at 1/10 or 10 times the speed of automobiles, ships, and airplanes, the space arrival cost can be aimed at 1 / 500,000 of existing space rockets, wheels and screws 7C, propeller 7A and rotor blade 7B are driven by a simple gas engine 88d, and a ship, an airplane, an automobile, etc. are driven by a rotational force. The effect of increasing the digestive capacity of medium microorganisms such as CO2 to tens of thousands of times of the forest is great, and phytoplankton, seaweeds, corals, etc. are proliferated, and fish food such as fish is greatly increased in the food chain etc. It prevents desertification, droughts, torrential rains, typhoons, seasonal winds, and earthquake tsunamis, delays the most important human race extinction, and aims to achieve the world's best profit rate.

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 with a high-temperature water heating pipe 5H etc. on the inner periphery of 4Q, the fuel injection nozzle 6X + oxygen injection nozzle 6L is opened, oxygen gas + fuel gas is mixed and ignited near the center, and the inner periphery of the theoretical combustion chamber 4Q The theoretical combustion chamber 4Q that optimally heats the fuel + oxygen + high-temperature water heating pipe 5H and superheats to the super-high-pressure high-temperature superheated steam 50, etc. By driving the simple injection engine 88f, the space arrival cost is aimed at 1 / 500,000 of the existing space rocket, and the same fuel cost is 10 times the injection propulsion output. Jet jet 100 times pressure 10 times calorie injection Short time 1000 times propulsion propulsion output aiming at propeller flight, rotor blade flight and injection propulsion with low fuel cost in the atmosphere, superheated steam injection speed and combustion gas injection speed are in vacuum Therefore, the mass injection of the existing space rocket on the ground is considered the worst. From the vicinity of the highest flight altitude of the existing aircraft, the injection amount of the high pressure high temperature combustion chamber 5M + high pressure high temperature superheated steam 50 of 24 to 200MPa is increased, It has the effect of aiming for a prime use of space where you can take a day trip anywhere on the planet.

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 88g (Example 4) Explanatory drawing of the simple multistage compressor 3t (Example 5) Explanatory drawing of simple gas engine 88d (Example 6) Explanatory drawing of the simple water injection engine 88e (Example 7) Explanatory drawing of the simple injection engine 88f (Example 8) Illustration of simple gas locomotive 7d (Example 9) Explanatory drawing of the simple gas engine ship 7e (Example 10) Explanatory drawing of the simple gas engine airplane 7f (Example 11) Explanatory drawing of the simple water injection engine ship 7G (Example 12) Explanatory drawing of the simple injection engine airplane 7h (Example 13) Explanatory drawing of the rotary wing airplane 7i (Example 14) Explanatory drawing of the rotary wing jet airplane 7j (Example 15)

  The use of gravity acceleration in vacuum for a long period of time is prevented by brainwashing such as existing steam turbine power generation, and one unit of 100 sets prevents the aim of generating power 43,000 times that of one existing steam turbine power generation, for example, the existing best steam turbine power generation Steam pressure is reduced by reducing the atmospheric pressure, the same speed, and the same volumetric power, kg weight m / second, to 1/1700 of the water power, and by installing the stationary blades alternately with the moving blades and blocking the rotation output to zero. The seawater temperature rises by 7 degrees with all of the driving heat of the sea, the fishes are drastically reduced, the bottom bedrock is expanded into earthquakes and tsunamis, and the typhoon, seasonal winds and sea tornadoes in the sea near Japan are increased to about 100 m / sec. There is a danger that food extinctions and humankind extinction will be approaching rapidly by providing salt coating on the land in around 50 to 100 years, such as heavy rain of suction seawater is expected over the sea. 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 Will be explained in substitution for three examples, and we will try to materialize the invention without common sense.

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 provided in the existing highest building height of 828m vertically, and one unit is provided. For example, the mercury 3E platinum ball 2E is raised vertically by 828m, etc. The platinum ball 2E is mixed and injected with a large material accelerator 6W at a pressure of mercury 3E to aim Mach 28 injection, driven by acceleration of gravity acceleration and vacuum, and the cylindrical turbine blade group 8A is counter-synchronously rotated by the counter-synchronous gear 4C. The rotating gear 4D is rotated at the same speed and in the same direction, such as 100 pairs, making it easy to mass-produce cheaply, eliminating the need for boilers and nuclear reactors, and accelerating the mercury acceleration etc. The generator 1 is selectively provided as an opposing synchronous gear 4C main shaft or a series co-rotating gear 4D main shaft, and more than 100 sets of driving power generation costs outside the turbine outer casing 77a are aimed at 1/10, and the structure is extremely Simple and extremely inexpensive electric product infinite and electric drive infinite, making the world's best energy conservation cycle combined engine power generation and combined method power generation with outstanding profitability.

The horizontal full-blade ratio critical material gravity turbine 8U power generation is composed of 100 units, such as 100 sets, vertically installed in the highest building 828m in the turbine outer box 77a. 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 used for the drop 828m, and compared with the final stage of the existing steam turbine power generation, the vacuum degree is 30mmHg water 43,000 times volume Mach 1 speed steaming As a simple comparison with 100 turbines of one turbine 8U power generation amount, 1/1000 volume of mercury is 43 × 100 × 13, 55 = 58265 times mercury power generation amount by Mach 1 speed injection, and platinum ball is 91891 The energy saving cycle coalescence engine fuel cost becomes 0 extremely low-cost power generation, which results in the power generation amount of astronomical magnification that requires experiments such as calculation of double 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 has a buoyancy on the surface of the water or a circular railroad on the flat ground, and the solar heater 21 is used as a floating device or a land device for maintaining and rotating sunlight at right angles from east to west. Is provided with a rotation support part 4f, and equipped with a gear unit 4d and a roller 4e, and as a cylindrical rotation part 77G, it controls the vertical rotation of sunlight in the vertical direction, and controls the rotation of the vertical direction in the east-west direction by using buoyancy and circular railway. , By controlling the rotation of sunlight in two directions at right angles, and setting it as a device that 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 heats it near the focal length. Absorption tube 4H The internal air passage 28A air 28a temperature is maximized, the external air passage 28A air 28a temperature is also increased, and the existing lens cross section is linearly extended as a rectangular long lens 2d. A heat insulating material 2c such as a cylinder is surrounded by a cylindrical rotating portion 77G or the like to make a long cylinder such as a cylinder, a long long lens 2d is a joint 80A + fastener 80B, and a sealed upper part is a 4H external air passage 28A. Intake and compression as 1 to multi-stage heat pump 1G for suction, simple multi-stage compressor 3t or the like as heat pump 1G is set to 800 to 1200 ° C. multiple times, and heat recovery is repeatedly performed by 1 to multi-stage compression heat recovery unit 2C. Then, the liquid air 28a cold heat is stored in the liquid oxygen chamber 5K + liquid nitrogen chamber 5L, and the 24-heat of about 200-400 MPa superheated steam is divided and stored in the high-pressure high-temperature steam chamber 5N. Electrical + liquid air cold + using various applications in the superheated steam heat supply facilities 3D, the electric drive flourish and battery driven prime, to various thermal utilization prime and various cold use PRIME electrical product.

  The liquid oxygen producing machine 88g, which is long and fast and easy to rotate in the reverse direction by supporting both sides in FIG. 4, can be used as the assembly assembly part 9M for a simple annular part by making the horizontal axis 1h double inversion. Fully automatic mass production, full automatic machining, easy assembly, aiming at 1/100 parts count, simple multistage compressor 3t connection aim, horizontal full blade ratio material gravity turbine 8U fuel cost 0 power generation extremely cheap electric drive In the case of multi-stage compression, a simple multi-stage compressor 3t and coupled drive compression are used, and in the case of single-stage compression, the heat production heated air 28a of the solar heater 21 is compressed and recovered, and water heating isothermal production + rectification Preparation of production of liquid oxygen + liquid nitrogen, etc. by cooling the tower exhaust pipe 5h, ultra-high-pressure compressed air 28a is driven into the air turbine 3u by super-high-speed injection and counter-rotating to generate a large rotational output, thereby greatly reducing the motor drive power Rectifying tower exhaust As in the existing technology, the liquid oxygen is purified to liquid oxygen + liquid nitrogen and the exhaust gas is supplied to the rectifying tower exhaust gas pipe 5h, and the liquid oxygen production machine 88g is driven by continuous mass production of hot and cold, and electricity + Supply to liquid air cold heat + high temperature water to superheated steam heat supply equipment 3D, for example, in heat supply, inject methane into the methane hydrate under the seabed or permafrost, and recover methane under permafrost It is set up and recovered from the tip of the top of the specific gravity difference utilization, and 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 21/21 of air compression Combined with 60000 volume liquid oxygen drive, simple gas engine 88d drive, simple water injection engine 88e drive and simple injection engine 88f drive, various rotational drives such as car drive, ship drive and airplane drive As a propulsion drive ultra-high-speed injection, in the case of an airplane drive to allow for day trips aim anywhere universe reaching cost 1/50 ten thousand aim on earth, to liquid oxygen production unit 88g.

The simple multi-stage compressor 3t, which is long and fast and easy to reverse by supporting both sides in the center shown in FIG. Easy to manufacture, fully automatic processing, easy to assemble, 1/100 number of parts, vertical type moving blade water gravity turbine 8P fuel cost 0 power generation extremely cheap electric drive, liquid oxygen production machine 88g in case of multi-stage compression And the like, and the compressed air recovery of the heated air 28a and the like by the solar heater 21 is repeated one or more times, and the superheated steam 50 heat production such as water heating + the compressed air 28a cold heat production is repeated one or more times. In order to make mass production of ultra-high pressure superheated steam 50 warm heat + ultrahigh-pressure compressed air 28a cold and aim at 1/10 production cost of the existing liquid oxygen production cost, both sides of each of the inner shaft device 60A and outer shaft device 60B are Central support A simple multi-stage compressor that can support all conditions by supporting a magnetic bearing, etc., and making the bearing load close to 0, enabling a large and large ultra high speed counter rotating compressor and a micro ultra high speed counter rotating compressor. 3t, the assembling part 9M is a final assembly that protrudes from the compressor outer box 77b as shown in the figure at the time of preceding assembly, with the counter-rotating machine outer box 77C divided into two parts at the horizontal axis 1h. Each of the outer compression blades 8m has a middle annular blade in the fitting assembly portion 9M fitting assembly, and thirdly, the inner compression blade 8k front annular blade has a fitting assembly portion 9M fitting assembly in the center support. The outer compression blade 8m front annular blade is provided with a center support for each of the fitting assembly portions 9M and the fourth compressor outer box 77b is provided with each of the fitting assembly portions 9M. Reversing machine outer box 77C with horizontal axis 1h Simplifies multistage compressor 3t of 1 to a plurality of stages for repeating a three-stage simple compressor 3s provided, like for driving the liquid oxygen production unit 88g connected to apply the configuration and assembly in the horizontal axis 1h-rotating driving all.

The simple gas engine 88d, which supports both sides of the center in FIG. 5 and facilitates long and high speed double reversal, can be used as a fitting assembly 9M assembly of simple annular parts by making the horizontal axis 1h double reversal. Aiming at automatic mass production, full automatic machining, easy assembly, 1/100 parts count, simple multistage compressor 3t connection, horizontal full blade ratio material gravity turbine 8U fuel cost 0 power generation extremely cheap electric production, Compressed liquid oxygen + electricity + hot water from the electricity + liquid air cold heat + hot water to superheated steam hot water supply facility 3D to the theoretical combustion chamber 4Q, etc. driven by cheap electric products, and compresses the liquid oxygen. Volumetric work rate is 21/60000 volumetric compression work rate of air compression, liquid oxygen + liquid fuel + high temperature water is compressed and heated to ultra high pressure such as 24-200MPa, and multiple opening / closing valves 1Q are closed to two types of rockets Combustion theory In the chamber 4Q, the oxygen + fuel injection combustion heated to the optimum temperature from the oxygen injection nozzle 6L + fuel injection nozzle 6X is performed, and the fuel + oxygen + superheated steam 50 is heated to the optimum temperature on the inner wall of the theoretical combustion chamber 4Q to achieve the theoretical air-fuel ratio combustion. Aiming at 10 times the pressure 10 times the combustion amount of the existing technology improved theoretical combustion chamber 4Q high pressure high temperature combustion chamber 5M, the existing technology improved theoretical combustion chamber 4Q is 200MPa as the stoichiometric air-fuel ratio combustion amount of the existing technology 4 times fuel The superheated steam 50 or the like is injected from the manufacturing superheated steam injection nozzle 6A, and the high-pressure high-temperature combustion chamber 5M having a fourfold combustion amount is sucked and injected by rocket injection. As a simple gas engine 88d close to the existing gas turbine, the compression power is reduced. Is a simple gas engine 88d that uses a combination of a plurality of liquid oxygen-driven theoretical combustion chambers 4Q with a 21/60000 volumetric compression power of air compression and uses even liquid oxygen 0 .

The case of driving the simple gas engine 88d with 0 liquid oxygen will be explained. The existing jet engine and the stationary vanes of the gas turbine are almost completely abolished, and the inside of the center support on both sides is provided by the counter rotating magnetic device 85 to the counter rotating gear device 85Y. The shaft device 60A + the outer shaft device 60B is counter-rotated and the air 28a sucked from the inlet stationary blade 6G is linearly compressed by the inner compression blade 8k + the outer compression blade 8m, and the counter-rotating linear compression 800-1200 ° C. is increased. A straight compression simple multistage compressor 3t is connected, and the relative speed of the existing gas turbine, etc. is doubled, and the compressed air pressure of the counter-rotating machine outer box 77C is set at a double reversing machine outer box 77C. Compressed air is injected into the theoretical combustion chamber 4Q from 6G, fuel is injected and combusted from the fuel injection nozzle 6X, and superheated steam 50 such as heat recovery 200 MPa is produced in the high-pressure high-temperature water heating pipe 5H. By using the same compressed air amount as a four-fold fuel combustion amount of an existing gas turbine, etc., the superheated steam 50 of 3/4 heat amount or 20 times pressure of the combustion gas 49 is rocket-injected and jointly with the combustion gas 49 The inner output blade 8n + outer output blade 8p is driven in reverse, and the same compressed air amount is aimed at a 10-times injection propulsion output or 10-times rotation output of an existing jet engine or gas turbine. The horizontal shaft 1h or the outer shaft device or The inner shaft device 60A is extended to rotate and drive generators, automobiles, ships, and airplanes. The airplanes and ships are additionally driven by injection with exhaust, and in the case of power generation, the simple gas engine 88d is exhausted. The whole is heat recovered by heat exchange heating air 28a, and the high temperature water 52b of the compressed water injection heat recovery is injected into the high pressure high temperature water heating pipe 5H by the inner compression blade 8k + outer compression blade 8m, and the air 28a is injected into the theoretical combustion chamber 4Q. Burning The power generation is repeated by injection combustion, and the power generation amount is further increased by the combined power generation of the high-temperature air 28a heated by the solar heater 21 in FIG. 11, and the exhaust heat and geothermal heat are similarly converted into the temperature of the air 28a and sucked compressed water jet compressed. Similarly, a simple gas engine 88d with an increased power generation amount is used.

The simple water injection engine 88e that is long and fast and easy to reverse in the center of both sides in FIG. 6 can be used as a fitting assembly 9M assembly of a simple annular part by making the horizontal axis 1h double inversion. Fully automatic mass production, full automatic processing, easy assembly, aiming at 1/100 parts count, simple multistage compressor 3t connection aim, horizontal full blade ratio material gravity turbine 8U fuel cost 0 power generation extremely cheap electric production By receiving liquid oxygen + electricity + high temperature water from the electricity + liquid air cold heat + high temperature water to superheated steam temperature heat supply equipment 3D to the theoretical combustion chamber 4Q etc. driven by an inexpensive electric product, and compressing the 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 and heated to ultrahigh pressure such as 24 to 200 MPa, and the on-off valve 1Q at the multiple inlet / outlet is closed to two types Rocket combustion In the theoretical combustion chamber 4Q, oxygen + fuel injection combustion heated to an optimum temperature from the oxygen injection nozzle 6L + fuel injection nozzle 6X is performed, and fuel + oxygen + superheated steam 50 is heated to the optimum temperature on the inner wall of the theoretical combustion chamber 4Q. Then, aiming at a 10-fold pressure and 10-fold combustion amount of the existing technological improved theoretical combustion chamber 4Q high-pressure high-temperature combustion chamber 5M, the superheated steam injection nozzle 6A + combustion gas injection nozzle 6Y of the suction flow of the theoretical combustion chamber 4Q outer air 28a to 200 MPa The superheated steam 50 and the high-pressure / high-temperature combustion chamber 5M that are approaching each other are injected, and the air 28a is suction-injected and water is suction-injected. Then, the superheated steam 50 is produced with the increased heat quantity and targeted at 200 MPa. Rotational output is generated in the high-pressure and high-temperature combustion chamber 5M, and the superheated steam is generated from the superheated steam injection nozzle 6A with the suction flow of the outer air 28a. 0, jetting forward air 28a and sucking and spraying water 52a, as a simple water injection engine 88e close to the existing jet engine, compression work rate is increased by 21/60000 volumetric compression work rate of air compression A simple water injection engine 88e that combines a plurality of liquid oxygen driven theoretical combustion chambers 4Q and uses even liquid oxygen zero.

The case of driving the simple water injection engine 88e with liquid oxygen 0 will be explained. The existing jet engine and the stationary blade of the gas turbine are almost completely abolished, and the center of both sides is supported by the counter rotating magnetic device 85 to the counter rotating gear device 85Y. The inner shaft device 60A + outer shaft device 60B is driven in a counter-rotating manner, and the air 28a sucked from the inlet stationary blade 6G is linearly compressed by the inner compression blade 8k + the outer compression blade 8m, and the counter-rotating linear compression simple multistage compressor 3t is connected. The relative speed of the existing gas turbine or the like is twice as high as that of the existing compressed gas pressure or the like, and the compressed air 28a is supplied to the theoretical combustion chamber 4Q from the compressed air injection vane 6G of the contra-rotating outer casing 77C. , The fuel is injected and combusted from the fuel injection nozzle 6X, and the heat recovery superheated steam 50 is made into the production theoretical air-fuel ratio combustion by the high-pressure and high-temperature water heating pipe 5H. The fuel combustion amount and the outer periphery are used as a rocket injection part, and superheated steam 50 of 3/4 heat amount or 20 times pressure of the combustion gas 49 is injected into the rocket outer box 77B. 8p is driven in reverse, with the same compressed air amount, aiming at 15 times injection propulsion output + 5 times rotation output of existing jet engines and gas turbines, equipped with a water suction injection part cylinder, to increase water suction injection speed and air suction amount Thus, the simple water injection engine 88e is used for the jet propulsion drive of the water-injecting vessels.

The simple injection engine 88f, which supports both sides and the center of FIG. 7 and facilitates long and high speed double reversal, can be used as a fitting assembly 9M assembly of a simple annular part by making the horizontal axis 1h double reversal. Fully automatic mass production, full automatic processing, easy assembly, aiming at 1/100 parts count, simple multistage compressor 3t connection aim, horizontal full blade ratio material gravity turbine 8U fuel cost 0 power generation extremely cheap electric production By receiving liquid oxygen + electricity + high temperature water from the electricity + liquid air cold heat + high temperature water to superheated steam temperature heat supply equipment 3D to the theoretical combustion chamber 4Q etc. driven by an inexpensive electric product, and compressing the 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 and heated to ultrahigh pressure such as 24 to 200 MPa, and the on-off valve 1Q at the multiple inlet / outlet is closed to two types Rocket combustion In the theoretical combustion chamber 4Q, oxygen + fuel injection combustion heated to an optimum temperature from the oxygen injection nozzle 6L + fuel injection nozzle 6X is performed, and fuel + oxygen + superheated steam 50 is heated to the optimum temperature on the inner wall of the theoretical combustion chamber 4Q. Thus, the superheated steam that is closer to 200 MPa than the superheated steam injection nozzle 6A + combustion gas injection nozzle 6Y on the outer periphery of the theoretical combustion chamber 4Q is aimed at 10 times the pressure 10 times the combustion amount of the existing technological improved theoretical combustion chamber 4Q high pressure high temperature combustion chamber 5M. 50 or high-pressure high-temperature combustion chamber 5M is injected, and when the on-off valve 1Q is closed, the high-power rocket combustion space utilization is primed. The driving rocket combustion chamber and jet combustion chamber are used, and in the existing technology improved theoretical combustion chamber 4Q, the theoretical air-fuel ratio combustion amount of the fuel four times that of the existing technology is increased by 200 MP with an increased heat amount. The target superheated steam 50 is rotated and generated in the high-pressure and high-temperature combustion chamber 5M, the superheated steam 50 is injected from the superheated steam injection nozzle 6A of the outer air 28a suction flow, the front air 28a is sucked and injected into the existing jet engine. As the simple injection engine 88f approached, a plurality of liquid oxygen drive theoretical combustion chambers 4Q are combined, and the simple injection engine 88f used even with liquid oxygen 0 is used.

The case of driving the simple injection engine 88f with 0 liquid oxygen will be explained. The existing jet engine and the stationary vanes of the gas turbine are almost completely abolished, and the inner sides of both side centers are supported by the counter rotating magnetic device 85 to the counter rotating gear device 85Y. The shaft device 60A + the outer shaft device 60B is driven in a counter-rotating manner, and the air 28a sucked from the inlet stationary blade 6G is linearly compressed by the inner compression blade 8k + the outer compression blade 8m, and the counter-rotating linear compression simple multistage compressor 3t is connected. With the relative speed of the existing gas turbine or the like, the compressed air pressure of 28 a is easily supplied to the theoretical combustion chamber 4Q from the compressed air injection vane 6G of the contra-rotating outer casing 77C. The fuel is injected and burned from the fuel injection nozzle 6X, and the heat recovery superheated steam 50 is made into the production theoretical air-fuel ratio combustion by the high-pressure high-temperature water heating pipe 5H. With the combustion amount of the fuel and the outer periphery as the rocket injection part, the superheated steam 50 of 3/4 heat amount or 20 times pressure of the combustion gas 49 is injected into the rocket outer box 77B, and the inner output blade 8n + outer output blade with the combustion gas 49 8p double reverse drive, aiming at the same compressed air amount 15 times injection propulsion output + 5 times rotation output of existing jet engines and gas turbines, making underwater injection ships and airplanes into injection propulsion drive etc. The engine 88f is selected.

The simple gas engine vehicle 7d in FIG. 8 is an improved invention of the existing micro gas turbine vehicle. The simple gas engine 88d is driven by compressed air + fuel cost 0 power generation electric product drive. Fuel cost 0 power generation Electricity + liquid air cold heat + high temperature water to superheated steam temperature heat supply equipment 3D, which is extremely inexpensive electricity production, receives liquid oxygen + electricity + high temperature water to the theoretical combustion chamber 4Q, etc. driven by low cost electric products By compressing liquid oxygen, the compression volume work rate is made to be 21/60000 volume compression work rate of air compression, and liquid oxygen + liquid fuel + high temperature water is compressed and heated to an ultrahigh pressure such as 24-200 MPa, and a plurality of inlets In the rocket combustion theoretical combustion chamber 4Q with the on-off valve 1Q 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 + superheated steam 50 is heated to the optimum temperature, and the theoretical air-fuel ratio combustion is performed, aiming at 10 times the pressure 10 times the combustion amount of the existing technological improved theoretical combustion chamber 4Q high pressure high temperature combustion chamber 5M, As the theoretical air-fuel ratio combustion amount of the quadruple fuel of the existing technology, the superheated steam 50 of 200 MPa or the like with an increased heat amount is injected from the production superheated steam injection nozzle 6A, and the high pressure and high temperature combustion aiming at the quadruple combustion amount or 40 times combustion by the rocket injection As a simple gas engine 88d that sucks and injects the chamber 5M and approaches the existing micro gas turbine, the generator 1 is driven to drive the storage battery driving wheel 4J to the storage battery 1A. A simple gas locomotive 7d that is used even with liquid oxygen 0 is used.

The simple gas engine ship 7e of FIG. 9 is an improved invention of an existing gas turbine ship. The simple gas engine 88d is driven by compressed air and fuel power is generated by an electric product. Cost 0 Power generation Extremely cheap electricity production, electricity + liquid air cold heat + high temperature water to superheated steam temperature heat supply equipment 3D receives liquid oxygen + electricity + high temperature water to the theoretical combustion chamber 4Q etc. driven by cheap electricity products By compressing liquid oxygen, the compression volume work rate is set to 21/60000 volume compression work rate of air compression, and liquid oxygen + liquid fuel + high temperature water is compressed and heated to an ultra-high pressure such as 24-200 MPa. In the rocket combustion theoretical combustion chamber 4Q in which the on-off valve 1Q is closed, oxygen + fuel injection is heated to an optimum temperature from the oxygen injection nozzle 6L + fuel injection nozzle 6X, and fuel + oxygen is heated on the inner wall of the theoretical combustion chamber 4Q. The superheated steam 50 is heated to the optimum temperature and the theoretical air-fuel ratio combustion is performed, and the existing technology improved theoretical combustion chamber 4Q is aimed at 10 times the pressure of the high pressure high temperature combustion chamber 5M. As the theoretical air-fuel ratio combustion amount of double fuel, superheated steam 50 with an increased heat quantity of 200 MPa or the like is injected from the manufactured superheated steam injection nozzle 6A, and the high pressure and high temperature combustion chamber 5M is sucked by rocket injection aiming at 4 times combustion amount or 40 times combustion. As a simple gas engine ship 7e that injects and comes close to an 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 88d. Liquid oxygen driven theoretical combustion chamber 4Q combined with a plurality of liquid oxygen driven theoretical combustion chambers that saves fuel oxygen by reducing friction loss drastically by rocket combustion And simple gas engine vessels 7e to use any element 0.

The simple gas engine airplane 7f of FIG. 10 is an improved invention of the existing jet aircraft. The simple gas engine 88d is driven by compressed air + fuel cost 0 power generation electric product drive. 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, and liquid oxygen + liquid fuel + high temperature water is compressed and heated to ultrahigh pressure such as 24 to 200 MPa, and a multiple inlet on-off valve 1Q is closed in the rocket combustion theoretical combustion chamber 4Q, oxygen + fuel injection combustion heated to the optimum temperature from the oxygen injection nozzle 6L + fuel injection nozzle 6X, fuel + oxygen + on the inner wall of the theoretical combustion chamber 4Q The thermal steam 50 is heated to the optimum temperature and heated to the theoretical air-fuel ratio combustion, aiming at 10 times the pressure 10 times the combustion amount of the existing high quality combustion chamber 4M of the existing technology improved high pressure combustion chamber 5M. As a theoretical air-fuel ratio combustion amount of double fuel, superheated steam 50 with an increased heat amount of 200 MPa or the like is injected from the manufactured superheated steam injection nozzle 6A, and a high pressure and high temperature combustion chamber aiming at four times combustion amount or 40 times combustion by exhaust injection or rocket injection. As a simple gas engine airplane 7f that sucks and injects 5M and comes close to an existing jet aircraft, propeller 7A driving exhaust is injected backward by the rotational output of the simple gas engine 88d, and rocket combustion + jet combustion capable of 10 times output or the like is achieved. The liquid oxygen driven theoretical combustion chamber 4Q is a simple gas engine airplane 7f that flies even with a space flight aim or liquid oxygen 0 as a combination of a plurality of combustion chambers 4Q.

The simple water injection engine ship 7G in FIG. 11 is an improved invention of an existing gas turbine ship. The simple injection engine 88e is driven by compressed air drive + zero fuel cost power generation electric product drive. Fuel cost 0 power generation Electricity + liquid air cold heat + high temperature water to superheated steam temperature heat supply equipment 3D, which is extremely inexpensive electricity production, receives liquid oxygen + electricity + high temperature water to the theoretical combustion chamber 4Q, etc. driven by low cost electric products By compressing liquid oxygen, the compression volume work rate is made to be 21/60000 volume compression work rate of air compression, and liquid oxygen + liquid fuel + high temperature water is compressed and heated to an ultrahigh pressure such as 24-200 MPa, and a plurality of inlets In the rocket combustion theoretical combustion chamber 4Q with the outlet on-off valve 1Q closed, oxygen + fuel injection heated to the optimum temperature from the oxygen injection nozzle 6L + fuel injection nozzle 6X is combusted and burned on the inner wall of the theoretical combustion chamber 4Q + Oxygen + Superheated steam 50 is heated to the optimum temperature, and the theoretical air-fuel ratio combustion is performed, and the existing technology improved theoretical combustion chamber 4Q high pressure high temperature combustion chamber 5M is aimed at 10 times the pressure 10 times combustion amount, superheated steam injection around the theoretical combustion chamber 4Q The superheated steam 50 and the high-pressure high-temperature combustion chamber 5M approaching 200 MPa are injected from the nozzle 6A + combustion gas injection nozzle 6Y. 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 and injected. Then, 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 theoretical combustion chamber 4Q, the theoretical air-fuel ratio combustion amount of the fuel four times that of the existing technology is overheated by 200 MPa with an increased heat amount. Steam 50 is produced in the high-pressure and high-temperature combustion chamber 5M. As a simple water injection engine 88e driven near the existing jet engine by sucking and injecting air 28a, the plane speed is obtained by combining a plurality of liquid oxygen driven theoretical combustion chambers 4Q, and even when liquid oxygen is 0, it moves at high speed. It is assumed that the simple water injection engine ship 7G.

The simple injection engine airplane 7h in FIG. 12 is an improved invention of the existing jet aircraft. The simple injection engine 88e is driven by compressed air + fuel cost 0 power generation electric product drive. 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 made to be 21/60000 volume compression work rate of air compression, and liquid oxygen + liquid fuel + high temperature water is compressed and heated to ultrahigh pressure such as 24 to 200 MPa to open and close multiple inlets and outlets In the rocket combustion theoretical combustion chamber 4Q with the valve 1Q closed, oxygen + fuel injection heated to an optimum temperature from the oxygen injection nozzle 6L + fuel injection nozzle 6X is combusted, and fuel + acid is generated on the inner wall of the theoretical combustion chamber 4Q. + The superheated steam 50 is heated to the optimum temperature and the theoretical air-fuel ratio combustion is performed, and the existing technology improved theoretical combustion chamber 4Q high pressure and high temperature combustion chamber 5M is aimed at 10 times the pressure 10 times the combustion amount, and the superheated steam injection nozzle 6A + on the outer periphery of the theoretical combustion chamber 4Q + From the combustion gas injection nozzle 6Y, superheated steam 50 or a high-pressure high-temperature combustion chamber 5M approaching 200 MPa is 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, the front air 28a is supplied. The plurality of theoretical combustion chambers 4Q are made into liquid oxygen driven rocket combustion chambers and jet combustion chambers by suction injection, and in the existing technology improved theoretical combustion chamber 4Q, the theoretical air-fuel ratio combustion amount of the fuel four times that of the existing technology is increased by 200 MPa with an increased heat amount. The target superheated steam 50 is rotated and generated in the high-pressure and high-temperature combustion chamber 5M, and the superheated steam 50 is injected from the superheated steam injection nozzle 6A of the suction flow of the outer air 28a. As a simple injection engine 88f driven near the existing jet engine by sucking and injecting the air 28a ahead, the liquid oxygen-driven theoretical combustion chamber 4Q is combined with a plurality of the space arrival costs, aiming at 1 / 500,000 of the existing technology, and liquid in the atmosphere A simple injection engine airplane 7h is used in which high-speed flight is performed with oxygen 0 and the propeller 7A is driven by extending the inner shaft device 60A depending on the application.

The rotary wing airplane 7i of FIG. 14 is an improved invention of the existing rotary wing aircraft. The simple gas engine 88d is driven by compressed air + fuel cost 0 power generation electric product drive. Horizontal full blade ratio critical 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 set to 21/60000 volume compression work rate of air compression, and liquid oxygen + liquid fuel + high temperature water is compressed and heated to ultrahigh pressure such as 24-200 MPa, and multiple inlets are opened and closed. In the rocket combustion theoretical combustion chamber 4Q with the valve 1Q closed, oxygen + fuel injection combustion heated to an optimum temperature from the oxygen injection nozzle 6L + fuel injection nozzle 6X and fuel + oxygen + superheated steam on the inner wall of the theoretical combustion chamber 4Q Heating the air to the optimal temperature with the theoretical air-fuel ratio combustion at 0, aiming at 10 times the pressure 10 times that of the compressed air combustion theoretical combustion chamber 4Q high pressure high temperature combustion chamber 5M, the heat exchange cooling air existing technology in the compressed air combustion theoretical combustion chamber 4Q As the theoretical air-fuel ratio combustion of 4 times fuel combustion, superheated steam 50 of 200 MPa or the like is manufactured with an increased heat amount of 3 times, injected from the superheated steam injection nozzle 6A, and exhausted or rocket injected by 4 times the combustion amount or 40 times. High-pressure high-temperature combustion chamber 5M injection aimed at combustion, as a rotary wing airplane 7j approaching an existing rotary wing aircraft, the rotational output of the simple gas engine 88d is set to rotational force + injection propulsion by the rotary blade 7B driven exhaust injection, and the outer shaft device 60B Is driven by the inner shaft device 60A extended rotor blade 7B, rocket combustion capable of 10 times output etc. + jet combustion + rotation output + injection propulsion output, compressed air + liquid oxygen drive theoretical fuel Rooms 4Q as a plurality of coalescing, and rotary-wing aircraft 7i to fly even space flight aim and liquid oxygen 0.

A rotary blade injection airplane 7j in FIG. 15 is an improved invention simple injection engine 88e of an existing rotary blade aircraft in which compressed air drive + fuel cost 0 power generation electric product drive is used. Cost 0 Power generation Extremely cheap electricity production, electricity + liquid air cold heat + high temperature water to superheated steam temperature heat supply equipment 3D receives liquid oxygen + electricity + high temperature water to the theoretical combustion chamber 4Q etc. driven by cheap electricity products By compressing liquid oxygen, the compression volume work rate is made to be 21/60000 volume compression work rate of air compression, and liquid oxygen + liquid fuel + high temperature water is compressed and heated to ultrahigh pressure such as 24 to 200 MPa, multiple inlets and outlets In the rocket combustion theoretical combustion chamber 4Q with the open / close valve 1Q closed, oxygen + fuel injection heated to an optimum temperature from the oxygen injection nozzle 6L + fuel injection nozzle 6X, and fuel + oxygen + on the inner wall of the theoretical combustion chamber 4Q The heating steam 50 is heated to the optimum temperature and the theoretical air-fuel ratio combustion is performed. The combustion chamber 4Q for high pressure and high temperature combustion chamber 5M for compressed air combustion is aimed at 10 times the pressure 10 times the combustion amount. From the combustion gas injection nozzle 6Y, superheated steam 50 approaching 200MPa or high-pressure high-temperature combustion chamber 5M is injected, and when the on-off valve 1Q is closed, the high power rocket combustion space utilization prime is used. Injected by air-fuel ratio combustion, etc., multiple theoretical combustion chambers 4Q are used as liquid oxygen-driven rocket combustion chambers and jet combustion chambers, and compressed air combustion theoretical combustion chamber 4Q is increased as the theoretical air-fuel ratio combustion of four times the fuel of the existing technology The superheated steam 50 is produced with a triple heat quantity and targeted at 200 MPa, and the high pressure and high temperature combustion chamber 5M combustion gas injection generates rotational output and the superheated steam injection nozzle with the suction flow of the outer air 28a. The superheated steam 50 is injected from A, the air 28a in front is sucked and injected, and as a simple injection engine 88f driven close to the existing jet engine, the liquid oxygen drive theoretical combustion chamber 4Q is combined with a plurality of space arrival costs 1 of the existing technology. Suppose that the target is / 500,000, flying with 0 liquid oxygen in the atmosphere, or driving the outer shaft device 60B or the inner shaft device 60A with the extension rotor blade 7B to obtain a rotary blade injection airplane 7j with rotational output + injection propulsion output drive.

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 For example, a combined driving car, ship, airplane, etc., liquid oxygen 5K is liquid compressed to a volumetric compression work rate of 21/60000, and a simple gas engine 88d, a simple water injection engine 88e, and a simple injection engine. Driving 88f, there is a possibility that the CO2 exhaust and fuel cost will be close to 1/10 in the car, the ship may be close to 10 times the speed with the same fuel cost, and the plane will have a space cost of 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, 3s: Simple compressor, 3t: Simple multistage 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 + heat production by gravity power generation electricity and supplying liquid oxygen and liquid nitrogen Drive airplane or supply with superheated steam Inject methane into methane hydrate, collect methane, etc. Electricity + cold heat + make full use of heat) 3E: Specific critical substances (specific critical liquid substances such as mercury and water at room temperature) 3E: Ratio Large material (low-melting-point alloy 500 ° C liquid and stable high-temperature liquid alloy) 3F: oxygen pressure reciprocating engine 3G: theoretical combustion gear engine, 3H: reciprocating piston, 3J: theoretical combustion reciprocating engine, 3K: external gear, 3L: multiple Stage combustion chamber 3M: Steam pressure reciprocating engine, 3N: Steam pressure gear engine, 3P: Theoretical expansion engine (the gas volume is inversely proportional to the pressure, aiming at the best engine + oxygen-hydrogen increase combustion) 3Q: Theoretical expansion engine (Boil's 3R: Theoretical gas turbine (theoretical best gas turbine with gas volume inversely proportional to pressure) 3S: Theoretical steam turbine (theoretical best with gas volume inversely proportional to pressure) 3T: Theoretical gas compressor (Theoretical best gas compressor whose gas volume is inversely proportional to the pressure) 3U: Theoretical turbine, 3V: Pump engine (existing) 3X: Compressor engine (uses various existing compressors in the engine) 3Y: Counter-rotating engine (engine whose gas volume is inversely proportional to pressure) 3Z: Oxygen pressure gear engine, 3a: repellent Water plating, 3b: water repellent coating, 4C: counter-synchronous gear, 4D: in-line co-rotating gear, 4F: combustion gas reciprocating engine, 4H: heat absorption tube (long-lens 2d collects sunlight into heat absorption tube in a straight line 4J: Battery drive wheel, 4K: Theoretical expansion engine vehicle, 4Q: Theoretical combustion chamber (superheated steam production, theoretical air-fuel ratio combustion, existing fourfold combustion) 4W: Theoretical compression chamber, 4Y: Theoretical combustion chamber (combustion chamber for high-temperature pyrolysis, electrolysis combustion, and target for compound 0) 4Z: Combustion gas gear machine 4X: Turbine blade cross section (enlarged surface area) 4a: Liquid fuel pump, 4b: Liquid oxygen pump, 4c: Water pump, 4d: Gear device, 4e: Roller, 4f: Rotating support, 5: Air Injection nozzle, 5a: high-pressure and high-temperature combustion gas control valve, 5b: compression 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 pipe, 5G: Steam heating pipe, 5G: High pressure high temperature water heating pipe, 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 steam chamber, 5N: High pressure high temperature steam, 5P : Steam system Valve, 5Q: Water control valve, 5R: Superheated steam control valve, 5S: Compressed air heating pipe, 5T: Liquid oxygen control valve, 6: Final compression blade, 6A: Superheated steam rocket nozzle, 6B: Compressed air injection nozzle, 6E : Specific critical substance injection nozzle, 6F: Water injection nozzle, 6G: Stator blade, 6H: Drain pipe, 6L: Oxygen injection nozzle, 6W: Specific critical substance accelerator (specific gravity using liquid specific critical substance 3E pressure and specific gravity difference) 6X: fuel injection nozzle, 6X: afterburner (combustion with the intake air flow and the fuel injection cold heat 28a combustion flow 6Y, and the combustion rises with a large increase in the amount of fuel combustion) 6Y: combustion gas injection nozzle ( 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 airplane, 7g: Simple water injection engine ship, 7h: Easy Injection engine airplane, 7i: Rotary wing airplane, 7j: Rotary wing airplane, 8c: Turbine wing (a straight long turbine blade is provided on the outer surface of the cylinder for full automatic machining and weight reduction on 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 group, 8m: Outer compression blade Blades, 8n: Inner output blades, 8p: Outer output blades, 8A: Cylindrical turbine blade group (enables fully automatic machining and precision assembly as a horizontal cylindrical turbine blade group) 8S: Horizontal full blade turbine (opposite full blade impeller) T Bin-series full blade impeller turbine biting full bucket impeller turbine) 8S: Horizontal full blade turbine (with straight long turbine blades on the outer surface of the cylinder for full automatic machining and weight reduction on the inner and outer circumferences) 8S: Horizontal All-blade hydrogravity turbines (existing steam turbines are stationary blades and the damming output approaches 0, so all blades are essential, and the work rate is as small as 1 / 36,000 of platinum spheres, so the vacuum level of critical substances increases. 8M: Vertical type moving blade water gravity turbine (6 types of cylindrical turbine moving blade group fitting assembly + close to magnetic bearing load 0) 8N: Critical type of vertical moving blade Mass Gravity Turbine (6 types of cylindrical turbine blade group fitting assembly + magnetic utilization bearing load approach 0) 8R: Horizontal all blade hydrogravity turbine (cylindrical turbine blade group series opposed synchronous rotation + magnetic utilization bearing load approach 0) 8S: Horizontal all blades Severe material gravity turbine (cylindrical turbine blade group in series opposed synchronous rotation + close to magnetic bearing load 0) 8P: vertical-type full blade hydrogravity turbine (6 types of cylindrical turbine blade group fitting assembly + magnetic bearing load) 8Q: Vertical type moving blade ratio critical material gravity turbine (6 types of cylindrical turbine blade group fitting assembly + magnetic bearing load 0 approach + ultra high speed peripheral speed) 8T : Horizontal type full-blade water gravity turbine (cylindrical turbine blade group serially opposed synchronous rotation + magnetic utilization bearing load approach 0 + super high speed peripheral speed) 8U: Horizontal type full blade specific gravity gravity turbine (cylindrical turbine blade group series opposed) Synchronous rotation + Magnetic bearing load approach 0 + Super high speed outer peripheral speed) 9: Wear-resistant annular assembly (fitting assembly method to reduce the weight of specific critical material flow path including 8c with cemented carbide annularly) 9A: Cylinder Annular assembly (Abrasion-resistant cylindrical annular assembly blade group is made into 6 types to make the structure simple, the number of parts is small, fully automatic processing is easy, assembly is easy, and weight reduction is easy.) 9A: Cylindrical annular assembly (fixed inlet outer blade 60E + outer annular) The cylindrical outer blade group 60D is configured by fitting the blade 60G + the outlet fixed outer blade 60J, and the cylindrical portion configuring the cylindrical inner blade group 60C by fitting the inlet fixed inner blade 60F + the inner annular blade 60H + the outlet fixed inner blade 60K) 9B : Repulsive permanent magnet, 9C: Suction permanent magnet, 9D: Compressed air part, 9E: Vacuum part, 9M: Fitting assembly part, 9Q: Vertical parallel plate (vertical parallel plate for guiding the blast air to the storage stern) 10: Hull, 10A: cabin, 10b: cockpit, 10c: control room, 10d: cabin, 10e: cargo compartment, 16: horizontal shaft plate (disk for easy precision assembly) 16A: horizontal shaft, 11D: cooling chamber dedicated to gas , 21: Thick Light heater (suction air passage is also provided in the heat absorption pipe 4H for main use) 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 (compressed air 28a is compressed by a heat pump, and is divided and stored into 50 heated hot air of compressed air heat + compressed air 28a cold containing liquid oxygen and liquid nitrogen) 28b: compressed air heat, 28A: Intake air passage, 28B: Air passage inlet, 38: Rotation guide, 38a: Flight trunk, 38b: Flight wing, 38c: Flight wing, 38d: Vertical wing, 38e: Wing leading edge, 38g: Water wing, 38h: Ascending boat, 38B: Air suction jet ship (with 79S79T79Y79Z) 38C: Water suction jet ship (with 79U79X) 38H: Theoretical screw ship, 38J: Theoretical jet ship, 8T: 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, 39H: Oxygen combined 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 wing 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: Superheated steam chamber, 50: Superheated steam chamber 50: Heat (air 28 a is compressed with a heat pump and divided into superheated steam 50 warm heat of compressed air calorie + compressed air 28a cold) 50A: water vapor, 50a: superheated steam injection pipe, 51: air extractor, 51: confluence extractor (join) 51A: Air extraction chamber, 52a: Hot water 52a: Deep sea water, 52b: Hot water, 52d: Hot water (change from 50) 52e: Cold heat (change from 28a) 55B: Transmission, 60A: Inside Shaft device (equipment with turbine blades) 60B: Outer shaft device (equipment with turbine blades) 60C: Cylindrical inner rotor blade group (Wear resistant cylindrical annular assembly fixed rotor blade group including fully automatic machining easy assembly) 60D: Cylindrical outer blade group (Wear resistant cylindrical annular assembly fixed blade group including fully automatic machining easy assembly) 60E: Inlet fixed outer blade (inlet blade for annular assembly fixing outer blade group) 60F: On Mouth-fixed inner blade (inlet blade for annular assembly fixing inner rotor blade group) 60G: outer annular blade (intermediate blade for annular assembly of outer rotor blade group) 60H: inner annular blade (intermediate blade for annular assembly of inner rotor blade group) 60J: Outlet fixed outer wing (exit wing for annular assembly fixing outer rotor blade group) 60K: Outlet fixed inner wing (exit wing for annular assembly fixing inner rotor blade group) 76: Gear device (magnetic friction power transmission device) 77B: Rocket outer box, 77C: Counter reversing machine outer box, 77F: Injection part outer box, 77G: Cylindrical rotating part, 77a: Turbine outer box, 77b: Compressor outer box, 80: Bearing (magnetic 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 to 5M Multiple fuel injection combustion Then, 5N is heated and injected several times from the inner and outer peripheries, and air is sucked and jetted to suck and jet water) 80Z: Liquid air suction water jet (high pressure high temperature combustion chamber 5M receiving high pressure high temperature steam chamber 5N) Then, 5N is injected and burned multiple times to 5M, and 5N is heated and injected multiple times from the inner and outer peripheries. 84: Counter-rotating magnetic friction device (a device that rotates the inner rotor blade group and the outer rotor blade group having a fixed portion at substantially the same speed and opposite rotation) 84Y: Counter-rotating gear device (same in existing technology) 85: Counter-rotating magnetic device (magnet-utilized gear height is slightly to non-contact and rotating mutually reversely with the horizontal shaft 1h gear) 85Y: Counter-rotating gear device (mutually rotating reversely with the existing horizontal shaft 1h gear) 88a : Simple gas engine, 88b: Simple injector Seki, 88c: simple water injection engine, 88d: simple gas engine, 88f: simple injection engine, 88e: simple water injection engine, 88g: liquid oxygen production machine, 88A: oxygen combined air injection unit (rocket combustion + jet combustion + steam) 88B: oxygen combined air injection unit (super high pressure rocket combustion + jet combustion + superheated steam injection suction) 88C: theoretical air injection unit, 88M: theoretical water injection unit, 88K: oxygen combined water injection unit (rocket Combustion + jet combustion + combined injection with steam injection, etc.) 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 energy recovery device,

Claims (417)

  A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, and a series rotation gear (4D) between the horizontal axes (16A), and a pair of vertical rotations in the same direction at the same speed rotation. + Various types of energy conservation cycles that combine the drive of a 1-20 set of gravity turbines (8U) with a horizontal all-blade ratio with a super-high-speed circumferential speed, and the drive of a double-sided center-supporting counter-rotating compressed air (28a). Merger engine and merger method.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, and a series rotation gear (4D) between the horizontal axes (16A), and a pair of vertical rotations in the same direction at the same speed rotation. + Horizontal type full blade ratio critical material gravity turbine (8U) 21-40 sets of power generation electrical product drive with ultra-high speed circumferential speed + Various energy conservation cycles to combine double-side center support counter-rotating compressed air (28a) drive Merger engine and merger method.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, and a series rotation gear (4D) between the horizontal axes (16A), and a pair of vertical rotations in the same direction at the same speed rotation. + Horizontal type full blade ratio critical material gravity turbine (8U) 41-60 sets generating electric product drive with super high speed circumferential speed + Various energy storage cycles to combine both sides center support counter-rotating compressed air (28a) drive Merger engine and merger method.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, and a series rotation gear (4D) between the horizontal axes (16A), and a pair of vertical rotations in the same direction at the same speed rotation. + Horizontal type full blade ratio material gravity turbine (8U) 61-80 sets of power generation electrical product drive with ultra-high speed circumferential speed + Various energy conservation cycles to combine double-side center support counter-rotating compressed air (28a) drive Merger engine and merger method.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, and a series rotation gear (4D) between the horizontal axes (16A), and a pair of vertical rotations in the same direction at the same speed rotation. + Horizontal type full blade ratio material gravity turbine (8U) 81-100 sets of power generation electrical product drive with ultra-high speed circumferential speed + Various energy conservation cycles to combine double-side center support counter-rotating compressed air (28a) drive Merger engine and merger method.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, and a series rotation gear (4D) between the horizontal axes (16A), and a pair of vertical rotations in the same direction at the same speed rotation. + Horizontal type full-blade ratio critical material gravity turbine (8U) 101-120 sets of power generation electric product drive with ultra-high speed circumferential speed + Various energy conservation cycles to combine both-side center support counter-rotating compressed air (28a) drive Merger engine and merger method.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, and a series rotation gear (4D) between the horizontal axes (16A), and a pair of vertical rotations in the same direction at the same speed rotation. + Horizontal type full-blade ratio critical material gravity turbine (8U) 121 to 140 sets driven by ultra-high speed circumferential speed 121-140 generator power generation electric product drive + various energy storage cycles to combine both-side center support counter-rotating compressed air (28a) drive Merger engine and merger method.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, and a series rotation gear (4D) between the horizontal axes (16A), and a pair of vertical rotations in the same direction at the same speed rotation. + Horizontal type full-blade ratio critical material gravity turbine (8U) 141-160 sets driven by ultra-high speed circumferential speed 141-160 power generation electric product drive + Double-side center support counter rotating compressed air (28a) drive combined with various energy storage cycles Merger engine and merger method.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, and a series rotation gear (4D) between the horizontal axes (16A), and a pair of vertical rotations in the same direction at the same speed rotation. + Horizontal type full blade ratio material gravity turbine (8U) 161-180 sets driven by super high speed circumferential speed 161-180 sets of power generation electric product drive + various energy conservation cycles to combine both sides center support counter-rotating compressed air (28a) drive Merger engine and merger method.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, and a series rotation gear (4D) between the horizontal axes (16A), and a pair of vertical rotations in the same direction at the same speed rotation. + Horizontal type full-blade ratio critical material gravity turbine (8U) 181 to 200 sets of power generation electrical product drive with ultra-high speed circumferential speed + Various energy storage cycles to combine double-side center support counter-rotating compressed air (28a) drive Merger engine and merger method.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Magnetically driven bearing load driven by Mach 1 to 30: Horizontal load blade ratio critical material gravity turbine (8U) 1-20 sets driven with super high speed circumferential speed + both sides center support double reversal Various energy storage cycle coalescence engines and coalescence methods for coalescence of compressed air (28a) drive.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Mach 1 to 30 injection drive using magnetic bearing load 0 approach + horizontal high-speed blade ratio critical material gravity turbine (8U) 21-40 sets driven by super high speed circumferential speed + both sides center support double reversal Various energy storage cycle coalescence engines and coalescence methods for coalescence of compressed air (28a) drive.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Mach 1-30 injection driven magnetic bearing load approaching zero + super high speed circumferential blade ratio critical material gravity turbine (8U) 41-60 sets power generation electric product drive + both sides center support double reversal Various energy storage cycle coalescence engines and coalescence methods for coalescence of compressed air (28a) drive.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Mach 1-30 injection driven magnetic bearing load approaching 0 + super high speed circumferential blade speed critical material gravity turbine (8U) 61-80 sets power generation electric product drive + both sides center support double reversal Various energy storage cycle coalescence engines and coalescence methods for coalescence of compressed air (28a) drive.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Mach 1 to 30 injection driven magnetic bearing load approaching 0 + ultra-high speed circumferential speed with full blade ratio critical material gravity turbine (8U) 81 to 100 power generation electric product drive + double center support double reversal Various energy storage cycle coalescence engines and coalescence methods for coalescence of compressed air (28a) drive.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Mach 1-30 injection driven magnetic bearing load approaching 0 + ultra-high speed circumferential speed blade ratio critical material gravity turbine (8U) 101-120 set power generation electric product drive + double-side center support double reversal Various energy storage cycle coalescence engines and coalescence methods for coalescence of compressed air (28a) drive.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Mach 1 to 30 injection drive using magnetic bearing load approaching zero + super high speed circumferential speed blade-weighted critical material gravity turbine (8U) 121-140 set generator electric product drive + double center support double reversal Various energy storage cycle coalescence engines and coalescence methods for coalescence of compressed air (28a) drive.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Mach 1-30 injection driven magnetic bearing load approaching 0 + ultra-high speed peripheral blade ratio critical material gravity turbine (8U) 141-160 set power generation electric product drive + double-side center support double reversal Various energy storage cycle coalescence engines and coalescence methods for coalescence of compressed air (28a) drive.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Mach 1 to 30 injection driven magnetic bearing load approaching 0 + ultra-high speed circumferential speed with full blade ratio critical material gravity turbine (8U) 161-180 set generator electric product drive + double center support double reversal Various energy storage cycle coalescence engines and coalescence methods for coalescence of compressed air (28a) drive.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Mach 1 to 30 injection driven magnetic bearing load approaching 0 + ultra-high speed circumferential blade speed critical material gravity turbine (8U) 181 to 200 sets of power generation electrical product drive + double center support double reversal Various energy storage cycle coalescence engines and coalescence methods for coalescence of compressed air (28a) drive.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Aiming at Mach 30 injection ratio critical substance (2E) mixed injection acceleration drive using magnetic bearing load 0 approach + horizontal all blade ratio critical substance gravity turbine (8U) 1-20 sets of generator electric production with super high speed circumferential speed Various energy storage cycle coalescing engines and coalescence methods for coalescence of object driving + both center support counter-rotating compressed air (28a) driving.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Aiming at Mach 30 with the injection ratio critical material (2E) driven by mixed injection acceleration using a magnetic bearing load of 0 approach + super high speed peripheral speed gravity material gravity turbine (8U) 21-40 sets Various energy storage cycle coalescing engines and coalescence methods for coalescence of object driving + both center support counter-rotating compressed air (28a) driving.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Horizontally-moving blade ratio critical material gravity turbine (8U) 41-60 sets of electric generators with a magnetic bearing load approaching 0 and super-high speed circumferential speed with mixed injection acceleration driving aiming at Mach 30 Various energy storage cycle coalescing engines and coalescence methods for coalescence of object driving + both center support counter-rotating compressed air (28a) driving.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Horizontally-moving blade ratio critical material gravity turbine (8U) 61-80 sets of electric generators with a magnetic bearing load approaching 0 and super-high speed circumferential speed with mixed injection acceleration drive aiming at Mach 30 Various energy storage cycle coalescing engines and coalescence methods for coalescence of object driving + both center support counter-rotating compressed air (28a) driving.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Horizontally-moving blade ratio critical material gravity turbine (8U) 81 to 100 sets of electric generators with a magnetic bearing load approaching 0 and super-high speed circumferential speed with mixed injection acceleration driving aiming at Mach 30 Various energy storage cycle coalescing engines and coalescence methods for coalescence of object driving + both center support counter-rotating compressed air (28a) driving.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Horizontally-moving blade ratio critical material gravity turbine (8U) 101-120 generator generator set with magnetic bearing load approaching 0 and super-high speed circumferential speed with mixed injection acceleration driving aiming at Mach 30 Various energy storage cycle coalescing engines and coalescence methods for coalescence of object driving + both center support counter-rotating compressed air (28a) driving.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Horizontally-moving blade ratio critical material gravity turbine (8U) 121-140 generators set to Mach 30 aiming at injection ratio critical material (2E) with mixed injection acceleration drive using magnetic bearing load 0 approach + super high speed circumferential speed Various energy storage cycle coalescing engines and coalescence methods for coalescence of object driving + both center support counter-rotating compressed air (28a) driving.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Horizontally-moving blade ratio critical material gravity turbine (8U) 141-160 generator generator set with magnetic load bearing approaching 0 + super-high speed circumferential speed with mixed injection acceleration driving aiming at Mach 30 Various energy storage cycle merging engines and merging methods for merging of object driving + both center support counter-rotating compressed air (28a) driving.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Horizontally-moving blade ratio critical material gravity turbine (8U) 161-180 sets of electric generators with a magnetic bearing load approaching 0 and super-high-speed circumferential speed for mixed injection acceleration drive of Mach 30 aiming injection injection critical material (2E) Various energy storage cycle merging engines and merging methods for merging of object driving + both center support counter-rotating compressed air (28a) driving.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Horizontally-moving blade ratio critical material gravity turbine (8U) 181 to 200 sets of electric generators with a magnetic bearing load approaching 0 and super-high speed circumferential speed with mixed injection acceleration drive aiming at Mach 30 Various energy storage cycle coalescing engines and coalescence methods for coalescence of object driving + both center support counter rotating compressed air (28a) driving   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal shafts (16A), and a set of each set rotating in the same vertical direction and at the same speed, allowing the entire inner diameter to be cut. Horizontal magnetic blade ratio critical material gravity turbine (8U) 1-20 sets driving electric product drive + double-side center support counter-rotating compressed air (28a) drive Various energy conservation cycle coalescence engines and coalescence methods for coalescence.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal shafts (16A), and a set of each set rotating in the same vertical direction and at the same speed, allowing the entire inner diameter to be cut. Horizontal magnetic blade ratio critical material gravity turbine (8U) 21 to 40 sets driven electric power product drive + both sides center support counter rotating compressed air (28a) drive Various energy conservation cycle coalescence engines and coalescence methods for coalescence.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal shafts (16A), and a set of each set rotating in the same vertical direction and at the same speed, allowing the entire inner diameter to be cut. Horizontal magnetic blade ratio critical material gravity turbine (8U) 41-60 sets generating electric product drive + both sides center support counter rotating compressed air (28a) drive Various energy conservation cycle coalescence engines and coalescence methods for coalescence.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal shafts (16A), and a set of each set rotating in the same vertical direction and at the same speed, allowing the entire inner diameter to be cut. Horizontal magnetic blade ratio critical material gravity turbine (8U) 61-80 sets generating electric product drive + both sides center support counter-rotating compressed air (28a) drive Various energy conservation cycle coalescence engines and coalescence methods for coalescence.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal shafts (16A), and a set of each set rotating in the same vertical direction and at the same speed, allowing the entire inner diameter to be cut Horizontal magnetic blade ratio critical material gravity turbine (8U) 81-100 sets generating electric product drive + double-side center support counter-rotating compressed air (28a) drive Various energy conservation cycle coalescence engines and coalescence methods for coalescence.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal shafts (16A), and a set of each set rotating in the same vertical direction and at the same speed, allowing the entire inner diameter to be cut. Horizontal magnetic blade ratio critical material gravity turbine (8U) 101 to 120 sets driven by a magnetic bearing with a diameter of 0 approach + super high speed circumferential speed drive + double-side center support counter-rotating compressed air (28a) drive Various energy conservation cycle coalescence engines and coalescence methods for coalescence.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal shafts (16A), and a set of each set rotating in the same vertical direction and at the same speed, allowing the entire inner diameter to be cut. Horizontal type full-blade ratio critical material gravity turbine (8U) 121-140 sets driven by a radial magnetic bearing load 0 approach + super high speed circumferential speed drive + double-side center support counter rotating compressed air (28a) drive Various energy conservation cycle coalescence engines and coalescence methods for coalescence.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal shafts (16A), and a set of each set rotating in the same vertical direction and at the same speed, allowing the entire inner diameter to be cut. Horizontal magnetic blade ratio critical material gravity turbine (8U) 141-160 sets driven by radial magnetic bearing load 0 approach + ultra high speed circumferential speed + both sides center support counter rotating compressed air (28a) drive Various energy conservation cycle coalescence engines and coalescence methods for coalescence.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal shafts (16A), and a set of each set rotating in the same vertical direction and at the same speed, allowing the entire inner diameter to be cut. Horizontal magnetic blade ratio critical material gravity turbine (8U) 161-180 sets driven by a magnetic bearing with a diameter of 0 approach + super high speed circumferential speed drive + double-side center support counter-rotating compressed air (28a) drive Various energy conservation cycle coalescence engines and coalescence methods for coalescence.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal shafts (16A), and a set of each set rotating in the same vertical direction and at the same speed, allowing the entire inner diameter to be cut. Horizontal magnetic blade ratio critical material gravity turbine (8U) 181 to 200 sets driving electric product drive + both sides center support counter rotating compressed air (28a) drive Various energy conservation cycle coalescence engines and coalescence methods for coalescence.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) The inner diameter driven by Mach 1-30 can be cut all over the surface The maximum diameter of the magnetically utilized bearing load 0 approach + super high speed circumferential speed ratio of the critical blade gravity material gravity turbine (8U) 1-20 sets Various energy storage cycle merging engines and merging methods for merging driving + both center support counter-rotating compressed air (28a) driving.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) The inner diameter driven by Mach 1 to 30 can be cut all over the surface. Test using the maximum diameter magnetic bearing load close to 0 + ultra-high speed circumferential speed ratio of critical blade gravity material gravity turbine (8U) 21 to 40 generator electric products Various energy storage cycle merging engines and merging methods for merging driving + both center support counter-rotating compressed air (28a) driving.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) The inner diameter driven by Mach 1 to 30 can be cut all over the surface. The maximum diameter of the magnetically utilized bearing load is close to 0 + the super-high-speed circumferential speed is the critical material gravity turbine (8U) 41-60 sets Various energy storage cycle merging engines and merging methods for merging driving + both center support counter-rotating compressed air (28a) driving.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) The inner diameter of the inner diameter driven by Mach 1 to 30 can be cut. Experiment using the maximum diameter magnet bearing load approaching 0 + super high speed circumferential speed ratio of the critical blade gravity material (8U) 61 to 80 generators Various energy storage cycle merging engines and merging methods for merging driving + both center support counter-rotating compressed air (28a) driving.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) The inner diameter of the inner diameter driven by Mach 1 to 30 can be cut. Experiment using the maximum diameter magnetic bearing load close to 0 + super high speed circumferential speed specific gravity turbine (8U) 81 to 100 generator electric products Various energy storage cycle merging engines and merging methods for merging driving + both center support counter-rotating compressed air (28a) driving.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) The inner diameter driven by Mach 1 to 30 can be cut all over the surface. The maximum diameter of the magnetically utilized bearing load is close to 0 + the super-high-speed circumferential speed is the critical material gravity turbine (8U) 101-120 generator electric product. Various energy storage cycle merging engines and merging methods for merging driving + both center support counter-rotating compressed air (28a) driving.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) The inner diameter of the inner diameter driven by Mach 1 to 30 can be cut. Experiment using the maximum diameter magnet bearing load approaching 0 + super high speed circumferential speed specific material gravity turbine (8U) 121-140 generator electric product Various energy storage cycle merging engines and merging methods for merging driving + both center support counter-rotating compressed air (28a) driving.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) The inner diameter driven by Mach 1 to 30 can be cut all over the surface The maximum diameter of the magnetically utilized bearing load close to 0 + super high speed peripheral speed gravity material gravity turbine (8U) 141 to 160 sets Various energy storage cycle merging engines and merging methods for merging driving + both center support counter-rotating compressed air (28a) driving.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Inner diameter of the inner diameter driven by Mach 1 to 30 can be cut. Experiment using the maximum diameter magnetic bearing load close to 0 + super high speed circumferential speed of gravity blade critical material gravity turbine (8U) 161 to 180 sets Various energy storage cycle merging engines and merging methods for merging driving + both center support counter-rotating compressed air (28a) driving.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) The inner diameter of the inside driven by Mach 1 to 30 can be cut. The maximum diameter of the magnetically utilized bearing load is close to 0 + the super-high-speed circumferential speed is a critical material gravity turbine (8U) 181 to 200 generators. Various energy storage cycle merging engines and merging methods for merging driving + both center support counter-rotating compressed air (28a) driving.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Aiming at Mach30, injection ratio critical material (2E) is mixed and accelerated. Full internal diameter cutting is possible. Experiment using the maximum diameter magnetic bearing load approaching zero + ultra-high speed circumferential speed ratio material gravity turbine (8U) ) Various energy storage cycle coalescing engines and coalescing methods for coalescence of 1 to 20 sets of power generation electric product drive + both center support counter-rotating compressed air (28a) drive.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Aiming at Mach30, injection ratio critical material (2E) is mixed and accelerated. Full internal diameter cutting is possible. Experiment using the maximum diameter magnetic bearing load approaching zero + ultra-high speed circumferential speed ratio material gravity turbine (8U) ) Various energy storage cycle coalescence engines and coalescence methods for combining 21 to 40 sets of power generation electric product drive + both center support counter-rotating compressed air (28a) drive.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Aiming at Mach30, injection ratio critical material (2E) is mixed and accelerated. Full internal diameter cutting is possible. Experiment using the maximum diameter magnetic bearing load approaching zero + ultra-high speed circumferential speed ratio material gravity turbine (8U) ) Various energy storage cycle coalescence engines and coalescence methods for coalescence of 41-60 sets of power generation electric product drive + both side center support counter-rotating compressed air (28a) drive.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Aiming at Mach30, injection ratio critical material (2E) is mixed and accelerated. Full internal diameter cutting is possible. Experiment using the maximum diameter magnetic bearing load approaching zero + ultra-high speed circumferential speed ratio material gravity turbine (8U) ) Various energy storage cycle coalescence engines and coalescence methods for combining 61 to 80 sets of power generation electric product drive + both center support counter-rotating compressed air (28a) drive.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Aiming at Mach30, injection ratio critical material (2E) is mixed and accelerated. Full internal diameter cutting is possible. Experiment using the maximum diameter magnetic bearing load approaching zero + ultra-high speed circumferential speed ratio material gravity turbine (8U) ) Various energy storage cycle coalescing engines and coalescing methods for coalescence of 81 to 100 sets of power generation electric product driving + both center support counter-rotating compressed air (28a) driving.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Aiming at Mach 30, the injection ratio critical material (2E) is driven by mixed injection acceleration. The whole inner diameter can be cut. Experiment using the maximum diameter magnetic bearing load close to 0 + Super high speed circumferential speed with a full blade ratio critical material gravity turbine (8U) ) Various energy storage cycle coalescing engines and coalescing methods for combining 101-120 generator electric product drive + both center support counter-rotating compressed air (28a) drive.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Aiming at Mach30, injection ratio critical material (2E) is mixed and accelerated. Full internal diameter cutting is possible. Experiment using the maximum diameter magnetic bearing load approaching zero + ultra-high speed circumferential speed ratio material gravity turbine (8U) ) Various energy storage cycle merging engines and merging methods for merging 121-140 generator electric product drive + both center support counter-rotating compressed air (28a) drive.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Aiming at Mach30, injection ratio critical material (2E) is mixed and accelerated. Full internal diameter cutting is possible. Experiment using the maximum diameter magnetic bearing load approaching zero + ultra-high speed circumferential speed ratio material gravity turbine (8U) ) Various energy storage cycle merging engines and merging methods for merging 141-160 generator electric product driving + both center support counter-rotating compressed air (28a) driving.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Aiming at Mach30, injection ratio critical material (2E) is mixed and accelerated. Full internal diameter cutting is possible. Experiment using the maximum diameter magnetic bearing load approaching zero + ultra-high speed circumferential speed ratio material gravity turbine (8U) ) Various energy storage cycle merging engines and merging methods for merging 161 to 180 sets of power generation electric product driving + both center support counter-rotating compressed air (28a) driving.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Aiming at Mach30, injection ratio critical material (2E) is mixed and accelerated. Full internal diameter cutting is possible. Experiment using the maximum diameter magnetic bearing load approaching zero + ultra-high speed circumferential speed ratio material gravity turbine (8U) ) Various energy storage cycle merging engines and merging methods for merging 181 to 200 sets of power generation electric product driving + both center support counter-rotating compressed air (28a) driving.   A pair of two horizontal shafts (16A) fixed with horizontal shaft plates (16) on both sides of the cylindrical turbine blade group (8A), which is a wear-resistant super-water-repellent plating (3a), to form an opposed series full blade impeller turbine Combined use of magnetic full-scale blade ratio critical gravity gravity turbine (8U) 1-20 sets generator electric product drive + double-side center support counter-rotating compressed air (28a) drive with magnetic bearing load approaching 0 + super high speed circumferential speed Various energy storage cycle coalescence engines and coalescence methods.   A pair of two horizontal shafts (16A) fixed with horizontal shaft plates (16) on both sides of the cylindrical turbine blade group (8A), which is a wear-resistant super-water-repellent plating (3a), to form an opposed series full blade impeller turbine. Combined use of magnetized bearing load approaching zero + super high speed circumferential speed with full blade ratio critical material gravity turbine (8U) 21 to 40 generator electric product drive + both sides center support counter rotating compressed air (28a) drive Various energy storage cycle coalescence engines and coalescence methods.   A pair of two horizontal shafts (16A) fixed with horizontal shaft plates (16) on both sides of the cylindrical turbine blade group (8A), which is a wear-resistant super-water-repellent plating (3a), to form an opposed series full blade impeller turbine. Combined use of magnetically driven bearing load approaching zero + super high speed circumferential speed with full blade ratio critical material gravity turbine (8U) 41-60 sets power generation electrical product drive + both sides center support counter-rotating compressed air (28a) drive Various energy storage cycle coalescence engines and coalescence methods.   A pair of two horizontal shafts (16A) fixed with horizontal shaft plates (16) on both sides of the cylindrical turbine blade group (8A), which is a wear-resistant super-water-repellent plating (3a), to form an opposed series full blade impeller turbine. Combined use of magnetic full-scale blade ratio critical gravity gravity turbine (8U) 61-80 sets power generation electrical product drive + double-side center support counter-rotating compressed air (28a) drive with magnetic bearing load approaching 0 + super high speed circumferential speed Various energy storage cycle coalescence engines and coalescence methods.   A pair of two horizontal shafts (16A) fixed with horizontal shaft plates (16) on both sides of the cylindrical turbine blade group (8A), which is a wear-resistant super-water-repellent plating (3a), to form an opposed series full blade impeller turbine. Combined use of magnetized bearing load 0 approach + super high speed circumferential speed with full blade ratio critical material gravity turbine (8U) 81-100 power generation electric product drive + both sides center support counter-rotating compressed air (28a) drive Various energy storage cycle coalescence engines and coalescence methods.   A pair of two horizontal shafts (16A) fixed with horizontal shaft plates (16) on both sides of the cylindrical turbine blade group (8A), which is a wear-resistant super-water-repellent plating (3a), to form an opposed series full blade impeller turbine. Combined use of magnetically driven bearing load approaching 0 + super high speed circumferential speed ratio of full blade ratio critical material gravity turbine (8U) 101-120 generator power generation electric product drive + both sides center support counter-rotating compressed air (28a) drive Various energy storage cycle coalescence engines and coalescence methods.   A pair of two horizontal shafts (16A) fixed with horizontal shaft plates (16) on both sides of the cylindrical turbine blade group (8A), which is a wear-resistant super-water-repellent plating (3a), to form an opposed series full blade impeller turbine. Combined use of magnetized bearing load approaching 0 + ultra-high speed circumferential speed with full blade ratio critical material gravity turbine (8U) 121-140 set generator electric product drive + double-side center support counter-rotating compressed air (28a) drive Various energy storage cycle coalescence engines and coalescence methods.   A pair of two horizontal shafts (16A) fixed with horizontal shaft plates (16) on both sides of the cylindrical turbine blade group (8A), which is a wear-resistant super-water-repellent plating (3a), to form an opposed series full blade impeller turbine. Combined use of magnetized bearing load approaching 0 + super high speed circumferential speed with full blade ratio critical material gravity turbine (8U) 141-160 generator power generation electric product drive + both sides center support counter-rotating compressed air (28a) drive Various energy storage cycle coalescence engines and coalescence methods.   A pair of two horizontal shafts (16A) fixed with horizontal shaft plates (16) on both sides of the cylindrical turbine blade group (8A), which is a wear-resistant super-water-repellent plating (3a), to form an opposed series full blade impeller turbine. Combined use of magnetically driven bearing load approaching 0 + super high speed circumferential speed with full blade ratio critical material gravity turbine (8U) 161-180 generator drive electric product drive + both sides center support counter rotating compressed air (28a) drive Various energy storage cycle coalescence engines and coalescence methods.   A pair of two horizontal shafts (16A) fixed with horizontal shaft plates (16) on both sides of the cylindrical turbine blade group (8A), which is a wear-resistant super-water-repellent plating (3a), to form an opposed series full blade impeller turbine. Combined use of magnetically driven bearing load approaching zero + super high speed circumferential speed ratio of full blade ratio gravity material gravity turbine (8U) 181 to 200 sets of power generation electric product drive + both sides center support counter-rotating compressed air (28a) drive Various energy storage cycle coalescence engines and coalescence methods.   A magnet with a wear-resistant super-water-repellent plating (3a), a set of two horizontal shafts (16A) fixed on both sides of a cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a series full blade impeller turbine. Combined use of horizontal full-blade ratio critical material gravity turbine (8U) 1 to 20 generator electric product drive + double-side center support counter-rotating compressed air (28a) drive with zero bearing load approach + super high speed circumferential speed Various energy storage cycle coalescence engine and coalescence method.   A magnet with a wear-resistant super-water-repellent plating (3a), a set of two horizontal shafts (16A) fixed on both sides of a cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a series full blade impeller turbine. Combined use of horizontal full-blade ratio critical material gravity turbine (8U) 21 to 40 generator electric product drive + double-side center support counter-rotating compressed air (28a) drive with bearing load approaching 0 + super high speed circumferential speed Various energy storage cycle coalescence engine and coalescence method.   A magnet with a wear-resistant super-water-repellent plating (3a), a set of two horizontal shafts (16A) fixed on both sides of a cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a series full blade impeller Combined use of horizontal full-blade ratio critical material gravity turbine (8U) 41-60 power generation electric product drive + double-side center support counter-rotating compressed air (28a) drive with bearing load approaching 0 + super high speed circumferential speed Various energy storage cycle coalescence engine and coalescence method.   A magnet with a wear-resistant super-water-repellent plating (3a), a set of two horizontal shafts (16A) fixed on both sides of a cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a series full blade impeller turbine. Combined use of horizontal full-blade ratio critical material gravity turbine (8U) 61-80 power generation electrical product drive + double-side center support counter-rotating compressed air (28a) drive with bearing load approaching 0 + super high speed circumferential speed Various energy storage cycle coalescence engine and coalescence method.   A magnet with a wear-resistant super-water-repellent plating (3a), a set of two horizontal shafts (16A) fixed on both sides of a cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a series full blade impeller turbine. Combined use of horizontal full-blade ratio critical material gravity turbine (8U) 81-100 power generation electrical product drive + double-side center support counter-rotating compressed air (28a) drive with bearing load approaching 0 + super high speed circumferential speed Various energy storage cycle coalescence engine and coalescence method.   A magnet with a wear-resistant super-water-repellent plating (3a), a set of two horizontal shafts (16A) fixed on both sides of a cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a series full blade impeller turbine. Combined use of horizontal full-blade ratio critical material gravity turbine (8U) 101-120 generator electric product drive + double-side center support counter-rotating compressed air (28a) drive with bearing load approaching 0 + super high speed circumferential speed Various energy storage cycle coalescence engine and coalescence method.   A magnet with a wear-resistant super-water-repellent plating (3a), a set of two horizontal shafts (16A) fixed on both sides of a cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a series full blade impeller turbine. Combined use of horizontal full-blade ratio critical material gravity turbine (8U) 121-140 generator power generation electrical product drive + double-side center support counter-rotating compressed air (28a) drive with bearing load approaching 0 + super high speed circumferential speed Various energy storage cycle coalescence engine and coalescence method.   A magnet with a wear-resistant super-water-repellent plating (3a), a set of two horizontal shafts (16A) fixed on both sides of a cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a series full blade impeller turbine. Combined use of horizontal full-blade ratio critical material gravity turbine (8U) 141-160 generator power generation electric product drive + double-side center support counter-rotating compressed air (28a) drive with bearing load approaching 0 + super high speed circumferential speed Various energy storage cycle coalescence engine and coalescence method.   A magnet with a wear-resistant super-water-repellent plating (3a), a set of two horizontal shafts (16A) fixed on both sides of a cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a series full blade impeller turbine. Combined use of horizontal full-blade ratio critical material gravity turbine (8U) 161-180 generator power generation electrical product drive + double-side center support counter-rotating compressed air (28a) drive with bearing load approaching 0 + super high speed circumferential speed Various energy storage cycle coalescence engine and coalescence method.   A magnet with a wear-resistant super-water-repellent plating (3a), a set of two horizontal shafts (16A) fixed on both sides of a cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a series full blade impeller turbine. Combined use of horizontal full-blade ratio critical material gravity turbine (8U) 181 to 200 sets of power generation electric product drive + double side center support counter-rotating compressed air (28a) drive with bearing load approaching 0 + super high speed circumferential speed Various energy storage cycle coalescence engine and coalescence method.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), which is a wear-resistant super water-repellent plating (3a). Of a full-scale blade ratio of horizontal type blades (8U) 1 to 20 sets generating electric product drive + double-side center support counter-rotating compressed air (28a) drive Various energy storage cycle coalescence engines and coalescence methods to be coalesced.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), which is a wear-resistant super water-repellent plating (3a). Horizontally-moving blade ratio critical material gravity turbine (8U) 21 to 40 sets of power generation electric product drive + double-side center support counter-rotating compressed air (28a) drive with magnetic bearing load 0 approached + super high speed circumferential speed Various energy storage cycle coalescence engines and coalescence methods to be coalesced.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), which is a wear-resistant super water-repellent plating (3a). Horizontally-moving blade ratio critical material gravity turbine (8U) 41-60 sets driven by a magnetically utilized bearing load 0 approach + super high speed circumferential speed + both sides center support counter rotating compressed air (28a) drive Various energy storage cycle coalescence engines and coalescence methods to be coalesced.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), which is a wear-resistant super water-repellent plating (3a). Horizontally-moving blade ratio critical material gravity turbine (8U) 61 to 80 sets generating electric product drive + double-side center support counter rotating compressed air (28a) Various energy storage cycle coalescence engines and coalescence methods to be coalesced.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), which is a wear-resistant super water-repellent plating (3a). Horizontally-moving blade ratio critical material gravity turbine (8U) 81 to 100 sets of power generation electric product drive + both-side center support counter-rotating compressed air (28a) drive with magnetically utilized bearing load approaching 0 + super high speed circumferential speed Various energy storage cycle coalescence engines and coalescence methods to be coalesced.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), which is a wear-resistant super water-repellent plating (3a). Horizontally-moving blade ratio critical material gravity turbine (8U) 101 to 120 sets driven by a magnetically utilized bearing load of 0 approach + ultra high speed circumferential speed + both-side center support counter-rotating compressed air (28a) drive Various energy storage cycle coalescence engines and coalescence methods to be coalesced.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), which is a wear-resistant super water-repellent plating (3a). Horizontally-moving blade ratio critical material gravity turbine (8U) 121-140 sets driven by a magnetically utilized bearing load of 0 approach + super high speed circumferential speed + both-side center support counter-rotating compressed air (28a) drive Various energy storage cycle coalescence engines and coalescence methods to be coalesced.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), which is a wear-resistant super water-repellent plating (3a). Horizontally-moving blade ratio critical material gravity turbine (8U) 141-160 sets driven by a magnetically utilized bearing load of 0 approach + super high speed circumferential speed + both sides center support counter-rotating compressed air (28a) drive Various energy storage cycle coalescence engines and coalescence methods to be coalesced.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), which is a wear-resistant super water-repellent plating (3a). Horizontally-moving blade ratio critical material gravity turbine (8U) 161-180 sets driven by a magnetically utilized bearing load of 0 approach + super high speed peripheral speed + both-side center support counter-rotating compressed air (28a) drive Various energy storage cycle coalescence engines and coalescence methods to be coalesced.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), which is a wear-resistant super water-repellent plating (3a). Horizontally-moving blade ratio critical material gravity turbine (8U) 181 to 200 sets driven by a magnetically utilized bearing load of 0 approach + super high speed circumferential speed + both sides center support counter-rotating compressed air (28a) drive Various energy storage cycle coalescence engines and coalescence methods to be coalesced.   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, recovered heat with a high-pressure high-temperature water heating pipe (5H) for each compression, electricity + liquid air cold + hot water to superheated steam heat Various energy storage cycle coalescing engines and coalescence methods that combine feed equipment (3D) feed drive + both center support counter-rotating compressed air (28a) drive coalescence.   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 Recovering heat with a heating pipe (5H), electricity + liquid air cooling + high temperature water to superheated steam temperature supply equipment (3D) feed drive + double-side center support counter-rotating compressed air (28a) drive energy storage Cycle coalescence engine 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), 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, compressed by simple compressor (3s) one or more times, heat recovered by high pressure high temperature water heating pipe (5H) for each compression, electricity + liquid air cold heat + high temperature Water-to-superheated steam temperature supply equipment (3D) feed drive + both center support counter-rotating compressed air (28a) drive coalescence various energy storage cycle coalescing engine 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 the rotation of sunlight at a right angle in the vertical direction, and as a device for controlling rotation at a right angle in the east-west direction by using buoyancy. Horizontal 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) Compress one or more times, recover heat with high-pressure high-temperature water heating pipe (5H) for each compression, electricity + liquid air cooling + high-temperature water to superheated steam temperature supply equipment (3D) feed drive + double-side center support double Reverse compressed air (28a) drive coalescence Various energy conservation cycle combined institutions and coalescence how to.   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) Compressed one or more times with a simple compressor (3s) of extremely inexpensive power generation and electric drive, recovered heat with a high-pressure high-temperature water heating pipe (5H) for each compression, electricity + liquid air cold heat + Hot water to superheated steam temperature supply facility (3D) feed drive + sides center support counter-rotating 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 and electric drive, recovered heat with a high-pressure high-temperature water heating pipe (5H) for each compression, electricity + liquid air cold + high-temperature water to superheated steam Various energy storage cycle coalescing engines and coalescence methods that combine warm heat equipment (3D) feed drive + both center support counter-rotating 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 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 Various energy to recover heat with water heating pipe (5H) to combine electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) feed drive + both sides center support counter-rotating compressed air (28a) drive Storage cycle coalescence engine and coalescence 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) 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) Compressed one or more times with a simple compressor (3s) of extremely inexpensive power generation and electric drive, recovered heat with a high-pressure high-temperature water heating pipe (5H) for each compression, electricity + liquid air cold heat + Various energy storage cycle coalescence engines and coalescence methods for combining hot water to superheated steam heat supply equipment (3D) feed drive + both center support counter-rotating 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) 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, heat is recovered with a 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 Counter-rotating compressed air (28a) Various energy conservation cycle combined institutions and coalescence how to dynamic union.   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) Extremely inexpensive power generation Electric drive, compressed by simple compressor (3s) one or more times, heat recovered by high pressure high temperature water heating pipe (5H) for each compression, electricity + liquid air Cold + hot water to superheated steam temperature Supply equipment (3D) feed drive + sides center support counter-rotating 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 counter-rotating compressed air (28a) driven 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) ) Liquid oxygen (5K) superheated steam (50) receiving drive + both center support counter-rotating compressed air (28a) driving 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 received and driven to a plurality of theoretical combustion chambers (4Q) + both center support counter-rotating compressed air (28a) and 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) ) Liquid energy (5K) superheated steam (50) is supplied to a plurality of theoretical combustion chambers (4Q) combined drive and double-side center support counter-rotating compressed air (28a) and various energy storage cycle combined engines and 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) ) Various oxygen storage cycle coalescence engines and coalescence methods in which liquid oxygen (5K) superheated steam (50) is supplied to a plurality of theoretical combustion chambers (4Q) and combined rocket combustion drive + both center support counter-rotating compressed air (28a) is driven.   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 additional drive + both center support counter-rotating compressed air (28a) and 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) ) Combined rocket combustion + jet combustion drive + double-side center support counter-rotating compressed air (28a) for receiving liquid oxygen (5K) superheated steam (50) in multiple theoretical combustion chambers (4Q) 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 received in multiple theoretical combustion chambers (4Q) and rocket combustion is performed. Others are jet combustion + both-side center support counter-rotating compressed air (28a) and various energy storage cycle combined engines 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 received in multiple theoretical combustion chambers (4Q) by rocket combustion, and the other theoretical combustion chambers (4Q) are jet combustion + both-side center support counter-rotating 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) ) Liquid oxygen (5K) superheated steam (50) is received in multiple rocket combustion chambers (4Q), and the other theoretical combustion chambers (4Q) are jet combustion driven + both center support counter-rotating compressed air (28a) Various energy storage cycle coalescence engines and coalescence methods 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 chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression (4Q) Super high pressure fuel combustion + Both sides center supported counter-rotating compressed air (28a) Combustion simple gas Various energy storage cycle coalescing engines and coalescence methods for driving an engine (88d) 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, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double-side center support counter-rotating compressed air (28a) combustion, simple gas engine (88d) drive and automobile drive 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, and driving a simple gas engine (88d) as a theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double-side center support counter-rotating compressed air (28a) combustion Various energy storage cycle coalescence engines and coalescence methods for driving automobiles.   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 (4Q) Super high pressure fuel combustion + Both sides center supported counter-rotating compressed air (28a) Combustion simple gas Engine (88d) Drive generator (1) Various energy storage cycle coalescing engine and coalescence method for accumulating power in the drive battery (1A) and driving the battery drive wheel (4J) rotating simple gas engine vehicle (7d).   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 counter-rotating compressed air (28a) combustion as simple gas engine (88d) drive generator (1 ) Various energy storage cycle coalescence engines and coalescence methods that store in the drive battery (1A) and drive the battery drive wheel (4J) rotating simple gas engine vehicle (7d).   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 + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support counter-rotating compressed air (28a) combustion, simple gas engine (88d) drive power generation (1) Various energy storage cycle coalescence engine and coalescence method for storing in the drive storage battery (1A) and driving the battery drive wheel (4J) rotating simple gas engine vehicle (7d).   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 (4Q) Super high pressure fuel combustion + Both sides center supported counter-rotating compressed air (28a) Combustion simple gas Engine (88d) Drive generator (1) Various energy storage cycle coalescence engine and coalescence that are stored in the drive battery (1A) and driven by a simple gas engine vehicle (7d) 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) ) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double-side center support counter-rotating compressed air (28a) combustion as simple gas engine (88d) drive generator (1 ) Various energy storage cycle coalescence engines and coalescence methods for storing in the drive accumulator (1A) and driving a simple gas engine vehicle (7d) capable of rotating the accumulator drive wheel (4J) and normal wheels.   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 + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support counter-rotating compressed air (28a) combustion, simple gas engine (88d) drive power generation (1) Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine vehicle (7d) capable of accumulating in a drive storage battery (1A) and rotating the battery drive wheels (4J) and normal wheels.   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 (4Q) Super high pressure fuel combustion + Both sides center supported counter-rotating compressed air (28a) Combustion simple gas Various energy storage cycle coalescence engine and coalescence method for driving the engine (88d) and driving a simple gas engine automobile (7d).   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 (4Q) Super high pressure fuel combustion + Both sides center supported counter-rotating compressed air (28a) Combustion simple gas Various energy storage cycle coalescence engine and coalescence method for driving the engine (88d) 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) ) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double-side center support counter-rotating compressed air (28a) combustion as simple gas engine (88d) and screw ( 7C) Various energy storage cycle coalescence engines and coalescence methods for driving a 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, and driving a simple gas engine (88d) as a theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double-side center support counter-rotating compressed air (28a) combustion Various energy storage cycle coalescence engine and coalescence method for 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) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression (4Q) Super high pressure fuel combustion + Both sides center supported counter-rotating compressed air (28a) Combustion simple gas Various energy storage cycle coalescence engines and coalescence methods for driving the engine (88d) 1 to plural and driving the screw (7C) plural 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, driving a simple gas engine (88d) one or more as a theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double-side center support counter-rotating compressed air (28a) combustion Various energy storage cycle coalescing engine and coalescence method for driving a screw (7C) multiple rotation 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 + high temperature water, theoretical combustion chamber (4Q) super high pressure fuel combustion + both sides center support counter-rotating compressed air (28a) combustion as simple gas engine (88d) 1 Various energy storage cycle coalescence engine and coalescence method for driving a plurality of screws and driving a screw (7C) 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 air compression (4Q) Super high pressure fuel combustion + Both sides center supported counter-rotating compressed air (28a) Combustion simple gas Various energy storage cycle coalescence engines and coalescence methods for driving the engine (88d) 1 to plural and driving the screw (7C) plural rotation simple gas engine ship (7e).   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, driving a simple gas engine (88d) one or more as a theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double-side center support counter-rotating compressed air (28a) combustion Various energy storage cycle coalescing engine and coalescence method for driving a screw (7C) multi-turn simple gas engine ship (7e).   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 + high temperature water, theoretical combustion chamber (4Q) super high pressure fuel combustion + both sides center support counter-rotating compressed air (28a) combustion as simple gas engine (88d) 1 Various energy storage cycle coalescing engines and coalescence methods for driving a plurality of screws and driving a screw (7C) multiple rotation simple gas engine ship (7e).   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 (4Q) Super high pressure fuel combustion + Both sides center supported counter-rotating compressed air (28a) Combustion simple gas Various energy storage cycle coalescence engines and coalescence methods for driving the engine (88d) and driving a simple gas engine ship (7e).   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 (4Q) Super high pressure fuel combustion + Both sides center supported counter-rotating compressed air (28a) Combustion simple gas Various energy storage cycle coalescence engines and coalescence methods for driving the engine (88d) and driving the propulsion vessel such as the screw (7C) rotating simple water injection engine (88e).   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 counter-rotating compressed air (28a) combustion as simple gas engine (88d) and screw ( 7C) Various energy storage cycle coalescence engines and coalescence methods for driving an injection propulsion ship such as a rotary simple water injection engine (88e).   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, and driving a simple gas engine (88d) as a theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double-side center support counter-rotating compressed air (28a) combustion Various energy storage cycle coalescence engine and coalescence method for driving an injection propulsion ship such as a screw (7C) rotation simple water injection engine (88e).   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 (4Q) Super high pressure fuel combustion + Both sides center supported counter-rotating compressed air (28a) Combustion simple gas Various energy storage cycle coalescence engines and coalescence methods for driving the engine (88d) 1 to plural and driving the propulsion and propulsion ship such as the screw (7C) plural rotation simple water injection engine (88e).   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, driving a simple gas engine (88d) one or more as a theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double-side center support counter-rotating compressed air (28a) combustion Various energy storage cycle coalescence engine and coalescence method for driving a propulsion propulsion ship such as a screw (7C) multiple rotation simple water injection engine (88e).   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 + high temperature water, theoretical combustion chamber (4Q) super high pressure fuel combustion + both sides center support counter-rotating compressed air (28a) combustion as simple gas engine (88d) 1 Various energy storage cycle coalescing engines and coalescence methods for driving a plurality of driven propulsion vessels such as a screw (7C) multi-turn simple water injection engine (88e).   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 (4Q) Super high pressure fuel combustion + Both sides center supported counter-rotating compressed air (28a) Combustion simple gas Various energy storage cycle coalescence engines and coalescence methods for driving the engine (88d) 1 to plural and driving the screw (7C) multiple rotation simple water injection engine (88e) 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, driving a simple gas engine (88d) one or more as a theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double-side center support counter-rotating compressed air (28a) combustion Screw (7C) multi-rotation simple water injection engine (88e), 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 + high temperature water, theoretical combustion chamber (4Q) super high pressure fuel combustion + both sides center support counter-rotating compressed air (28a) combustion as simple gas engine (88d) 1 Various energy storage cycle coalescence engines and coalescence methods for driving a plurality of driven screw (7C) multiple rotation simple water injection engines (88e), 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 air compression (4Q) Super high pressure fuel combustion + Both sides center supported counter-rotating compressed air (28a) Combustion simple gas Various energy storage cycle coalescing engine and coalescence method for driving the engine (88d) and driving a simple water injection engine (88e) injection propulsion screw injection 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) which receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression Multiple super high pressure fuel combustion injection propulsion + Both sides center support counter-rotating compressed air (28a) combustion Various energy storage cycle coalescence engines and coalescence methods for driving a jet propulsion ship such as a simple water injection engine (88e).   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) ) Simple water injection engine (88e) that receives cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) multiple ultra-high pressure fuel combustion injection propulsion + both-side center support counter-rotating compressed air (28a) combustion Various energy storage cycle coalescence engine and coalescence method for driving an equal injection propulsion 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) ) Simple water injection engine that receives cheaper liquid oxygen (5K) + electricity + hot water and burns theoretical combustion chamber (4Q) multiple ultra high pressure fuel combustion injection propulsion + both-side center support counter-rotating compressed air (28a) combustion (88e) Various energy conservation cycle coalescing engines and coalescence methods for driving an injection propulsion 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 has a compression volume of 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 (88e) that is 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) equipped with air suction channel, multiple ultra high pressure fuel combustion injection propulsion + both sides center support counter-rotating compressed air (28a) combustion Various energy storage cycle coalescing engine and coalescence method for driving an injection propulsion ship such as a water injection engine (88e).   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 channel, multiple ultra high pressure fuel combustion injection propulsion + both sides center support counter-rotating compressed air (28a) combustion Various energy storage cycle coalescence engines and coalescence methods for driving a jet propulsion ship such as a simple water injection engine (88e).   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 has a compression volume of 21/60000 of air compression Various energy storage cycle coalescing engines and coalescence methods for driving a simple water injection engine (88e), such as a compressed water (28a) combustion, and a simple water injection engine ship (7g).   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) equipped with air suction channel, multiple ultra high pressure fuel combustion injection propulsion + both sides center support counter-rotating compressed air (28a) combustion Various energy storage cycle coalescence engines and coalescence methods for driving a water injection engine (88e) or other such propulsion simple water injection engine ship (7g).   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 channel, multiple ultra high pressure fuel combustion injection propulsion + both sides center support counter-rotating compressed air (28a) combustion A simple water injection engine (88e), etc., an injection propulsion simple water injection engine ship (7g) and various energy storage cycle combining engines and combining 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) ) Simple water injection engine that receives cheaper liquid oxygen (5K) and compresses the compression volume to 21/60000 of air compression by multiple combustion chambers (4Q) + both sides center supported counter-rotating compressed air (28a) combustion (88e) Equip propulsion simple water injection engine ship (7g) Various energy storage cycle coalescence engine and coalescence method for driving.   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) which receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression Multiple super high pressure fuel combustion injection propulsion + Both sides center support counter-rotating compressed air (28a) combustion Various energy storage cycle coalescing engine and coalescence method for making a simple injection engine (88f) 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) ) Simple injection engine (88f) injection that receives cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) multiple ultra high pressure fuel combustion injection propulsion + double side center support counter-rotating compressed air (28a) combustion Various energy conservation cycle coalescence engines and coalescence methods for propulsion 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) ) Simple injection engine that receives cheaper liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) multiple ultra-high pressure fuel combustion injection propulsion + bilateral center support counter-rotating compressed air (28a) combustion ( 88f) Various energy conservation cycle coalescing engines and coalescence methods for making jet propulsion 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 has a compression volume of 21/60000 of air compression Various energy storage cycle coalescing engine and coalescence method for making a simple injection engine (88f) 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) equipped with air suction channel, multiple ultra high pressure fuel combustion injection propulsion + both sides center support counter-rotating compressed air (28a) combustion Various energy conservation cycle coalescence engine and coalescence method for making an injection engine (88f) 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) equipped with air suction channel, multiple ultra high pressure fuel combustion injection propulsion + both sides center support counter-rotating compressed air (28a) combustion Various energy storage cycle coalescing engine and coalescence method for making a simple injection engine (88f) 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 has a compression volume of 21/60000 of air compression A simple injection engine (88f) that uses compressed air (28a) combustion, a simple injection engine, and an airplane (7h).   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) equipped with air suction channel, multiple ultra high pressure fuel combustion injection propulsion + both sides center support counter-rotating compressed air (28a) combustion Various energy storage cycle coalescence engine and coalescence method for driving an injection engine (88f) injection propulsion simple injection airplane (7h).   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 channel, multiple ultra high pressure fuel combustion injection propulsion + both sides center support counter-rotating compressed air (28a) combustion Various energy storage cycle coalescence engine and coalescence method for driving simple injection engine (88f) injection propulsion simple injection airplane (7h).   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) ) A simple injection engine that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression multiple combustion + 4 side center support counter-rotating compressed air (28a) combustion ( 88f) Injection propulsion simple injection engine airplane (7h) Various energy storage cycle coalescing engine and coalescence method for driving.   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 (4Q) Super high pressure fuel combustion + Both sides center supported counter-rotating compressed air (28a) Combustion simple gas Various energy storage cycle coalescence engines and coalescence methods for driving the engine (88d) 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) ) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double-side center support counter-rotating compressed air (28a) combustion as simple gas engine (88d) driving propeller ( 7A) Various energy storage cycle coalescence engines and coalescence methods for driving a 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 + hot water, and driving a simple gas engine (88d) as a theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double-side center support counter-rotating compressed air (28a) combustion Various energy storage cycle coalescence engine and coalescence method for 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) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression (4Q) Super high pressure fuel combustion + Both sides center supported counter-rotating compressed air (28a) Combustion simple gas Engine (88d) 1 to multiple energy storage cycle coalescence engine and coalescence method for driving a plurality of propellers (7A) and driving 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) ) Receiving cheaper liquid oxygen (5K) + electricity, driving a simple gas engine (88d) one or more as a theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double-side center support counter-rotating compressed air (28a) combustion Propeller (7A) Various energy storage cycle coalescence engine and coalescence method for driving a multi-turn 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 + high temperature water, theoretical combustion chamber (4Q) super high pressure fuel combustion + both sides center support counter-rotating compressed air (28a) combustion as simple gas engine (88d) 1 Various energy storage cycle coalescing engine and coalescence method for driving a plurality of propellers (7A) to drive a multi-rotation 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 (4Q) Super high pressure fuel combustion + Both sides center supported counter-rotating compressed air (28a) Combustion simple gas Engine (88d) 1 to multiple energy storage cycle coalescence engine and coalescence method for driving a plurality of propellers (7A) and a multi-turn simple gas engine airplane (7f).   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, driving a simple gas engine (88d) one or more as a theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double-side center support counter-rotating compressed air (28a) combustion Various energy storage cycle coalescing engines and coalescence methods for driving a propeller (7A) multi-turn simple gas engine airplane (7f).   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 + high temperature water, theoretical combustion chamber (4Q) super high pressure fuel combustion + both sides center support counter-rotating compressed air (28a) combustion as simple gas engine (88d) 1 Various energy storage cycle coalescing engines and coalescence methods for driving a plurality of propellers (7A) and a multi-turn simple gas engine airplane (7f).   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 (4Q) Super high pressure fuel combustion + Both sides center supported counter-rotating compressed air (28a) Combustion simple gas Various energy storage cycle coalescence engine and coalescence method for driving the engine (88d) and driving the propeller (7A) rotating simple gas engine airplane (7f).   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 (4Q) Super high pressure fuel combustion + Both sides center supported counter-rotating compressed air (28a) Combustion simple gas Engine (88d) driving 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) ) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double-side center support counter-rotating compressed air (28a) combustion as simple gas engine (88d) driven rotor blade (7B ) Various energy conservation cycle coalescence engines and coalescence methods that rotate and drive the aircraft.   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 + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double side center support counter-rotating compressed air (28a) combustion, simple gas engine (88d) drive rotation Various energy storage cycle coalescing engine and coalescence method for rotating a wing (7B) 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 air compression (4Q) Super high pressure fuel combustion + Both sides center supported counter-rotating compressed air (28a) Combustion simple gas Engine (88d) 1 to multiple drive rotor blades (7B) various energy storage cycle coalescing engine and coalescence method for driving an airplane by making 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, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double side center support counter-rotating compressed air (28a) combustion as simple gas engine (88d) 1 to multiple drive rotation Wings (7B) Various energy storage cycle coalescing engines and coalescence methods for driving a plurality of wings to drive an airplane.   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 + high temperature water, theoretical combustion chamber (4Q) super high pressure fuel combustion + both sides center support counter-rotating compressed air (28a) combustion as simple gas engine (88d) 1 Plural drive rotor blades (7B) Various energy storage cycle coalescing engine and coalescence method for driving 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 air compression (4Q) Super high pressure fuel combustion + Both sides center supported counter-rotating compressed air (28a) Combustion simple gas Engines (88d) 1 to multiple drive rotor blades (7B) various energy storage cycle coalescing engines and coalescence methods for driving the rotor blade airplane (7i) by rotating 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, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double side center support counter-rotating compressed air (28a) combustion as simple gas engine (88d) 1 to multiple drive rotation Various energy storage cycle coalescing engine and coalescence method for driving a wing airplane (7i) by rotating a plurality of wings (7B).   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 + high temperature water, theoretical combustion chamber (4Q) super high pressure fuel combustion + both sides center support counter-rotating compressed air (28a) combustion as simple gas engine (88d) 1 Various energy storage cycle coalescing engine and coalescence method for driving a multi-rotor blade (7B) and rotating a rotor blade airplane (7i).   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 (4Q) Super high pressure fuel combustion + Both sides center supported counter-rotating compressed air (28a) Combustion simple gas Engine (88d) driving rotor blade (7B) Various energy storage cycle coalescence engine and coalescence method for rotating rotor blade airplane (7i) 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 air compression (4Q) Super high pressure fuel combustion + Both sides center supported counter-rotating compressed air (28a) Combustion simple gas Engine (88d) drive propeller (7A) rotating and simple injection engine (88f) injection propulsion airplane driving 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) ultra high pressure fuel combustion + double-side center support counter-rotating compressed air (28a) combustion as simple gas engine (88d) drive propeller (7A) Various energy storage cycle coalescence engine and coalescence method for rotating and driving simple injection engine (88f) 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 + double-side center support counter-rotating compressed air (28a) combustion, simple gas engine (88d) drive propeller (7A) Rotating and simple injection engine (88f) Various energy storage cycle merging engines and merging methods 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 air compression (4Q) Super high pressure fuel combustion + Both sides center supported counter-rotating compressed air (28a) Combustion simple gas Engine (88d) 1 -multiple drive propeller (7A) multiple rotations and simple injection engine (88f) 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) ) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double side center support counter-rotating compressed air (28a) combustion as simple gas engine (88d) 1 to multiple drive propellers (7A) Various energy storage cycle coalescing engine and coalescing method for driving a plurality of rotations and simple injection engine (88f) 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 + high temperature water, theoretical combustion chamber (4Q) super high pressure fuel combustion + both sides center support counter-rotating compressed air (28a) combustion as simple gas engine (88d) 1 A multi-drive propeller (7A), a simple injection engine (88f), and a multi-rotation propulsion (88f) injection propulsion airplane driven 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 air compression (4Q) Super high pressure fuel combustion + Both sides center supported counter-rotating compressed air (28a) Combustion simple gas Engine (88d) 1-Plural drive propeller (7A) Various energy storage cycle coalescence engine and coalescence method for driving multiple injection, simple injection engine (88f) injection propulsion simple gas engine airplane (7f), 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, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double side center support counter-rotating compressed air (28a) combustion as simple gas engine (88d) 1 to multiple drive propellers (7A) Various energy storage cycle coalescence engines and coalescence methods for driving a plurality of rotations and driving simple injection engines (88f) injection propulsion simple gas engine airplanes (7f) 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 + high temperature water, theoretical combustion chamber (4Q) super high pressure fuel combustion + both sides center support counter-rotating compressed air (28a) combustion as simple gas engine (88d) 1 Multi-drive propeller (7A) Various energy storage cycle coalescing engine and coalescence method for driving multiple injection, simple injection engine (88f) injection propulsion simple gas engine airplane (7f), 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 air compression (4Q) Super high pressure fuel combustion + Both sides center supported counter-rotating compressed air (28a) Combustion simple gas Engine (88d) drive propeller (7A), simple injection engine (88f) injection propulsion simple gas engine airplane (7f), etc. to drive 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) ) Theoretical combustion chamber (4Q) which receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression (4Q) super high pressure fuel combustion + both sides center support counter-rotating compressed air (28a) combustion, high pressure Various energy storage cycle coalescence engine and coalescence method for injecting high-temperature combustion gas (5M) and driving a simple gas engine (88d).   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 sides center support counter-rotating compressed air (28a) combustion, high pressure high temperature combustion gas (5M) is injected Various energy storage cycle coalescence engine and coalescence method for driving a simple gas engine (88d).   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 counter-rotating compressed air (28a) combustion, high pressure high temperature combustion gas (5M) Various energy storage cycle coalescing engine and coalescence method for driving a simple gas engine (88d) by injecting a gas.   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) which receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression (4Q) super high pressure fuel combustion + both sides center support counter-rotating compressed air (28a) combustion, high pressure Various energy storage cycle coalescence engines and coalescence methods driven by a simple gas engine (88d) that injects a high-temperature combustion gas (5M) and reverses 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) super high pressure fuel combustion + both sides center support counter-rotating compressed air (28a) combustion, high pressure high temperature combustion gas (5M) is injected The horizontal axis (1h) is a simple gas engine (88d) that 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) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support counter-rotating compressed air (28a) combustion, high pressure high temperature combustion gas (5M) Various energy storage cycle coalescing engine and coalescence method driven by a simple gas engine (88d) that inverts the horizontal axis (1h) and reverses.   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) which receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression (4Q) super high pressure fuel combustion + both sides center support counter-rotating 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 (88d) with a horizontal axis (1h) counter-inversion.   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 sides center support counter-rotating compressed air (28a) combustion, high pressure high temperature combustion gas (5M) is injected The horizontal axis (1h) is a combination of a plurality of simple inversion gas engines (88d) and 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 counter-rotating compressed air (28a) combustion, high pressure high temperature combustion gas (5M) Various energy storage cycle coalescing engine and coalescence method for driving a plurality of simple gas engines (88d) with a horizontal axis (1h) counter-rotating multiple times.   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) which receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression (4Q) super high pressure fuel combustion + both sides center support counter-rotating 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 (88d) with a horizontal axis (1h) counter-inversion.   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 (4Q) Super high pressure fuel combustion + Both sides center supported counter-rotating compressed air (28a) Combustion simple gas Various energy storage cycle coalescing engines and coalescence methods for the engine (88d).   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 + both sides center support counter-rotating compressed air (28a) various energy storage to make simple gas engine (88d) combustion 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, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double-side center support counter-rotating compressed air (28a) combustion into simple gas engine (88d) 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) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression (4Q) Ultra high pressure fuel combustion + Double-side center support counter-rotating compressed air (28a) Maximum speed Various energy storage cycle coalescing engine and coalescence method to make simple gas engine (88d).   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 counter-rotating compressed air (28a) to a simple gas engine (88d) that maximizes speed as 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) ) Simple gas engine that receives cheaper liquid oxygen (5K) + electricity + hot water, and achieves maximum speed as theoretical combustion chamber (4Q) super high pressure fuel combustion + double-side center support counter-rotating compressed air (28a) combustion ( 88d) 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) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression (4Q) Super high pressure fuel combustion + Double-side center support counter-rotating compressed air (28a) maximum drive Various energy storage cycle coalescence engine and coalescence method to make simple gas engine (88d) to 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) ) Simple gas engine (88d) which receives cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultrahigh pressure fuel combustion + double-side center support counter-rotating compressed air (28a) combustion and maximum driving speed 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) ) Simple gas engine that receives cheaper liquid oxygen (5K) + electricity + high-temperature water and achieves maximum driving speed as theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double-side center support counter-rotating compressed air (28a) combustion (88d) 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) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression (4Q) Super high-pressure fuel combustion + Double-side center supported counter-rotating compressed air (28a) Maximum speed Various energy storage cycle coalescing engine and coalescence method to make simple gas engine (88d).   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 that receives cheaper liquid oxygen (5K), compresses liquid together with liquid fuel (1c) and water (52a), and injects and burns ultra-high-pressure compressed fuel with air compression of 21/60000 volume, etc. (4Q) + both center support counter-rotating compressed air (28a) various energy storage cycle coalescence engine and coalescence method 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) ) Theory of receiving cheaper liquid oxygen (5K) + electricity, compressing liquid together with liquid fuel (1c) and water (52a), and compressing the compression volume with 21/60000 volume of air compression, etc. Various energy storage cycle coalescence engines and coalescence methods for combustion chamber (4Q) + both center support counter-rotating 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, liquid compression with liquid fuel (1c) and water (52a), ultra-high pressure compressed fuel injection with air compression of 21/60000 volume, etc. Various energy storage cycle coalescing engine and coalescence method for burning the theoretical combustion chamber (4Q) + both center support counter-rotating 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), compress liquid with liquid fuel (1c) and water (52a) and heat to the optimal temperature on the inner wall of the theoretical combustion chamber (4Q) 28a) Various energy storage cycle coalescence engines and coalescence methods for 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) + electricity, compress liquid with liquid fuel (1c) and water (52a) and heat to the optimum temperature on the inner wall of the theoretical combustion chamber (4Q) Various energy storage cycle coalescence engine and coalescence method for burning 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, compress liquid with liquid fuel (1c) and water (52a), and heat to the optimum temperature on the inner wall of the theoretical combustion chamber (4Q) Various energy storage cycle coalescence engine and coalescence method for burning heavy inverted 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), compress liquid with liquid fuel (1c) and water (52a) and heat to the optimal temperature on the inner wall of the theoretical combustion chamber (4Q) 28a) Various energy storage cycle coalescence engines and coalescence methods that open the 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) ) Receive cheaper liquid oxygen (5K) + electricity, compress liquid with liquid fuel (1c) and water (52a) and heat 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 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) ) Receive cheaper liquid oxygen (5K) + electricity + hot water, compress liquid with liquid fuel (1c) and water (52a), and heat to the optimum temperature on the inner wall of the theoretical combustion chamber (4Q) Various energy storage cycle coalescence engines and coalescence methods for opening the heavyly inverted 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) ) Receive cheaper liquid oxygen (5K) + hot water, compress liquid with liquid fuel (1c) and water (52a) and heat to the optimum temperature on the inner wall of the theoretical combustion chamber (4Q) Various energy storage cycle coalescence engine and coalescence method for injecting compressed air (28a) combustion oxygen injection nozzle (6L) + fuel injection nozzle (6X) + superheated steam injection nozzle (6A) together with open received 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) ) 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 Various energy storage cycle coalescing engine and coalescence method to make two types of theoretical combustion chambers (4Q) to burn center support counter-rotating 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, open heated oxygen injection nozzle (6L) + fuel injection nozzle (6X) + superheated steam injection nozzle (6A) to the optimum temperature + heat superheated steam (50) + Both energy saving cycle coalescence engine and coalescence method to make two kinds of theoretical combustion chambers (4Q) to burn both sides center support counter-rotating 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, open heated oxygen injection nozzle (6L) + fuel injection nozzle (6X) + superheated steam injection nozzle (6A) to the optimum temperature + superheated steam (50 ) Is heated + two-side center support counter-rotating compressed air (28a), and two kinds of theoretical combustion chambers (4Q) for burning are combined with 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) ) 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-side center support counter-rotating 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) Various energy storage cycle coalescence engine and coalescence method to make high temperature + both sides center support counter-rotating compressed air (28a) combustion two kinds of 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) ) 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 center support counter-rotating compressed air (28a) combustion 2 types of theoretical combustion chamber (4Q) 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) ) 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) + Various energy storage cycle coalescence engine and coalescence method to make two-side center support counter-rotating compressed air (28a) combustion two kinds of 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) ) 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-side center support counter-rotating 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 ) + Both center support counter-rotating 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. Various energy storage cycle coalescence engines and coalescence methods for heating the outer peripheral superheated steam (50) including the received superheated steam by combustion at a temperature higher than + C, and both-side center support counter-rotating compressed air (28a) combustion, two types of 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) ) Receiving cheaper liquid oxygen (5K), high-pressure high-temperature combustion gas (5M) injection accelerated injection with multiple theoretical combustion chambers (4Q) + both-side center support counter-rotating compressed air (28a) simple water injection Various energy storage cycle coalescence engines and coalescence methods in an engine (88e).   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, high-pressure high-temperature combustion gas (5M) with multiple theoretical combustion chambers (4Q) + accelerated injection + double-side center support counter-rotating compressed air (28a) Various energy storage cycle coalescence engine and coalescence method in water injection engine (88e).   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 + high temperature water, high pressure high temperature combustion gas (5M) injection accelerating injection with multiple theoretical combustion chambers (4Q) + both sides center support counter-rotating compressed air (28a) Various energy storage cycle coalescence engine and coalescence method in a simple water injection engine (88e) 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) and use high pressure high temperature combustion gas (5M) with multiple theoretical combustion chambers (4Q) (4Q) oxygen + fuel + superheated steam on the inner wall + Various energy storage cycle coalescence engine and coalescence method in a simple water injection engine (88e) that combusts both sides center support counter-rotating 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, 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 counter-rotating compressed air (28a) various energy storage cycle coalescing engine and coalescence method for simple water injection engine (88e) 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) ) 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 coalescing engine and coalescence method which is a simple water injection engine (88e) which burns and uses + both center support counter-rotating compressed air (28a) and 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) ) 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 engine and coalescence method in the form of a simple water injection engine (88e) for theoretical combustion chamber (4Q) combustion + both center support counter-rotating 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 engine and coalescence method in the form of a simple water injection engine (88e) for theoretical combustion chamber (4Q) combustion + both center support counter-rotating 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 coalescing engines and coalescence methods that are heated to a theoretical combustion chamber (4Q) combustion + both center supported counter-rotating compressed air (28a) combustion into a simple water injection engine (88e).   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 coalescing engine and coalescence method, which is a simple water injection engine (88e) which is heated to the optimum temperature to produce the theoretical combustion chamber (4Q) combustion + both-side center support counter-rotating 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), heated oxygen + fuel + superheated steam at the optimal temperature on the inner wall, theoretical combustion chamber (4Q) combustion + both sides center support counter-rotating compressed air (28a) simple water for combustion Various energy storage cycle coalescing engine and coalescence method for an injection engine (88e).   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 and burn the theoretical combustion chamber (4Q) combustion + both sides center support counter-rotating compressed air (28a) combustion Various energy storage cycle coalescing engine and coalescence method in a simple water injection engine (88e).   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 + hot water is received, oxygen + fuel + superheated steam is heated at the optimum temperature on the inner wall, theoretical combustion chamber (4Q) combustion + both sides center support counter-rotating compressed air (28a ) Various energy storage cycle coalescing engine and coalescence method in a simple water injection engine (88e) 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), heat oxygen + fuel + superheated steam on the inner wall at the optimum temperature and burn it in the theoretical combustion chamber (4Q) + easy on both sides center supported counter-rotating compressed air (28a) Various energy storage cycle coalescence engine and coalescence method in water injection engine (88e).   Magnetic type bearing load approaching 0 + super high speed circumferential speed horizontal + both sides center support counter-rotating compressed air (28a) combustion blade ratio critical material gravity turbine (8U) electricity + liquid of extremely low cost electric power production Air-cooled heat + hot water to superheated steam temperature supply equipment (3D) receives cheap liquid oxygen (5K) + electricity and heats oxygen + fuel + superheated steam at the inner wall at the optimum temperature and burns in the theoretical combustion chamber (4Q) + Both energy storage cycle coalescence engine and coalescence method in a simple water injection engine (88e) of both sides center support counter-rotating 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, oxygen + fuel + superheated steam on the inner wall is heated to the optimum temperature and burned in the theoretical combustion chamber (4Q) + double-side center support counter-rotating compressed air ( 28a) Combining various energy storage cycle engines and combining methods in a simple water injection engine (88e) 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), 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 Various energy storage cycle coalescing engine and coalescence method in the form of a simple water injection engine (88e) that combusts injection + both sides center support counter-rotating 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, 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 engine and coalescence method, which is a simple water injection engine (88e) that burns by heating injection + both sides center support counter-rotating 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 engines and coalescence methods, wherein (50) is a simple water injection engine (88e) for heating injection + both-side center support counter-rotating 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) + 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 coalescing engines and coalescence methods, including a simple water injection engine (88e) that burns superheated steam (50) including heated injection + both sides center support counter-rotating 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), the air (28a) is also provided with a plurality of theoretical combustion chambers (4Q) at the optimum place of the suction injection flow, combustion injection + both sides center support counter-rotating compressed air (28a) combustion Various energy storage cycle coalescing engines and coalescence methods for a simple water injection engine (88e).   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, and air (28a) is provided with a plurality of theoretical combustion chambers (4Q) at the optimum place of the suction injection flow as well as combustion injection + both sides center support counter-rotating compressed air (28a) ) Various energy storage cycle coalescing engine and coalescence method for a simple water injection engine (88e) 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) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, air (28a) suction injection flow at the optimal location with multiple theoretical combustion chambers (4Q) as well as combustion injection + both sides center support counter-rotating compression Various energy storage cycle coalescing engines and coalescing methods in a simple water injection engine (88e) that burns 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) ) Various energy storage cycle coalescence engines and coalescence methods which received cheaper liquid oxygen (5K), made simple water injection engine (88e) and combusted air inlet forward + both sides center support counter-rotating 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) ) Cheaper liquid oxygen (5K) + receiving electricity + both sides center support counter-rotating compressed air (28a) burning, simple water injection engine (88e), various energy storage cycle coalescing engines with forward air inlets 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) ) Cheaper liquid oxygen (5K) + Electricity + High temperature water received + Both sides center supported counter-rotating compressed air (28a) burned to make simple water injection engine (88e), various energy storage cycles with forward air inlet 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) + burning both sides center support counter-rotating compressed air (28a), making it a simple water injection engine (88e), approaching a straight line with the air inlet facing forward, and the largest bubble at the bottom of the ship 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) ) Cheaper liquid oxygen (5K) + receiving electricity + both sides center support counter-rotating compressed air (28a) burning, making it a simple water injection engine (88e) with the air inlet facing forward and approaching a straight line to the bottom of the ship Various energy storage cycle coalescence engine and coalescence method for jetting bubbles to the maximum.   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 counter-rotating compressed air (28a) burned to make a simple water injection engine (88e) with the air inlet facing forward and approaching a straight line Various energy storage cycle coalescence engine and coalescence method for jetting 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) ) Receive cheaper liquid oxygen (5K) + hot water + both sides center support counter-rotating compressed air (28a) burn, make simple water injection engine (88e) and bring the air inlet forward and approach a straight line Various energy storage cycle coalescence engine and coalescence method for jetting bubbles to the maximum.   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) + combustion on both sides center support counter-rotating compressed air (28a), easy high-pressure high-temperature combustion gas (5M) injection acceleration injection with two types of theoretical combustion chambers (4Q) Various energy storage cycle coalescing engine and coalescence method for an injection engine (88f).   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 counter-rotating compressed air (28a) combustion, high-pressure high-temperature combustion gas (5M) injection accelerated injection with multiple two types of theoretical combustion chamber (4Q) Various energy storage cycle coalescing engines and coalescence methods of the simple injection engine (88f).   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 counter-rotating compressed air (28a) burned, High pressure high temperature combustion gas (5M) with multiple two types of theoretical combustion chambers (4Q) Various energy storage cycle coalescing engine and coalescence method, which is a simple injection engine (88f) 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) ) Receiving cheaper liquid oxygen (5K) + both side center support counter-rotating compressed air (28a), and (4Q) inner wall with 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, which are simple injection engines (88f) that use oxygen + fuel + superheated steam at an optimal 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) + receiving electricity + both sides center support counter-rotating compressed air (28a) and burning with high-pressure and high-temperature combustion gas (5M) equipped with two types of theoretical combustion chambers (4Q) (4Q ) Various energy storage cycle coalescing engine and coalescence method, which is a simple injection engine (88f) that uses oxygen + fuel + superheated steam on the inner wall with optimum temperature heating.   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 counter-rotating compressed air (28a) burned, High pressure high temperature combustion gas (5M) with multiple two types of theoretical combustion chambers (4Q) (4Q) Various energy storage cycle coalescing engines and coalescence methods that are simple injection engines (88f) that use 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) ) Receiving cheaper liquid oxygen (5K) + both side center support counter-rotating compressed air (28a), and (4Q) inner wall with 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, which are made into a simple injection engine (88f) in which oxygen + fuel + superheated steam is heated at an optimal temperature to make two kinds of theoretical combustion chambers (4Q) combustion or 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) ) Less expensive liquid oxygen (5K) + receiving electricity + both sides center support counter-rotating compressed air (28a) and burning with high-pressure and high-temperature combustion gas (5M) equipped with two types of theoretical combustion chambers (4Q) (4Q ) Various energy storage cycle coalescence engine and coalescence method, which is a simple injection engine (88f) in which the inner wall oxygen + fuel + superheated steam is heated to an optimum temperature to make two types of theoretical combustion chamber (4Q) combustion or 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) ) Cheaper liquid oxygen (5K) + Electricity + High temperature water received + Both sides center support counter-rotating compressed air (28a) burned, High pressure high temperature combustion gas (5M) with multiple two types of theoretical combustion chambers (4Q) (4Q) Various energy storage cycle coalescing engines and coalescence methods in which a simple injection engine (88f) is made by heating the oxygen + fuel + superheated steam on the inner wall at the optimum temperature to make two kinds of theoretical combustion chambers (4Q) combustion or 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) + hot water + both-side center support counter-rotating compressed air (28a) and burning with high-pressure and high-temperature combustion gas (5M) equipped with two types of theoretical combustion chambers (4Q) ( 4Q) Various energy storage cycle coalescing engines and coalescence methods that make a simple injection engine (88f) that heats superheated steam containing oxygen + fuel + received high-temperature water on the inner wall to the 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) ) Receiving cheaper liquid oxygen (5K) + combustion on both sides center supported counter-rotating compressed air (28a), heating oxygen + fuel + superheated steam at one type of inner wall at optimal temperature, and two types of theoretical combustion chamber (4Q ) Various energy storage cycle coalescing engine and coalescence method in a simple combustion engine (88f).   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 counter-rotating compressed air (28a), burning oxygen + fuel + superheated steam at one kind of inner wall at the optimum temperature, two kinds of theoretical combustion chambers (4Q) Various energy storage cycle coalescing engines and coalescence methods that are made into a combustion simple injection engine (88f).   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 + double-side center support counter-rotating compressed air (28a) combustion, oxygen + fuel + superheated steam heated at the optimum temperature on one type of inner wall, two types Various energy storage cycle coalescence engine and coalescence method in a simple combustion engine (88f) for 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) + combustion on both sides center supported counter-rotating compressed air (28a), heating oxygen + fuel + superheated steam at one type of inner wall at optimal temperature, and two types of theoretical combustion chamber (4Q ) Various energy storage cycle coalescing engines and coalescence methods made into a simple injection engine (88f) 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) + receiving electricity + both sides center support counter-rotating compressed air (28a), burning oxygen + fuel + superheated steam at one kind of inner wall at the optimum temperature, two kinds of theoretical combustion chambers (4Q) Various energy storage cycle coalescing engines and coalescence methods that are simple injection engines (88f) that 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) ) Cheaper liquid oxygen (5K) + electricity + high-temperature water received + double-side center support counter-rotating compressed air (28a) combustion, oxygen + fuel + superheated steam heated at the optimum temperature on one type of inner wall, two types Various energy storage cycle coalescing engine and coalescence method in a simple combustion engine (88f) that burns in the 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) ) Receiving cheaper liquid oxygen (5K) + combustion on both sides center supported counter-rotating compressed air (28a), heating oxygen + fuel + superheated steam at one type of inner wall at optimal temperature, and two types of theoretical combustion chamber (4Q ) Various energy storage cycle coalescence engines and coalescence methods that are simple injection engines (88f) that heat and inject superheated steam (50) of the high-temperature water heating pipe (5H) by 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 counter-rotating compressed air (28a), burning oxygen + fuel + superheated steam at one kind of inner wall at the optimum temperature, two kinds of theoretical combustion chambers (4Q) Various energy storage cycle coalescing engines and coalescence methods that are simple injection engines (88f) that heat and inject superheated steam (50) of the high-temperature water heating pipe (5H) by 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 + double-side center support counter-rotating compressed air (28a) combustion, oxygen + fuel + superheated steam heated at the optimum temperature on one type of inner wall, two types Various energy storage cycle coalescence engines and coalescence methods that are simple injection engines (88f) that heat and inject superheated steam (50) of a high-temperature water heating pipe (5H) in 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) + high temperature water + both side center support counter-rotating compressed air (28a), oxygen + fuel + superheated steam is heated at optimum temperature on one kind of inner wall, and two kinds of theoretical combustion Various energy storage cycle coalescence engines and coalescence methods, which are simple injection engines (88f) for heating and injecting superheated steam (50) including received superheated steam in the high-temperature water heating pipe (5H) by 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) + both sides center support counter-rotating compressed air (28a), and air (28a) a plurality of two types of theoretical combustion chamber (4Q) injection parts at the optimum place of suction injection flow Various energy storage cycle coalescing engines and coalescence methods that are simple injection engines (88f) that perform combustion injection 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) ) Cheaper liquid oxygen (5K) + electricity received + both sides center support counter-rotating compressed air (28a) burned, air (28a) a plurality of two theoretical combustion chambers (4Q) also in the optimum place of suction injection flow Various energy storage cycle coalescing engine and coalescence method, which is a simple injection engine (88f) 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) + electricity + hot water received + both sides center support counter-rotating compressed air (28a) combustion, air (28a) a plurality of two types of theoretical combustion chambers in the optimum place of suction jet flow (4Q) Various energy storage cycle coalescence engines and coalescence methods that are simple injection engines (88f) that perform 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) ) Receiving cheaper liquid oxygen (5K) + both sides center support counter-rotating compressed air (28a), and rotating with a simple injection engine (88f) to enable vertical ascending and descending various energy storage cycle coalescing engines 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) ) Less expensive liquid oxygen (5K) + receiving electricity + both sides center support counter-rotating compressed air (28a) burning, rotating together with simple injection engine (88f), allowing various vertical energy saving cycles 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) ) Cheaper liquid oxygen (5K) + Electricity + High temperature water received + Both sides center support counter-rotating compressed air (28a) Combustion, rotating with simple injection engine (88f), various energies enabling vertical ascent and descent 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) + both sides center support counter-rotating compressed air (28a) burning, rotating together with simple injection engine (88f) and enabling reverse injection, and various energy storage cycle coalescence engines 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) ) Less energy liquid oxygen (5K) + receiving electricity + both sides center support counter-rotating compressed air (28a) burning, rotating together with simple injection engine (88f), enabling various types of 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) ) Less expensive liquid oxygen (5K) + electricity + high temperature water received + both sides center support counter-rotating compressed air (28a) burned and rotated with a simple injection engine (88f) to enable reverse injection and save various energy 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) + high temperature water + both sides center support counter-rotating compressed air (28a) burned and rotated together with simple injection engine (88f) to enable reverse injection combined with various energy storage cycles 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) ) Supply of electricity + high temperature water (52b) as liquid oxygen production, simple targeted multistage compressor (3t) + liquid oxygen production machine (88g) of electric drive to make simple target intake speed maximum, 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) ) Various energy storage cycle coalescence engines and coalescence methods for producing liquid oxygen by supplying electricity, simple electric multistage compressor (3t) + liquid oxygen producing machine (88g) of electric drive to maximize the target intake 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) ) Various energy storage cycle coalescence engines and coalescence methods, such as electricity + superheated steam to supply liquid oxygen production, simple multistage compressor (3t) + liquid oxygen production machine (88g) of electric drive to maximize the target intake 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) ) Supplying electricity + high temperature water (52b) as liquid oxygen production, simple aiming to maximize the suction speed Electric simple multistage compressor (3t) + liquid oxygen production machine as liquid oxygen production machine (88g) 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) ) Various energy storage cycle coalescence engines and coalescence methods for producing liquid oxygen as a supply of electricity and producing liquid oxygen as a simple multistage compressor (3t) + liquid oxygen production machine (88g) of electric drive that makes liquid oxygen production simple and aimed at maximum.   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) Electricity + Superheated Steam Supply Liquid Oxygen Production, Simple Aimed Multi-stage Compressor (3t) + Liquid Oxygen Manufacture Machine (88g) with Easy Aiming to Maximize Suction Speed 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) ) Supplying electricity + high temperature water (52b) as liquid oxygen production, easy aiming to maximize the suction speed Electric driven simple multistage compressor (3t) + liquid oxygen production machine (88g) as air suction compression heat exchange superheated steam Various energy storage cycle coalescence engine and coalescence method for manufacturing   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 a liquid oxygen production, easy aiming to maximize the suction speed Electricly driven simple multi-stage compressor (3t) + liquid oxygen production machine (88g) as intake air compression heat exchange to produce superheated steam 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) ) Electric + Superheated steam is supplied to produce liquid oxygen, easy aiming to maximize the intake speed Electric driven simple multistage compressor (3t) + Liquid oxygen producing machine (88g) to produce compressed heat exchange superheated steam by sucking air 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) ) Electric + high-temperature water (52b) + superheated steam to supply liquid oxygen, simple target-driven multistage compressor (3t) to maximize suction speed + liquid oxygen generator (88g) to suck air and compress heat Various energy storage cycle coalescence engine and coalescence method for producing 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) ) Supplying electricity + high temperature water (52b) as liquid oxygen production, easy aiming to maximize suction speed, electric driven simple multistage compressor (3t) + liquid oxygen production machine (88g) as liquid nitrogen 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) ) Supplying electricity as liquid oxygen production, easy aiming to maximize suction speed, electric driven simple multistage compressor (3t) + liquid oxygen production machine (88g) as various energy storage cycle coalescence engine and coalescence method 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) Electricity + Superheated Steam Supply Liquid Oxygen Production, Easy Aiming to Maximize Suction Speed Electricly Driven Simple Multistage Compressor (3t) + Liquid Oxygen Production Machine (88g) Various Energy Storage Cycle Combined Engines Producing Liquid Nitrogen 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) ) Supplying electricity + hot water (52b) as liquid oxygen production, easy aiming to maximize suction speed, electric driven simple multistage compressor (3t) + liquid oxygen production machine (88g) as liquid nitrogen production and supply equipment (3D ) Various energy storage cycle coalescence engines and coalescence methods to be supplied to   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 a liquid oxygen production, easy aiming to maximize the suction speed Electricly driven simple multistage compressor (3t) + liquid oxygen as a liquid oxygen production machine (88g) Various energy to supply liquid nitrogen to production supply equipment (3D) 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, simply aiming and maximizing the suction speed Electrically driven simple multistage compressor (3t) + liquid oxygen producing machine (88g) supplying liquid nitrogen to production and supply equipment (3D) 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) ) Supplying electricity + high temperature water (52b) as liquid oxygen production, easy aiming to maximize suction speed, electric multi-stage compressor (3t) + liquid oxygen production machine (88g) as liquid nitrogen + liquid oxygen + superheated steam Various energy storage cycle coalescing engines and coalescence methods for supplying 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) ) Supplying electricity as liquid oxygen production, simple aiming to maximize the intake speed Easy electric multi-stage compressor (3t) + liquid oxygen production machine (88g) as liquid nitrogen + liquid oxygen + superheated steam production supply equipment (3D ) Various energy storage cycle coalescence engines and coalescence methods to be supplied to   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 Electric driven multistage compressor (3t) + liquid oxygen production machine (88g) as liquid nitrogen + liquid oxygen + superheated steam manufactured and supplied Various energy storage cycle coalescence engines and coalescence methods to be supplied to the 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) ) Electricity + hot water (52b) + superheated steam supply liquid oxygen production, easy aiming to maximize intake speed, simple multistage compressor (3t) of electric drive + liquid oxygen production machine (88g) liquid nitrogen + liquid oxygen + Various energy storage cycle coalescence engines and coalescence methods for supplying superheated steam to the production and supply facility (3D).   A structure that maximizes the suction speed of a simple multistage compressor (3t) that uses an extremely low-cost electric drive with an extremely low-priced material gravity turbine (8U) that uses a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed. Various energy storage cycle coalescence engines and coalescence methods.   A structure that maximizes the suction speed of a simple multistage compressor (3t) that uses an extremely low-cost electric drive with an extremely low-priced material gravity turbine (8U) that uses a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed. Various energy storage cycle coalescence engine and coalescence method for air compression.   A structure that maximizes the suction speed of a simple multistage compressor (3t) that uses an extremely low-cost electric drive with an extremely low-priced material gravity turbine (8U) that uses a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed. Various energy storage cycle coalescence engine and coalescence method for compressing air (28a) as   A structure that maximizes the suction speed of a simple multistage compressor (3t) that uses an extremely low-cost electric drive with an extremely low-priced material gravity turbine (8U) that uses a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed. 1 to a plurality of energy storage cycle coalescence engine and coalescence method for compressing a plurality of stages.   A structure that maximizes the suction speed of a simple multistage compressor (3t) that uses an extremely low-cost electric drive with an extremely low-priced material gravity turbine (8U) that uses a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed. As various energy storage cycle coalescing engine and coalescence method for heating 1 to multi-stage compressed water.   A structure that maximizes the suction speed of a simple multistage compressor (3t) that uses an extremely low-cost electric drive with an extremely low-priced material gravity turbine (8U) that uses a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed. Various energy storage cycle coalescence engine and coalescence method for heating 1 to multi-stage compressed high temperature water.   A structure that maximizes the suction speed of a simple multistage compressor (3t) that uses an extremely low-cost electric drive with an extremely low-priced material gravity turbine (8U) that uses a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed. Various energy storage cycle coalescence engines and coalescence methods for heating 1 to multiple-stage compressed superheated steam.   A structure that maximizes the suction speed of a simple multistage compressor (3t) that uses an extremely low-cost electric drive with an extremely low-priced material gravity turbine (8U) that uses a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed. Various energy storage cycle coalescence engines and coalescence methods for heating water with 1 to multiple compression.   A structure that maximizes the suction speed of a simple multistage compressor (3t) that uses an extremely low-cost electric drive with an extremely low-priced material gravity turbine (8U) that uses a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed. Various energy storage cycle coalescence engines and coalescence methods for heating high-temperature water with 1 to multiple compression.   A structure that maximizes the suction speed of a simple multistage compressor (3t) that uses an extremely low-cost electric drive with an extremely low-priced material gravity turbine (8U) that uses a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed. Various energy storage cycle coalescence engine and coalescence method for heating superheated steam with 1 to multiple compression.   A structure that maximizes the suction speed of a simple multistage compressor (3t) that uses an extremely low-cost electric drive with an extremely low-priced material gravity turbine (8U) that uses a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed. Various energy storage cycle coalescence engine and coalescence method for producing superheated steam by compression.   A structure that maximizes the suction speed of a simple multistage compressor (3t) that uses an extremely low-cost electric drive with an extremely low-priced material gravity turbine (8U) that uses a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed. Various energy storage cycle coalescence engine and coalescence method for producing liquid oxygen + superheated steam by compression.   A structure that maximizes the suction speed of a simple multistage compressor (3t) that uses an extremely low-cost electric drive with an extremely low-priced material gravity turbine (8U) that uses a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed. Various energy storage cycle coalescence engine and coalescence method for producing liquid oxygen + liquid nitrogen + superheated steam by compression.   A structure that maximizes the suction speed of a simple multistage compressor (3t) that uses an extremely low-cost electric drive with an extremely low-priced material gravity turbine (8U) that uses a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed. Various energy storage cycle coalescence engine and coalescence method for producing liquid oxygen + liquid nitrogen + high temperature water by compression.   A structure that maximizes the suction speed of a simple multistage compressor (3t) that uses an extremely low-cost electric drive with an extremely low-priced material gravity turbine (8U) that uses a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed. Various energy storage cycle coalescence engine and coalescence method to be supplied to liquid oxygen + superheated steam production and supply equipment (3D) by compression.   A structure that maximizes the suction speed of a simple multistage compressor (3t) that uses an extremely low-cost electric drive with an extremely low-priced material gravity turbine (8U) that uses a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed. Various energy storage cycle coalescence engine and coalescence method to be supplied to liquid oxygen + liquid nitrogen + high pressure superheated steam production / supply facility (3D) by compression.   A structure that maximizes the suction speed of a simple multistage compressor (3t) that uses an extremely low-cost electric drive with an extremely low-priced material gravity turbine (8U) that uses a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed. Various energy storage cycle coalescence engine and coalescence method to be supplied to liquid oxygen + liquid nitrogen + super high pressure superheated steam production / supply facility (3D) by compression.   A structure that maximizes the suction speed of a simple multistage compressor (3t) that uses an extremely low-cost electric drive with an extremely low-priced material gravity turbine (8U) that uses a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed. Various energy storage cycle coalescence engine and coalescence method to be supplied to liquid oxygen + super high pressure superheated steam production and supply facility (3D) by compression.   A structure that maximizes the suction speed of a simple multistage compressor (3t) that uses an extremely low-cost electric drive with an extremely low-priced material gravity turbine (8U) that uses a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed. Various energy storage cycle coalescence engine and coalescence method to be supplied to liquid oxygen + liquid nitrogen + super high pressure superheated steam production / supply facility (3D) by compression.   A structure that maximizes the suction speed of a simple multistage compressor (3t) that uses an extremely low-cost electric drive with an extremely low-priced material gravity turbine (8U) that uses a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed. Various energy storage cycle coalescence engine and coalescence method to be supplied to electricity + liquid oxygen + liquid nitrogen + super high pressure superheated steam production and supply equipment (3D) by compression.   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 engine and coalescence method for receiving cheap liquid oxygen (5K) in a simple gas engine (88d) and fuel injection combustion in compressed air + fuel injection combustion 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 simple injection engine (88f) receive cheap liquid oxygen (5K) by two types of 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) ) Various energy storage cycle coalescence engines and coalescence methods that make the simple water injection engine (88e) low-cost liquid oxygen (5K) receive fuel injection combustion + compressed air and fuel injection combustion into two types of theoretical combustion chambers.   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 gas engine (88d) less expensive liquid oxygen (5K) received fuel injection combustion + compressed air into 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) ) Easier injection engine (88f) receiving cheap liquid oxygen (5K) Fuel injection combustion + Compressed air fuel injection combustion 2 types of theoretical combustion chamber (4Q) Various types of energy equipped with on-off valve (1Q) at 1 type inlet 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) ) Easy water injection engine (88e) receiving 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) Various energy storage cycle coalescence engines and coalescence methods provided.   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) ) Simpler gas engine (88d) receives 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) Various energy storage cycle coalescence engines and coalescence methods provided in the 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) ) More simple injection engine (88f) receives cheap liquid oxygen (5K) fuel injection combustion + compressed air fuel injection combustion into two types of theoretical combustion chamber (4Q) and one type inlet valve (1Q) oxygen injection nozzle ( 6L) Various energy storage cycle coalescence engines and coalescence methods for closing the fuel injection nozzle (6X) and the on-off 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) ) Easy water injection engine (88e) receiving 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) Open / close valve (1Q) Closed oxygen fuel injection Combining 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) ) Simpler gas engine (88d) receives 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 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) ) More simple injection engine (88f) receives cheap liquid oxygen (5K) fuel injection combustion + compressed air fuel injection combustion into two types of theoretical combustion chamber (4Q) and 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) ) Easy water injection engine (88e) receiving 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) Open / close valve (1Q) Closed oxygen fuel injection Combustion rotation output increase 2 types (4Q) Various energy storage cycle coalescing engine that sucks and injects combustion gas (49) by superheated steam (50) injection 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) ) Simpler gas engine (88d) receives 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) Open / close valve (1Q) Closed oxygen fuel injection Combustion rotation output increase 2 types (4Q) Superheated steam (50) injection, combustion gas (49) suction injection injection propulsion output increase 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) ) More simple injection engine (88f) receives cheap liquid oxygen (5K) fuel injection combustion + compressed air fuel injection combustion into two types of theoretical combustion chamber (4Q), one type inlet / outlet valve (1Q) oxygen injection nozzle (6L) Various energy storage cycle coalescence engine and coalescence method provided with 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) ) Easy water injection engine (88e) with low cost liquid oxygen (5K) received fuel injection combustion + fuel injection combustion into compressed air 2 types of theoretical combustion chamber (4Q) 1 type inlet and outlet valve (1Q) oxygen injection Various energy storage cycle coalescence engine and coalescence method for closing a nozzle (6L), a fuel injection nozzle (6X), and an on-off 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) ) Easier gas engine (88d) receives cheap liquid oxygen (5K) Fuel injection combustion + compressed air fuel injection combustion into two types of theoretical combustion chamber (4Q) One type inlet and outlet valve (1Q) oxygen injection nozzle (6L) Fuel injection nozzle (6X) Open / close valve (1Q) Closed oxygen fuel injection Combining 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) ) More simple injection engine (88f) receives cheap liquid oxygen (5K) fuel injection combustion + compressed air fuel injection combustion into two types of theoretical combustion chamber (4Q), one type inlet / 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) Various energy storage cycle coalescence engines and coalescence methods for injecting the outer periphery (6Y).   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) ) Simpler water injection engine (88e) Receiving low-priced liquid oxygen (5K) fuel injection combustion + compressed air into two types of theoretical combustion chamber (4Q) and one type inlet / outlet valve (1Q) oxygen injection nozzle (6L) Fuel injection nozzle (6X) Equipped with open / close valve (1Q) Closed oxygen fuel injection combustion High pressure high temperature combustion gas (5M) Outer periphery (6Y) Injected superheated steam (50) also outer periphery (6A) Various energy conservation 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) ) Simpler injection engine (88f) Low cost liquid oxygen (5K) received fuel injection combustion + fuel injection combustion into compressed air 2 types of theoretical combustion chamber (4Q) 1 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 increase in outer periphery (6A) Rocket injection injection propulsion output 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) ) Simpler water injection engine (88e) Receiving low-priced liquid oxygen (5K) fuel injection combustion + compressed air into two types of theoretical combustion chamber (4Q) and one type inlet / 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) rocket injection and forward Various energy storage cycle coalescing engine and coalescence method for increasing water suction / 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) Series rotation gear (4D) Electric drive solar heater (21) + simple multistage compressor (3t) + liquid oxygen generator (88g) Various energy storage cycle coalescence engines and coalescence methods.   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) In-line rotating gear (4D) Various types of electric drive solar heater (21) + simple multi-stage compressor (3t) + liquid oxygen production machine (88g) generated by multiple turbines Energy conservation cycle coalescence engine and coalescence method.   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 Various energy storage cycle coalesced engines with rotating shaft (16A), cylindrical turbine blade group (8A), multi-generation electric drive solar heater (21) + simple multistage compressor (3t) + liquid oxygen production machine (88g) And coalescing method.   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 Combined with various energy conservation cycles to rotate shaft (16A) into cylindrical turbine blade group (8A) 20 power generation electric drive solar heater (21) + simple multistage compressor (3t) + liquid oxygen production machine (88g) Organization and coalescence method.   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 Combined with various energy conservation cycles to rotate the shaft (16A) into a cylindrical turbine blade group (8A) 40 sets of electric drive solar heater (21) + simple multistage compressor (3t) + liquid oxygen production machine (88g) Organization and coalescence method.   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 Combined with various energy conservation cycles to rotate shaft (16A) into cylindrical turbine blade group (8A) 80 sets of electric drive solar heater (21) + simple multistage compressor (3t) + liquid oxygen production machine (88g) Organization and coalescence method.   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 Combined with various energy conservation cycles to rotate shaft (16A) into cylindrical turbine blade group (8A) 100 power generation electric drive solar heater (21) + simple multistage compressor (3t) + liquid oxygen production machine (88g) Organization and coalescence method.   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 Combined with various energy storage cycles to rotate shaft (16A) into cylindrical turbine blade group (8A) 150 power generation electric drive solar heater (21) + simple multistage compressor (3t) + liquid oxygen production machine (88g) Organization and coalescence method.   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 Combined with various energy storage cycles to rotate shaft (16A) into cylindrical turbine blade group (8A) 200 sets of electric drive solar heater (21) + simple multistage compressor (3t) + liquid oxygen production machine (88g) Organization and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) power generation electric product + rocket combustion + jet combustion with a magnetic bearing load of 0 approach + super high speed circumferential speed, etc. Various energy storage cycle coalescence engines and coalescence methods.   Horizontally moving blade ratio critical material gravity turbine (8U) power generation electrical product + two rocket combustion + two jet combustion two-point center support simple water injection engine (88e) ) Various energy storage cycle coalescence engines and coalescence methods that are driven equally.   Horizontally moving blade ratio critical material gravity turbine (8U) power generation electrical product + three rocket combustion + three jet combustion three-point centrally supported simple water injection engine (88e) ) Various energy storage cycle coalescence engines and coalescence methods that are driven equally.   Horizontally-moving blade ratio critical material gravity turbine (8U) power generation electric product + 4 rocket combustion + 4 jet combustion 4 locations centered simple water injection engine (88e) ) Various energy storage cycle coalescence engines and coalescence methods that are driven equally.   Horizontally-moving blade ratio critical material gravity turbine (8U) power generation electrical product + 5 rocket combustion + 5 jet combustion 5 locations on both sides centered simple water injection engine (88e) ) Various energy storage cycle coalescence engines and coalescence methods that are driven equally.   Horizontally moving blade ratio critical material gravity turbine (8U) power generation electric product + 6 rocket combustion + 6 jet combustion 6 locations on both sides centered simple water injection engine (88e) ) Various energy storage cycle coalescence engines and coalescence methods that are driven equally.   Horizontally-moving blade ratio critical material gravity turbine (8U) power generation electrical product + rocket combustion + jet combustion with both sides center supported simple injection engine (88f) driven by magnetic bearing load 0 approach + super high speed circumferential speed Storage cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) power generation electrical product + 2 rocket combustion + 2 jet combustion 2 locations center support simple injection engine (88f) Various energy storage cycle coalescence engines and coalescence methods to be driven.   Horizontal full-blade ratio critical material gravity turbine (8U) power generation electrical product + three rocket combustion + three jet combustion three-point central support simple injection engine (88f) Various energy storage cycle coalescence engines and coalescence methods to be driven.   Horizontally-moving blade ratio critical material gravity turbine (8U) power generation electric product + 4 rocket combustion + 4 jet combustion 4 places center support simple injection engine (88f) Various energy storage cycle coalescence engines and coalescence methods to be driven.   Horizontally-moving blade ratio critical material gravity turbine (8U) power generation electrical product + 5 rocket combustion + 5 jet combustion 5 points centered simple injection engine (88f) Various energy storage cycle coalescence engines and coalescence methods to be driven.   Horizontally moving blade ratio critical material gravity turbine (8U) power generation electric product + 6 rocket combustion + 6 jet combustion 6 locations on both sides centered simple injection engine (88f) Various energy storage cycle coalescence engines and coalescence methods to be driven.   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 coalescing engine and coalescence method in which a simple water injection engine (88e) or other driven simple water injection engine ship (7g) is used to inject the maximum amount of bubbles into the bottom vertical parallel plate (9Q).   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 for making a simple water injection engine (88e) driven screw injection ship and injecting the maximum amount of bubbles into the bottom vertical parallel plate (9Q).   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 a simple water injection engine (88e), etc. drive simple water injection engine ship (7g) wide and have a bottom vertical parallel plate (9Q) wide to maximize the amount of air floating.   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 a simple water injection engine (88e) driven screw injection ship wide and have a bottom vertical parallel plate (9Q) wide to maximize the amount of air floating.   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 a simple water injection engine (88e), etc. drive simple water injection engine ship (7g) wide and have a bottom vertical parallel plate (9Q) wide to maximize friction reduction.   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 coalescing engines and coalescence methods that make a simple water-injection engine (88e) driven screw-injected ship wide and have a bottom vertical parallel plate (9Q) wide to 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 conservation cycle coalescing engine and coalescence method for simple injection engine (88f) rotary blade injection airplane (7j) with propulsion + both center support counter-rotating compressed air (28a) combustion.   Horizontal all-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 counter-rotating compression Various energy storage cycle coalescing engine and coalescence method to make a simple injection engine (88f) rotary blade injection airplane (7j) with 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) multiple ultra high pressure fuel combustion propulsion + both sides center support two Various energy storage cycle coalescing engine and coalescence method to make a simple injection engine (88f) rotary blade injection airplane (7j) with heavy inverted 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 Various energy storage cycle coalescence engine and coalescence method to make a simple injection engine (88f) rotary blade injection airplane (7j) with multiple super high pressure fuel combustion injection propulsion + both center support counter-rotating compressed air (28a) combustion.   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 Various energy conservation cycle coalescing engine and coalescence method for a simple injection engine (88f) rotary blade injection airplane (7j) with center-supporting counter-rotating compressed air (28a) combustion.   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 conservation cycle coalescing engine and coalescence method for simple injection engine (88f) rotary blade injection airplane (7j) with propulsion + both center support counter-rotating 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 Various energy storage cycle coalescence engine and coalescence method driven by simple injection engine (88f) rotary blade injection airplane (7j) with multiple ultra-high pressure fuel combustion injection propulsion + both center support contra-rotating compressed air (28a) combustion.   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 Various energy storage cycle coalescing engine and coalescence method for driving a simple injection engine (88f) rotary blade injection airplane (7j) with center-supporting counter-rotating compressed air (28a) combustion.   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 A simple injection engine (88f) rotating blade injection airplane (7j) driven by propulsion + both center support counter-rotating compressed air (28a) and various energy storage cycle coalescence engines and coalescence methods.   Horizontal all-blade ratio critical material gravity turbine (8U) generation of electric power generation, receiving liquid oxygen (5K) and making the compression volume 21/60000 of air compression multiple theoretical combustion chambers (4Q) + both sides center support Various energy storage cycle coalescence engines and coalescence methods for driving a simple injection engine (88f) rotary blade injection airplane (7j) with heavy inversion 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 Various energy storage cycle coalescing engine and coalescence method for driving a simple gas engine (88d) rotorcraft (7i) as center supported counter-rotating compressed air (28a) combustion.   Horizontal full-blade ratio critical material gravity turbine (8U) power generation electricity production, liquid oxygen (5K) + electricity received, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support counter-rotating compressed air (28a ) Various energy storage cycle coalescence engine and coalescence method for driving a simple gas engine (88d) rotor blade airplane (7i) as combustion.   Horizontal all-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double-side center support counter-rotating compression Various energy storage cycle coalescence engine and coalescence method for driving a simple gas engine (88d) rotor blade airplane (7i) as air (28a) combustion.   Theoretical combustion chamber (4Q) with high pressure fuel combustion + both sides receiving liquid oxygen (5K) and making compression volume 21/60000 Various energy storage cycle coalescence engines and coalescence methods in which a simple gas engine (88d) 1 to multiple drives are driven as a center support counter-rotating compressed air (28a) combustion to drive a rotary wing airplane (7i).   Horizontal full-blade ratio critical material gravity turbine (8U) power generation electricity production, liquid oxygen (5K) + electricity received, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support counter-rotating compressed air (28a ) Various energy storage cycle coalescing engines and coalescence methods for driving a simple gas engine (88d) 1 to plural and driving a rotary wing airplane (7i) as combustion.   Horizontal all-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double-side center support counter-rotating compression Various energy storage cycle coalescing engine and coalescence method for driving a simple air engine (88d) 1 to a plurality of air (28a) combustion to drive a rotary wing airplane (7i).   Theoretical combustion chamber (4Q) with high pressure fuel combustion + both sides receiving liquid oxygen (5K) and making compression volume 21/60000 Various energy storage cycle coalescence engines and coalescence methods in which a simple gas engine (88d) 1 to multiple drives are driven as a center support counter-rotating compressed air (28a) combustion to drive a rotary wing airplane (7i).   Horizontal full-blade ratio critical material gravity turbine (8U) power generation electricity production, liquid oxygen (5K) + electricity received, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support counter-rotating compressed air (28a ) Various energy storage cycle coalescing engines and coalescence methods for driving a simple gas engine (88d) 1 to plural and driving a rotary wing airplane (7i) as combustion.   Horizontal all-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double-side center support counter-rotating compression Various energy storage cycle coalescing engine and coalescence method for driving a simple air engine (88d) 1 to a plurality of air (28a) combustion to drive a rotary wing airplane (7i).   Theoretical combustion chamber (4Q) with high pressure fuel combustion + both sides receiving liquid oxygen (5K) and making compression volume 21/60000 Various energy storage cycle coalescence engines and coalescence methods in which a simple gas engine (88d) is driven as a center support counter-rotating compressed air (28a) combustion to drive a rotary wing airplane (7i).   Theoretical combustion chamber (4Q) with high pressure fuel combustion + both sides receiving liquid oxygen (5K) and making compression volume 21/60000 Various energy storage cycle coalescence engines and coalescence methods for rotating a simple air engine (88d) driven rotor blade (7B) and driving a rotor blade airplane (7i) as center support counter-rotating compressed air (28a) combustion.   Horizontal full-blade ratio critical material gravity turbine (8U) power generation electricity production, liquid oxygen (5K) + electricity received, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support counter-rotating compressed air (28a ) Various energy storage cycle coalescence engine and coalescence method for driving a simple gas engine (88d) driven rotor blade (7B) as a combustion and rotating the rotor blade airplane (7i).   Horizontal all-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double-side center support counter-rotating compression Various energy storage cycle coalescence engines and coalescence methods for rotating a simple air engine (88d) driven rotor blade (7B) and driving a rotor blade airplane (7i) as air (28a) combustion.   Theoretical combustion chamber (4Q) with high pressure fuel combustion + both sides receiving liquid oxygen (5K) and making compression volume 21/60000 Various energy storage cycle coalescence engine and coalescence method for driving a rotary blade airplane (7i) by rotating a simple gas engine (88d) 1 to multiple drive rotor blades (7B) multiple times as center support counter-rotating compressed air (28a) combustion.   Horizontal full-blade ratio critical material gravity turbine (8U) power generation electricity production, liquid oxygen (5K) + electricity received, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support counter-rotating compressed air (28a ) Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88d) 1 to multiple drive rotor blades (7B) as a combustion and rotating the rotor blade airplane (7i).   Horizontal all-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double-side center support counter-rotating compression Various energy storage cycle coalescing engine and coalescence method for driving a rotary blade airplane (7i) by rotating a simple gas engine (88d) 1 to a plurality of driving rotor blades (7B) as air (28a) combustion.   Theoretical combustion chamber (4Q) with high pressure fuel combustion + both sides receiving liquid oxygen (5K) and making compression volume 21/60000 Various energy storage cycle coalescence engine and coalescence method for driving a rotary blade airplane (7i) by rotating a simple gas engine (88d) 1 to multiple drive rotor blades (7B) multiple times as center support counter-rotating compressed air (28a) combustion.   Horizontal full-blade ratio critical material gravity turbine (8U) power generation electricity production, liquid oxygen (5K) + electricity received, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support counter-rotating compressed air (28a ) Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88d) 1 to multiple drive rotor blades (7B) as a combustion and rotating the rotor blade airplane (7i).   Horizontal all-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double-side center support counter-rotating compression Various energy storage cycle coalescing engine and coalescence method for driving a rotary blade airplane (7i) by rotating a simple gas engine (88d) 1 to a plurality of driving rotor blades (7B) as air (28a) combustion.   Theoretical combustion chamber (4Q) with high pressure fuel combustion + both sides receiving liquid oxygen (5K) and making compression volume 21/60000 Various energy storage cycle coalescence engines and coalescence methods for rotating a simple air engine (88d) driven rotor blade (7B) and driving a rotor blade airplane (7i) as center support counter-rotating 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 Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88d) driven simple injection engine (88f) as center support counter-rotating compressed air (28a) combustion.   Horizontal full-blade ratio critical material gravity turbine (8U) power generation electricity production, liquid oxygen (5K) + electricity received, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support counter-rotating compressed air (28a ) Various energy storage cycle coalescing engine and coalescence method for driving a simple gas engine (88d) driving a simple injection engine (88f) as combustion.   Horizontal all-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double-side center support counter-rotating compression Various energy storage cycle coalescence engine and coalescence method for driving a simple gas engine (88d) driven simple injection engine (88f) as air (28a) combustion.   Theoretical combustion chamber (4Q) with high pressure fuel combustion + both sides receiving liquid oxygen (5K) and making compression volume 21/60000 Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88d) 1 to a multiple drive simple injection engine (88f) as center support counter-rotating compressed air (28a) combustion.   Horizontal full-blade ratio critical material gravity turbine (8U) power generation electricity production, liquid oxygen (5K) + electricity received, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support counter-rotating compressed air (28a ) Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88d) 1 to a multiple drive simple injection engine (88f) as combustion.   Horizontal all-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double-side center support counter-rotating compression Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88d) 1 to a multiple drive simple injection engine (88f) as air (28a) combustion.   Theoretical combustion chamber (4Q) with high pressure fuel combustion + both sides receiving liquid oxygen (5K) and making compression volume 21/60000 Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88d) 1 to a multiple drive simple injection engine (88f) as center support counter-rotating compressed air (28a) combustion.   Horizontal full-blade ratio critical material gravity turbine (8U) power generation electricity production, liquid oxygen (5K) + electricity received, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support counter-rotating compressed air (28a ) Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88d) 1 to a multiple drive simple injection engine (88f) as combustion.   Horizontal all-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double-side center support counter-rotating compression Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88d) 1 to a multiple drive simple injection engine (88f) as air (28a) combustion.   Theoretical combustion chamber (4Q) with high pressure fuel combustion + both sides receiving liquid oxygen (5K) and making compression volume 21/60000 A simple gas engine (88d) driven simple injection engine (88f) as a center support counter-rotating compressed air (28a) combustion, and various energy storage cycle coalescing engines and coalescence methods.