JP2014043847A - Various energy storage cycle jointing engine - Google Patents

Abstract

PROBLEM TO BE SOLVED: To solve a problem that power generation of an existing steam turbine whose half of stationary blades has a 0-output is almost 0-output power generation in which a steam velocity is reduced to 1/10 and a maximum velocity part water has a capacity 43000 times larger by blocking the steam velocity.SOLUTION: A half of stationary blades have a 0-output, so as to block a light-weight steam velocity and the like. Then, a power generation amount is improved to 1/10 or less at light object power generation, so as to double-reverse all of moving blades by a gear with a transverse axis 1h. Power is generated at, for example, mercury gravity acceleration under vacuum of 30 mmHg, so as to reach Mach 30. One hundred sets of mercury injection turbines are overlaid, and the power generation amount of one turbine is 1355 times as large as that of the existing one, so as to obtain a bearing load of 0. An inexpensive electric-driven solar power heater with fuel consumption of 0 and power initial cost of 1/100 is manufactured, so as to provide heat supply facility 3D of electricity, liquid-air, and overheated steam. An automobile, a ship, an aircraft and the like are compression-driven by liquid oxygen, so as to provide 21/60000 capacity compression power of that of air compression, 1/10 fuel consumption, and 10 times velocity. The aircraft is targeted to 1/500000 costs for reaching a cosmic space, so as to make a profit ratio for operating all of products extraordinarily best in the world and permanent like a one-day round trip everywhere 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 Aiming at the amount of power generation, as a power generation that requires zero fuel cost experiments for boilers and nuclear reactors, the horizontal all blade specific material gravity turbine 8U power generation electric drive and electric product drive A simple multistage compressor 3f + liquid oxygen producing machine 88h, a simple gas engine 88i, a simple water injection engine 88j, a simple injection engine 88k, etc., which are close to the center support bearing load of both sides, are connected to a simple multistage compressor 3f, etc. The heat of the vessel 21 is heated to a high compression temperature to produce various heat such as heat recovery liquid oxygen, etc., and divided and stored into 24-200 MPa superheated steam 50 hot water + liquid air 28a cold heat, as electricity + liquid air cold heat + superheated steam heat supply equipment 3D , Various heat use + liquid use for infinite applications, ships, vehicles, airplanes, etc. For example, ships, vehicles, airplanes, etc. receive liquid oxygen and the compression volume work rate is 21/60000 volume work of air compression And the rotational pressure of the simple gas engine 88i, the combined injection of the simple injection engine 88k and the simple water injection engine 88j are facilitated by reducing the compression pressure of liquid oxygen or water by 20 times. Promote unification of ships, speed up natural phenomena 2a Supply nitrogen, oxygen and CO2 to seawater Increase microorganisms and seaweeds, greatly increase human food such as fish in food chains, etc. The present invention relates to technologies for various energy conservation cycle coalescence engines and various energy conservation coalescence methods, aiming at space exploration 1/10, fuel cost 1/10 and 1 / 500,000, and space and aircraft and ships aiming at 10 times speed.

  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 of the high-pressure high-temperature water heating pipe 5H is heated by high-temperature combustion, and the research on ultra-high speed counter-rotation is performed with zero liquid oxygen and close to both-side center support bearing load including the drive of the simple gas engine 88i, etc. The combustion gas 49 is sucked and injected from the superheated steam rocket nozzle 6A as super high pressure combustion gas 49 + superheated steam 50 in the theoretical combustion chamber 4Q, and the simple gas engine 88i is driven to drive various vehicles such as automobiles and tillers, and propellers. 7A, rotor blade 7B and screw 7C are driven, various vehicles, propeller airplanes and screw ships are driven, and the fuel cost is set to 1/10 or 10 times speed by using liquid oxygen 5K for electric power generation, The present invention relates to technologies of various energy conservation cycle coalescence engines and coalescence methods aiming at the best in the world in terms of operating profit rate.

  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 a liquid compression simple injection engine 88k injection propulsion aim, horizontal full blade ratio critical material gravity turbine 8U power generation electric drive multiple multistage simple multistage compressor 3f etc. heat pump 1G + solar heater 21 24 to 200 MPa high-temperature water to superheated steam temperature 50 + liquid air cold heat 28a is divided and stored. As electricity + liquid air cold heat + superheated steam temperature heat supply equipment 3D, the aircraft propulsion is liquid oxygen 5K + liquid fuel 1c + high-pressure high-temperature water 52a. The compressed volume work rate is received by liquid oxygen compression and compressed by ultra-high pressure at 21/60000 volume work rate of air compression. Fuel heating pipe 1L High pressure high temperature water heating pipe 5H Oxygen heating pipe 5F is set to the optimum heating temperature, and the fuel control valve 25b + oxygen control valve 24D + superheated steam control valve 25 not shown is opened. Then, the on-off valve 1Q closing theoretical combustion chamber 4Q aiming at one or more stoichiometric air-fuel ratio super high pressure combustion is injected and burned, and the oxygen recovery nozzle 6L and the fuel injection nozzle 6X multiple combustion, the superheated steam 50 as the heat recovery superheated steam rocket nozzle 6A injection + combustion gas injection nozzle 6Y injection, aiming for combined injection such as rocket injection and suction injection, etc., both sides center support bearing load 0 approach, high speed counter rotating compressed air 28a combustion additional combination, overheat in rocket outer box 77B Steam rocket nozzle 6A + Combustion gas injection nozzle 6Y 200MPa target rocket injection, aiming for space arrival cost 1 / 500,000 and aiming at near zero fuel cost Anywhere on Earth equal to 16 laps the earth in one day flight 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 contained, air compressor of liquid oxygen production machine 88h is also added to use simple multi-stage compressor 3f that is simple in theory, horizontal type full blade ratio material gravity turbine 8U power generation electric drive 1 to multi-stage simple As the heat pump 1G compression of the multistage compressor 3f, etc., the solar heater 21 solar heating air is compressed to high temperature, the high pressure high temperature water heating pipe 5H heat recovery is divided and stored, and 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 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 on the inner periphery of the simple water injection engine 88j theoretical combustion chamber 4Q, respectively. The simple water injection engine 88j and the simple gas engine 88i approaching zero load are driven to make the water suction injection propulsion of the simple water injection engine 88j and the screw 7C rotation propulsion of the simple gas engine 88i. 1/10 Fuel Cost Aiming for a screw propulsion simple gas engine 88i, the bottom of the ship is an exhaust injection propulsion, a natural phenomenon is accelerated in the process of the friction reduction injection propulsion, and oxygen, nitrogen, CO2 etc. are supplied into the sea Various phytoplankton, seaweeds, corals, fish, etc. Law relating to the technology.

  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 supply facility 3D, which is compressed and recovered multiple times by the heat pump 1G, etc., and is divided and stored in 24-200 MPa high-temperature water 52a-superheated steam temperature 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 a plurality of times by a fuel cost 0 power generation electric drive 1 to multiple-stage simple multistage compressor 3f + liquid oxygen production machine 88h. 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 have been 38 applications, including PCT, from the filing date of Japanese Patent Application No. 2012-175489 to August 8, 2012.

  In the existing thermal power plants in the world, the total heat generation is 7 degrees Celsius, and the seawater temperature rise is 1000 times in 100 years, and the downdrafts and updrafts are increased as much as possible. As the number of storms, torrential rains, heat waves, cold waves, etc. increases without limit, typhoons, seasonal winds, tornadoes, etc., around 100 years in the sea near Japan, salt water on the land due to concentrated heavy rains, etc. Covering increases the danger of human land food loss, making it impossible for the natural phenomenon of supplying nutrients to the sea-cooled seabed in winter, dramatically reducing microorganisms, phytoplankton, seaweeds, corals, etc., fish through food chains, etc. The number of human underwater foods has been reduced as much as 1/100, and droughts, torrential rains, typhoons and seasonal winds have increased 10 times in 100 years. For example, typhoons and seasonal winds have an upper limit such as 300m / sec. weather 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 type full blade ratio material gravity turbine 8U fuel cost 0 power generation cheap electric drive all, solar heater 21 + 1 to multistage both sides center support bearing load approach 0, simple multistage compressor 3f + liquid oxygen production machine 88h etc. As a facility for 3D, electricity + liquid air cooling + high temperature water to superheated steam temperature heat supply equipment, the received liquid oxygen 5K is compressed to 21/60000 volumetric compression work rate of air compression, ultra high pressure combustion or ultra high temperature combustion As the theoretical combustion chamber 4Q, which is easy to heat, the superheated steam 50 is heated so that the theoretical air-fuel ratio combustion becomes possible. The simple gas engine 88i, the simple water injection engine 88j, and the simple injection engine 88k are used to drive vehicles such as automobiles, ships and airplanes, and to drive the rotational force and propulsion and drive. In the propulsion drive, rapid levitation propulsion and natural phenomenon acceleration 2a are performed by short-time rocket injection, and oxygen, nitrogen, CO2 and the like are supplied into the sea to propagate microorganisms, phytoplankton, seaweeds, corals, fish, etc. Increasingly, airplanes will fly around the earth 16 times a day in the prime of space flight by short-time rocket injection, etc. Every day on the earth, aiming for day trips and a little CO2 exhaust in the atmosphere, 100% world-wide monopoly and top secret manufacturing As the top-secret power generation, ships, airplanes, automobiles, etc., making it the best in the world with outstanding profitability and the best in new employment, preventing droughts, torrential rains, typhoons, seasonal winds, heavy rains in seawater, and earthquake tsunamis 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 As a result of the increase in the super high pressure superheated steam 50 in the vicinity of the center of the theoretical combustion chamber 4Q, the simple gas engine 88i, the simple water injection engine 88j, and the simple injection that are close to the both-side center support bearing load by the theoretical combustion chamber 4Q. The engine 88k has the effect of being able to drive at ultra-high speed most efficiently, and in addition to the effect of aiming for a fuel cost of 1/10 or 10 times the speed of automobiles, ships and airplanes, the space arrival cost is reduced to 1 / 500,000 of existing space rockets. There is an effect that can be aimed at the expense, the wheel, the screw 7C, the propeller 7A and the rotor blade 7B are simply driven by the gas engine 88i, the ship, the airplane, the automobile, etc. are driven by the rotational force, and the ship is jetted. The propulsion drive speeds up natural phenomena 2a, and the effect of increasing the digestibility of underwater microorganisms, such as CO2, is tens of thousands of times that of forests, and so on. Greatly increase undersea food of human beings, prevent desertification, drought, torrential rain, typhoon, seasonal wind, earthquake tsunami, etc. There is a target effect.

Airplane drive receives liquid oxygen + high temperature water from electricity + liquid air cold heat + high temperature water to superheated steam temperature heat supply equipment 3D of fuel drive 0 horizontal type whole blade ratio critical material gravity turbine 8U power generation electric drive, theoretical combustion chamber Optimum heating of ultra-high pressure water, ultra-high pressure fuel, etc. with the high-temperature water heating pipe 5H etc. on the inner periphery of 4Q, open the fuel injection nozzle 6X + oxygen injection nozzle 6L, and mix injection ignition combustion near the center of multiple locations of oxygen gas + fuel gas As a theoretical combustion chamber 4Q that optimally heats the fuel + oxygen + high-temperature water heating pipe 5H in the inner periphery of the theoretical combustion chamber 4Q and superheats it to the super-high pressure high-temperature superheated steam 50 or the like, a plurality of theoretical combustion chambers 4Q of the existing technical improvement invention are provided. Driven by a simple injection engine 88k with close load on both sides of the center support bearings, which is greatly simplified, aiming for a space arrival cost of 1 / 500,000, compared with the existing space rocket, and the same fuel cost 10 times injection propulsion output so It has the effect of aiming to make the best use of the space. For example, the propulsion output is 100 times the pressure of existing jets, 10 times the calorie injection, and 1000 times the injection propulsion output for a short time. Because the superheated steam injection speed and combustion gas injection speed are the highest in vacuum, the existing space rocket ground mass injection is considered the worst, and the high pressure high temperature combustion chamber 5M + high pressure high temperature of 24-200MPa from near the highest flight altitude of the existing aircraft There is an effect that the injection amount of the superheated steam 50 is increased and the earth is made 16 orbits a day, and the space utilization prime that enables a day trip anywhere on the earth can be aimed.

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 88h (Example 4) Explanatory drawing of the simple multistage compressor 3f (Example 5) Explanatory drawing of simple gas engine 88i (Example 6) Explanatory drawing of the simple water injection engine 88j (Example 7) Explanatory drawing of the simple injection engine 88k (Example 8) Illustration of simple gas locomotive 7k (Example 9) Illustration of a simple gas engine ship 7l (Example 10) Illustration of Simple Gas Engine Airplane 7m (Example 11) Explanatory drawing of the simple water injection engine ship 7n (Example 12) Explanatory drawing of simple injection engine airplane 7o (Example 13) Explanatory drawing of the rotary wing airplane 7p (Example 14) Explanatory drawing of the rotary wing jet airplane 7q (Example 15)

  The use of gravity acceleration power generation in a vacuum for a long period of time with brainwashing such as existing steam turbine power generation is blocked, and the target of 43,000 times the power generation amount of one existing steam turbine power generation is blocked by one unit of 100 sets, for example, the existing best steam turbine The power generation atmospheric pressure, the same speed, the same volumetric power, kg-heavy m / sec, are reduced to 1/1700 of the water power, and the stationary blades are arranged alternately with the moving blades to dam and close the rotation output to zero. The total amount of heat generated by the power generation increases by 7 degrees in the seawater temperature, the fishes drastically decrease, the bottom bedrock expands into earthquakes and tsunamis, and the typhoon, seasonal winds, and sea tornadoes in the sea near Japan are increased to about 100m / sec. There is a danger that the drought of humans will rapidly extinguish due to the provision of salt coating on the land in about 50 to 100 years, such as a heavy rain of suctioned seawater is expected over the sea. In other words, since the invention becomes too large due to many fatal defects of the existing technology, the invention is described in the explanation of the reference numerals, and the parts that have been repeatedly explained in the previous application are omitted, and other than the horizontal type full blade ratio material gravity turbine 8U The three types of examples are used as substitutes, and the use of existing technology such as magnetic bearings challenges the realization of the invention that omits common sense. , Simple multistage compressor 3f + liquid oxygen production machine 88h, simple gas engine 88i, simple water injection engine 88j and simple injection engine 88k driven cars, ships and airplanes.

Figure 1 Gravity acceleration in vacuum + mercury injection speed Mach 30 drive, etc., aiming to the limit, horizontal type blade blade critical material gravity turbine 8U power generation is proportional to kg weight m / second, so both sides of cylindrical turbine blade group 8A And repulsive permanent magnets 9B attracting permanent magnets 9C at a plurality of locations such as the center, and the cylindrical turbine blade group 8A side as a ring type inner periphery 1 pole outer periphery 1 pole magnetization, and the turbine outer box 77a side as a ring type inner periphery 2 poles The upper attraction permanent magnet 9C is the lower repulsion permanent magnet 9B, and the weight of the rotating part is made close to 0 by the repulsive force and the attraction force at multiple locations, the bearing load is made close to 0, and the aim is to update the super high speed turbine peripheral speed record. Medium mercury gravity acceleration Mach 30 Turbine driving approach aiming, horizontal axis 16A with horizontal shaft plate 16 aiming at infinite increase of fixed rotation speed and rotation outer diameter, one type is manufactured 2 sets 1 set 100 sets in series Movement As a manufacture of flywheel turbines, or as one set, 200 series full-blade flywheel turbines and bite-in series full-blade flywheel turbines, each with 100-200 sets vertically by fully automatic casting, fully automatic processing, etc. One unit is manufactured, and 100 units, etc. are installed in the existing highest building height of vertical 828m, and one unit is provided. For example, the mercury 3E platinum ball 2E is vertically increased by 50 to 828m etc. by the specific material rising device 2F. The platinum sphere 2E is mixed and injected with the mercury 3E pressure by the specific material accelerator 6W to aim at the Mach 28 injection, and the gravitational acceleration acceleration vacuum acceleration drive is performed, and the cylindrical turbine blade group 8A is rotated counterclockwise by the countersynchronous gear 4C. The gravity acceleration part 1g that makes 100 sets of the same speed and the same direction and the same direction and the same rotation in the same direction and the same rotational speed 4D, facilitates mass production inexpensively, eliminates the need for a boiler and a reactor, and accelerates mercury etc. in a vacuum. The generator 1 is provided for each of the upper synchronous gear 4C main shaft and the series co-rotating gear 4D main shaft, and the generator power generation cost is targeted for 1/10 out of the turbine outer box 77a. Extremely simple and extremely inexpensive electric products and electric drive infinity, and the world's best energy conservation cycle combined engine power generation and combined method power generation with outstanding profitability.

The horizontal full-blade 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 form a long cylinder such as a cylinder, a long long lens 2d is a joint 80A + fastener 80B, and a sealed upper portion is a 4H external air passage 28A. Intake and compression as 1 to multi-stage heat pump 1G for suction, simple multi-stage compressor 3f 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 88h, which has a bearing load close to 0 by the attracting repulsive magnet 9b on both sides of the center support in FIG. As a 9M assembly of simple annular parts, fully automatic mass production, fully automatic processing, easy assembly, aiming at 1/100 parts count, simple multistage compressor 3f connection aim, horizontal full blade ratio significant material gravity Turbine 8U fuel cost 0 power generation Extremely inexpensive electric drive, in the case of multi-stage compression, simple multi-stage compressor 3f and coupled drive compression, in the case of single-stage compression, heat production heating air 28a of solar heater 21 is compressed heat Recovered, water heated isothermal production + rectification tower exhaust pipe 5h cooling to prepare liquid oxygen + liquid nitrogen production, ultra high pressure compressed air 28a to air turbine 3u, ultra high speed injection counter-rotating drive, bearing load Large of 0 approaching super high speed rotation By generating a rotating output, exhaust gas is supplied to the rectification tower as a significant reduction in motor drive power, and purified to liquid oxygen + liquid nitrogen, etc., as in the existing technology, and the exhaust gas is supplied to the rectification tower exhaust pipe 5h. Then, the liquid oxygen production machine 88h is driven continuously into mass production of heat + cold and supplied to the supply equipment 3D of electricity + liquid air cold + hot water to superheated steam heat, for example, in the heat supply under the seabed or permafrost land Recover methane injected into the methane hydrate, recover methane under permafrost land from the top of the top using a transparent enclosure, and use the specific gravity difference. Aiming at the prime use of various types of thermal energy, the simple gas engine 88i drive, the simple water injection engine 88j drive, and the simple injection are combined with the liquid oxygen supply, which is combined with the air compression 21/60000 volume liquid oxygen drive. With engine 88k drive, various rotational drives such as car drive, ship drive and airplane drive, and ultra-high speed jet propulsion drive, in the case of airplane drive, the space arrival cost is aimed at 1 / 500,000, making it possible to aim for a day trip anywhere on earth. A liquid oxygen producing machine 88h is used.

The simple multi-stage compressor 3f, which has a bearing load close to zero by the attracting repulsive magnet 9b on both sides of the center support in FIG. 9M assembly, fully automatic mass production, fully automated processing, easy assembly, 1/100 parts count, vertical full blade hydrogravity turbine 8P fuel cost 0 power generation extremely cheap electric drive In the case of multi-stage compression, it is connected and compressed with a liquid oxygen production machine 88h, etc., and the solar heater 21 repeats air compression heat recovery such as heated air 28a one or more times to produce superheated steam 50 temperature heat such as water heating. + Compressed air 28a cold production is repeated one or more times to make mass production of ultra high pressure superheated steam 50 warm heat + ultrahigh pressure compressed air 28a cold heat, aiming at 1/10 production cost target of existing liquid oxygen production cost, etc. Inner shaft device 60 Both sides center support bearing load close to 0, enabling large and large ultra high speed counter rotating compressor and micro ultra high speed counter rotating compressor to make simple multistage compressor 3f that can handle all conditions, and counter rotating during assembly The outer casing 77C is divided into two parts at the horizontal shaft 1h, and the counter rotating gear device 85Y is first assembled, so that the outer compression blade 8m outlet blade of the outer shaft device 60B60B and the inlet blade + inner shaft device 60A60A inner compression blade 8k outlet blades and inlet blades are assembled, and one to a plurality of inner compression blades 8k intermediate blades intermediate blades + outer compression blades 8m intermediate blades intermediate blades are assembled into assembly parts 9M, and each inner compression blade 8k inlet is assembled. Assemble the blade outlet blade + outer compression blade 8m inlet blade outlet blade into the fitting assembly 9M, assemble the compressor outer box 77b77b into the counter-rotating machine outer box 77C and assemble the fitting assembly 9M into the compressor outer box 77b. Next reverse box 77 The assembly assembly 9M is assembled into the simple two-stage compressor 3t, and the assembly assembly section 9M is assembled and connected one after another to form a simple multistage compressor 3f having one or more stages that repeats the provision of the simple compressor 3s. Oxygen production machine 88h Connected drive, etc. Horizontal axis 1h Double reversal drive simple multistage compressor 3f.

The simple gas engine 88i, in which the bearing load is close to zero by the attracting repulsive magnet 9b on both sides of the center support in FIG. As a 9M assembly of annular parts, fully automatic mass production, fully automatic processing, easy assembly, aiming at 1/100 parts count, simple multistage compressor 3f connection aim, horizontal type full blade ratio material gravity turbine 8U fuel cost 0 power generation Extremely cheap electricity production Electricity + liquid air cold heat + hot water to superheated steam heat supply facility 3D Receives liquid oxygen + electricity + hot water to the theoretical combustion chamber 4Q, etc. driven by cheap electricity products Then, by compressing liquid oxygen, the compression volume work rate is 21/60000 volume compression work rate of air compression, liquid oxygen + liquid fuel + high temperature water is compressed to ultrahigh pressure such as 24-200 MPa, high pressure high temperature water heating With tube 5H etc. Heated and closed two types of on-off valves 1Q, the rocket combustion theoretical combustion chamber 4Q is heated to an optimal temperature from the oxygen injection nozzle 6L + fuel injection nozzle 6X, oxygen + fuel injection combustion is performed, and the inner wall of the theoretical combustion chamber 4Q The fuel + 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 aims at a 10 times pressure 10 times combustion amount of the high pressure high temperature combustion chamber 5M, and the existing technology improved theoretical combustion chamber 4Q Then, 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 rocket nozzle 6A, and the high-pressure high-temperature combustion chamber 5M having a fourfold combustion amount is formed by the rocket injection. As a simple gas engine 88i with suction injection and greatly improved existing gas turbine, the compression work rate is 21/60000 volumetric compression work rate of air compression, liquid oxygen drive theory And baked chamber 4Q plurality of coalesced, and simple gas engine 88i to use any liquid oxygen 0.

The case of driving the simple gas engine 88i in the liquid oxygen 0 existing technology improved theoretical combustion chamber 4Q will be described. The existing jet engine and the stationary blade of the gas turbine are almost completely abolished, and the counter rotating magnetic device 85 to the counter rotating gear device 85Y. Thus, the inner shaft device 60A + outer shaft device 60B approaching zero on both side center support bearing loads is double-reversed and the air 28a sucked from the inlet stationary blade 6G is linearly compressed by the inner compression blade 8k + outer compression blade 8m. Double reversal linear ultra-high-speed expansion, high output, compression 800-1200 ° C rise process, linear compression simple multistage compressor 3f connected, and relative speeds as easy as twice the target of existing gas turbines, etc. Ultra high pressure, compressed air injection from the compressed air injection stationary vane 6G of the contra-rotating machine outer box 77C to the theoretical combustion chamber 4Q, fuel injection combustion from the fuel injection nozzle 6X, high pressure high temperature water heating By making the superheated steam 50 such as heat recovery 200 MPa at 5H into the production theoretical air-fuel ratio combustion, the same compressed air amount as the quadruple fuel combustion amount of the existing gas turbine or the like, more than 3/4 heat amount of the combustion gas 49 or 20 times pressure The superheated steam 50 or the like is rocket-injected, and the inner output blade 8n + the outer output blade 8p is driven in reverse with the combustion gas 49, and the same compressed air amount is increased by 10 times the propulsion output of the existing jet engine or gas turbine. Aiming for double-rotation output, the horizontal shaft 1h or outer shaft device or inner shaft device 60A is extended to rotate and drive generators, cars, ships and airplanes, and airplanes and ships are injected with exhaust In addition to the propulsion drive, particularly in the case of power generation, the entire exhaust gas of the simple gas engine 88i is recovered by the heat exchange heating air 28a, and the high temperature water 52b of the compressed water injection heat recovery is recovered by the inner compression blade 8k + the outer compression blade 8m. Pressurized into the pressurized high-temperature water heating pipe 5H, the air 28a generates power repeatedly repeating fuel injection and combustion in the theoretical combustion chamber 4Q, and further increases the power generation amount by the combined high-temperature air 28a heating of the solar heater 21 in FIG. Similarly, the geothermal heat is also converted into the temperature of the air 28a and compressed by suction compressed water injection, and similarly, the simple gas engine 88i with an increased power generation amount is obtained.

The simple water injection engine 88j, which has a bearing load close to 0 by the attracting repulsive magnet 9b on both sides of the center support in FIG. As a 9M assembly of simple annular parts, fully automatic mass production, fully automatic processing, easy assembly, aiming at 1/100 parts count, simple multistage compressor 3f connection aim, horizontal full blade ratio significant material gravity Turbine 8U Fuel cost 0 Power generation Extremely inexpensive electricity production Electricity + liquid air cold heat + high temperature water ~ superheated steam temperature heat supply equipment 3D, liquid oxygen + electricity + high temperature water is supplied to the theoretical combustion chamber 4Q etc. driven by cheap electric products By receiving and compressing liquid oxygen, the compression volume work rate is 21/60000 volume compression work rate of air compression, liquid oxygen + liquid fuel + high temperature water is compressed to ultra high pressure such as 24-200 MPa, high pressure high temperature water Heating tube 5H etc. Heating and closing the multiple inlet / outlet on-off valves 1Q in the rocket combustion theoretical combustion chamber 4Q, oxygen + fuel injection combustion heated to an optimal temperature from the oxygen injection nozzle 6L + fuel injection nozzle 6X, theoretical combustion chamber Fuel + oxygen + superheated steam 50 is heated to the optimum temperature on the 4Q inner wall, and the theoretical air-fuel ratio combustion is performed, aiming at 10 times the 10-fold combustion amount of the existing technological improved theoretical combustion chamber 4Q high pressure high temperature combustion chamber 5M, the outer periphery of the theoretical combustion chamber 4Q From the superheated steam rocket nozzle 6A + combustion gas injection nozzle 6Y of the air 28a suction flow, the superheated steam 50 and the high-pressure high-temperature combustion chamber 5M combustion gas 49 approaching 200 MPa are injected, and the air 28a is suction-injected and water is suction-injected. In the existing technology improved theoretical combustion chamber 4Q, as the theoretical air-fuel ratio combustion amount of the fuel four times that of the existing technology, the superheated steam 50 is manufactured aiming at 200 MPa with increased heat quantity. 7B superheated steam rocket nozzle 6A is injected, high-pressure high-temperature combustion chamber 5M combustion gas 49 generates rotational output, sucks and injects air 28a in front of the suction flow of outer air 28a and sucks and injects water 52a. As an improved simple water injection engine 88j, a simple water injection engine 88j that combines a plurality of liquid oxygen drive theoretical combustion chambers 4Q with a compression work rate of 21/60000 volumetric compression work addition of air compression and is used even with zero liquid oxygen is used. To do.

The case where the simple water injection engine 88j is driven in the liquid oxygen 0 existing technology improved theoretical combustion chamber 4Q will be described. The existing jet engine and the stationary blades of the gas turbine are almost completely abolished, and the counter rotating magnetic device 85 to the counter rotating gear device. By 85Y, the inner shaft device 60A + outer shaft device 60B approaching zero on both side center support bearing loads is double-reversed and the air 28a sucked from the inlet stationary blade 6G is linearly compressed by the inner compression blade 8k + outer compression blade 8m, Double reversal linear ultra-high speed expansion, high output, simple multi-stage compressor 3f connection, relative speed of existing gas turbines, etc., double compression air pressure more than double, etc., make ultra-high pressure easy, compression of counter reversing machine outer box 77C The compressed air 28a is injected into the theoretical combustion chamber 4Q from the air injection vane 6G, the fuel is injected and combusted from the fuel injection nozzle 6X, and the heat recovery superheated steam 50 is produced by the high-pressure high-temperature water heating pipe 5H. By calcination, the same compressed air amount as the existing gas turbine etc. 4 times the fuel combustion amount and the outer periphery as the rocket injection part, the overheated steam 50 of the combustion gas 49 more than 3/4 heat amount or 20 times pressure etc. 77B is injected, and the inner output vane 8n + outer output vane 8p is driven in reverse by the combustion gas 49 so that the same compressed air amount is aimed at 15 times propulsion output +5 times rotation output of existing jet engines and gas turbines. A simple water injection engine 88j is provided which has a suction injection cylinder only at the rear, increases the air suction injection amount with zero water resistance increase, and makes it an injection propulsion drive for ships that inject underwater.

The simple injection engine 88k, in which the bearing load is close to zero by the attracting repulsive magnet 9b on both sides of the center support in FIG. As a 9M assembly of simple annular parts, fully automatic mass production, fully automatic processing, easy assembly, aiming at 1/100 parts count, simple multistage compressor 3f connection aim, horizontal full blade ratio significant material gravity Turbine 8U Fuel cost 0 Power generation Extremely inexpensive electricity production Electricity + liquid air cold heat + high temperature water ~ superheated steam temperature heat supply equipment 3D, liquid oxygen + electricity + high temperature water is supplied to the theoretical combustion chamber 4Q etc. driven by cheap electric products By receiving and compressing liquid oxygen, the compression volume work rate is set to 21/60000 volume compression work rate of air compression, and liquid oxygen + liquid fuel + high temperature water is compressed and heated to an ultrahigh pressure such as 24-200 MPa, Multiple entrances and exits In the rocket combustion theoretical combustion chamber 4Q with two types of closed valves 1Q closed, oxygen + fuel injection combustion heated to the optimal temperature from the oxygen injection nozzle 6L + fuel injection nozzle 6X, fuel + oxygen + superheat on the inner wall of the theoretical combustion chamber 4Q The 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 the combustion amount, superheated steam rocket nozzle 6A + combustion gas injection in the rocket outer box 77B From the nozzle 6Y, superheated steam 50 or a high-pressure high-temperature combustion chamber 5M combustion gas 49 approaching 200 MPa is injected, and when the on-off valve 1Q is closed, the high-power rocket combustion space utilization prime etc. is used. As a result of suction injection, a plurality of theoretical combustion chambers 4Q are made into liquid oxygen-driven rocket combustion chambers and jet combustion chambers. As the stoichiometric air-fuel ratio combustion amount of the double fuel, the superheated steam 50 is produced aiming at 200 MPa with an increased heat quantity, injected from the rocket outer box 77B superheated steam rocket nozzle 6A, and rotational output is generated in the high-pressure and high-temperature combustion chamber 5M combustion gas 49, As a simple injection engine 88k that sucks and injects the air 28a and greatly improves the existing jet engine, a combination of a plurality of liquid oxygen drive theoretical combustion chambers 4Q and a simple injection engine 88k that uses even liquid oxygen 0 are used.

The case of the simple injection engine 88k driving in the liquid oxygen 0 existing technology improved theoretical combustion chamber 4Q will be explained. The existing jet engine and the stationary blade of the gas turbine are almost completely abolished, and the counter rotating magnetic device 85 to the counter rotating gear device 85Y. Thus, the inner shaft device 60A + outer shaft device 60B, which are supported at the center on both sides, is double-reversed and the air 28a sucked from the inlet stationary blade 6G is linearly compressed by the inner compression blade 8k + outer compression blade 8m. High-speed expansion and large output, simple multistage compressor 3f connection, and relative speed of existing gas turbines, etc., double the compressed air pressure more than twice, etc. make it an ultra-high pressure easily, and the stationary blade for compressed air injection of the contra-rotating machine outer box 77C From 6G, compressed air 28a is injected into the theoretical combustion chamber 4Q, fuel is injected and combusted from the fuel injection nozzle 6X, and the heat-recovered 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 same compressed air amount as the existing gas turbine, etc., the fuel combustion amount of 4 times or the outer periphery is used as the rocket injection part, and 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. The inner output blade 8n + outer output blade 8p is driven in reverse by the combustion gas 49, and the same compressed air amount is aimed at 15 times propulsion output +5 times rotation output of existing jet engines and gas turbines, and ships and airplanes that inject underwater The simple injection engine 88k is used for the injection propulsion drive.

The simple gas engine vehicle 7k in FIG. 9 is an improved invention of the existing micro gas turbine vehicle. The simple gas engine 88i can be selected from compressed air drive + fuel cost 0 power generation electric product selection drive. Large material gravity turbine 8U Fuel cost 0 Power generation Extremely inexpensive electricity production Electricity + Liquid air cold heat + High temperature water to superheated steam temperature heat supply equipment 3D, Low oxygen electric product driven theoretical combustion chamber 4Q etc. Liquid oxygen + electricity + By receiving high-temperature water and compressing liquid oxygen, the compression volume work rate is 21/60000 volume compression work rate of air compression, and liquid oxygen + liquid fuel + high-temperature water is compressed and heated to an ultrahigh pressure such as 24-200 MPa. Then, in the rocket combustion theoretical combustion chamber 4Q in which the on-off valves 1Q at the plurality of inlets are closed, the oxygen + fuel injection combustion heated to the optimum temperature from the oxygen injection nozzle 6L + fuel injection nozzle 6X is performed. Fuel + oxygen + superheated steam 50 is heated to the optimum temperature on the inner wall of the combustion chamber 4Q, and the theoretical air-fuel ratio combustion is performed to improve the existing technology. In the jet combustion theoretical combustion chamber 4Q, as the theoretical air-fuel ratio combustion amount of the quadruple fuel fourfold combustion amount of the existing technology, superheated steam 50 of 200 MPa or the like with an increased heat amount is injected from the production superheated steam rocket nozzle 6A, and 4 by rocket injection. High-pressure high-temperature combustion chamber 5M combustion gas 49 is sucked and injected for double combustion or 40-fold combustion, and the generator 1 is driven as a simple gas engine 88i, which is a greatly improved existing micro gas turbine, and the storage battery drive wheel 4J is driven to the storage battery 1A. However, a simple gas engine that can be used as a compressed air-driven power plant or power storage unit, combined with a plurality of liquid oxygen-driven theoretical combustion chambers 4Q, and also used with zero liquid oxygen And Dosha 7k.

The simple gas engine ship 7l in FIG. 10 is an improved invention of an existing gas turbine ship. The simple gas engine 88i can select a compressed air drive + a fuel cost 0 power generation electric product selection drive. Material Gravity Turbine 8U Fuel Cost 0 Power Generation Extremely Low Cost Electric Manufacturing Electricity + Liquid Air Cold Heat + High Temperature Water-Superheated Steam Heat Supply Facility 3D to Low Temperature Electric Product Driven Theoretical Combustion Chamber 4Q etc. Liquid Oxygen + Electricity + High Temperature By receiving water and compressing liquid oxygen, the compression volume work rate is set to 21/60000 volume compression work rate of air compression, and liquid oxygen + liquid fuel + hot water is compressed and heated to an ultrahigh pressure such as 24-200 MPa. Thus, in the rocket combustion theoretical combustion chamber 4Q in which the on-off valves 1Q of the plurality of inlets are closed, the oxygen + fuel injection heated to the optimum temperature from the oxygen injection nozzle 6L + fuel injection nozzle 6X is combusted, and the theoretical combustion chamber 4 Fuel + oxygen + superheated steam 50 is heated to the optimum temperature on the inner wall, 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, existing technology improved theoretical combustion chamber In 4Q, as the theoretical air-fuel ratio combustion amount of the quadruple fuel of the existing technology, the superheated steam 50 of 200 MPa or the like with an increased heat amount is injected from the production superheated steam rocket nozzle 6A, and the high pressure aiming at the four times combustion amount or 40 times combustion by the rocket injection. The high temperature combustion chamber 5M combustion gas 49 is sucked and injected, and as a simple gas engine ship 7l that greatly improves the existing gas turbine ship, the screw 7C drive exhaust is injected to the top bottom of the ship with the rotational output of the simple gas engine 88i. Liquid oxygen conserving drive that makes rapid levitation approach by rocket combustion that can output 10 times as much as the minimum loss, and reduce fuel loss by reducing friction loss extremely Theoretical combustion chamber 4Q plurality of coalesced, and simple gas engine vessels 7l used any liquid oxygen 0.

The simple gas engine airplane 7m in FIG. 11 is an improved invention of an existing jet aircraft. The simple gas engine 88i can be selected to be driven by compressed air + zero power generation electric product selection drive. 8U fuel cost 0 power generation Extremely cheap electricity production Electricity + liquid air cold heat + hot water to superheated steam heat supply facility 3D Receives liquid oxygen + electricity + hot water to the theoretical combustion chamber 4Q, etc. driven by cheap electricity products Then, by compressing liquid oxygen, the compression volume work rate is set to 21/60000 volume compression work rate of air compression, and liquid oxygen + liquid fuel + high temperature water is compressed and heated to an ultrahigh pressure such as 24-200 MPa. In the rocket combustion theoretical combustion chamber 4Q in which the on-off valve 1Q is closed, oxygen + fuel injection heated to an optimum temperature from the oxygen injection nozzle 6L + fuel injection nozzle 6X is combusted, and the inner wall of the theoretical combustion chamber 4Q Fuel / oxygen + 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 fourfold fuel amount 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 rocket nozzle 6A, and four times the combustion amount by exhaust injection or rocket injection As a simple gas engine airplane 7m, which is a simple gas engine airplane 7m that greatly improves the existing jet aircraft, the propeller 7A drive exhaust is injected backwards with the rotational output of the simple gas engine 88i. As a combination of multiple liquid oxygen-driven theoretical combustion chambers 4Q, aiming at rocket combustion aiming at 40 times output + jet combustion aiming at 4 times output for a short time, space arrival cost is 1 / 500,000 Well the simple gas engine airplane 7m to fly even liquid oxygen 0.

A simple water injection engine ship 7n in FIG. 12 is an improved invention of an existing gas turbine ship. The simple injection engine 88e can be selected to be driven by compressed air + zero fuel cost, and a power generation electrical product selection drive. Material Gravity Turbine 8U Fuel Cost 0 Power Generation Extremely Low Cost Electric Manufacturing Electricity + Liquid Air Cold Heat + High Temperature Water-Superheated Steam Heat Supply Facility 3D to Low Temperature Electric Product Driven Theoretical Combustion Chamber 4Q etc. Liquid Oxygen + Electricity + High Temperature By receiving water and compressing liquid oxygen, the compression volume work rate is set to 21/60000 volume compression work rate of air compression, and liquid oxygen + liquid fuel + hot water is compressed and heated to an ultrahigh pressure such as 24-200 MPa. Then, oxygen + fuel injection combustion heated to an optimum temperature from the oxygen injection nozzle 6L + fuel injection nozzle 6X in the rocket combustion theoretical combustion chamber 4Q with the multiple inlet / outlet opening / closing valves 1Q closed, and theoretical combustion Fuel + oxygen + superheated steam 50 is heated to the optimum temperature on the 4Q inner wall, and the theoretical air-fuel ratio combustion is performed, aiming at 10 times the 10-fold combustion amount of the existing technological improved theoretical combustion chamber 4Q high pressure high temperature combustion chamber 5M, the outer periphery of the theoretical combustion chamber 4Q The superheated steam rocket nozzle 6A + combustion gas injection nozzle 6Y injects superheated steam 50 and high-pressure high-temperature combustion chamber 5M combustion gas 49 close to 200 MPa to close the on-off valve 1Q for high-power rocket combustion, and on-off valve 1Q open The forward air 28a is used as suction injection jet combustion, the plurality of theoretical combustion chambers 4Q are used as rocket combustion chambers and jet combustion chambers driven by liquid oxygen, and the existing technology improved theoretical combustion chamber 4Q is used as the theoretical air-fuel ratio combustion of four times the fuel of the existing technology. , Manufacturing superheated steam 50 aiming at 200 MPa with increased heat quantity, injecting from rocket outer box 77B superheated steam rocket nozzle 6A, high pressure high temperature combustion chamber 5M As a simple water injection engine 88j is driven by generating a rotational output from the burning gas 49, sucking and injecting the air 28a in front and sucking and injecting water, the existing jet engine is greatly improved. In this case, it is set as a simple water injection engine ship 7n aiming at maintaining the flight speed even in the vicinity of zero liquid oxygen.

The simple injection engine airplane 7o in FIG. 13 is an improved invention of the existing jet aircraft. The simple injection engine 88e can select a compressed air drive + a fuel cost zero power generation electric product selection drive. 8U fuel cost 0 power generation Extremely cheap electricity production Electricity + liquid air cold heat + hot water to superheated steam heat supply facility 3D Receives liquid oxygen + electricity + hot water to the theoretical combustion chamber 4Q, etc. driven by cheap electricity products Then, by compressing liquid oxygen, the compression volume work rate is set to 21/60000 volume compression work rate of air compression, and liquid oxygen + liquid fuel + high temperature water is compressed and heated to an ultrahigh pressure such as 24-200 MPa. In the rocket combustion theoretical combustion chamber 4Q in which the opening / closing valve 1Q at the inlet / outlet is closed, the oxygen + fuel injection combustion heated to the optimum temperature from the oxygen injection nozzle 6L + fuel injection nozzle 6X is performed, and the theoretical combustion chamber 4Q The fuel + oxygen + superheated steam 50 is heated to the optimum temperature at the wall, and the combustion is aimed at the theoretical air-fuel ratio combustion, aiming at the 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, The superheated steam rocket nozzle 6A + combustion gas injection nozzle 6Y injects superheated steam 50 and high-pressure high-temperature combustion chamber 5M combustion gas 49 close to 200 MPa. When 1Q is open, the front air 28a is sucked and injected, and a plurality of theoretical combustion chambers 4Q are used as rocket combustion chambers and jet combustion chambers driven by liquid oxygen, and the theoretical air combustion ratio of the existing technology is 4 times higher than that of the existing technology. As combustion, the superheated steam 50 is manufactured with an increased heat quantity and targeted at 200 MPa, injected from the rocket outer box 77B superheated steam rocket nozzle 6A, and the high pressure high temperature combustion chamber 5M combustion gas Rotation output is generated at 49, the air 28a in front is sucked and injected, and the existing jet engine is greatly improved as a simple injection engine 88k drive. It is assumed that the target is 500,000 and is a simple injection engine airplane 7o in which high-speed flight is performed with zero liquid oxygen in the atmosphere and the propeller 7A is driven by extending the inner shaft device 60A depending on the application.

The rotary wing airplane 7p in FIG. 14 is an improved invention of the existing rotary wing aircraft. The simple gas engine 88i can be selected to be driven by compressed air + zero fuel cost power generation electrical product selection drive. Turbine 8U Fuel cost 0 Power generation Extremely inexpensive electricity production Electricity + liquid air cold heat + high temperature water ~ superheated steam temperature heat supply equipment 3D, liquid oxygen + electricity + high temperature water is supplied to the theoretical combustion chamber 4Q etc. driven by cheap electric products By receiving and compressing liquid oxygen, the compression volume work rate is set to 21/60000 volume compression work rate of air compression, and liquid oxygen + liquid fuel + high temperature water is compressed and heated to an ultrahigh pressure such as 24-200 MPa, In the rocket combustion theoretical combustion chamber 4Q in which the on-off valve 1Q at the plurality of inlets is closed, oxygen + fuel injection heated to an optimum temperature from the oxygen injection nozzle 6L + fuel injection nozzle 6X is combusted, and fuel + Elemental and superheated steam 50 is heated to the optimum temperature and the theoretical air-fuel ratio combustion is performed, and the target is 10 times the pressure 10 times that of the jet combustion theoretical combustion chamber 4Q high-pressure high-temperature combustion chamber 5M. As the stoichiometric air-fuel ratio combustion of double fuel combustion, superheated steam 50 of 200 MPa or the like is manufactured with an increased triple heat quantity, injected from superheated steam rocket nozzle 6A, and targeted for quadruple combustion quantity or 40 times combustion by exhaust injection or rocket injection As a rotor blade airplane 7p which is injected with a high pressure and high temperature combustion chamber 5M and greatly improves the existing rotor wing aircraft, the rotational output of the simple gas engine 88i is used to drive the rotor 7B and exhaust force is driven by the rotating blade 7B. Compressed air + liquid oxygen drive mechanism that drives the inner shaft device 60A extension rotor blade 7B to make rocket combustion + jet combustion + rotation output + injection propulsion output capable of 10 times output, etc. As the combustion chamber 4Q plurality of coalesced, and rotary wing aircraft 7p flying even spaceflight aim and liquid oxygen 0.

A rotary blade injection plane 7q in FIG. 15 is an improved invention simple injection engine 88e of an existing rotary blade aircraft, which can select a compressed air drive + a fuel cost 0 power generation electrical product selection drive. Gravity turbine 8U Fuel cost 0 Power generation Electricity + liquid air cold heat + high temperature water to superheated steam temperature heat supply equipment 3D from liquid electricity + electricity + high temperature water to the theoretical combustion chamber 4Q etc. driven by low cost electric products And compressing liquid oxygen, the compression volume work rate is 21/60000 volume compression work rate of air compression, and liquid oxygen + liquid fuel + high-temperature water is compressed and heated to an ultrahigh pressure such as 24-200 MPa. In the rocket combustion theoretical combustion chamber 4Q with the multiple inlet / outlet on-off valves 1Q closed, the oxygen + fuel injection combustion heated to the optimum temperature from the oxygen injection nozzle 6L + fuel injection nozzle 6X and the inner wall of the theoretical combustion chamber 4Q The fuel + oxygen + superheated steam 50 is heated to the optimum temperature, and the theoretical air-fuel ratio combustion is performed. The combustion chamber 4Q for compressed air combustion is aimed at 10 times the pressure 10 times that of the high-pressure and high-temperature combustion chamber 5M. The superheated steam 50 and the high-pressure high-temperature combustion chamber 5M combustion gas 49 approaching 200 MPa are injected from the steam rocket nozzle 6A + combustion gas injection nozzle 6Y. In the open state, compressed air 28a combustion is injected by theoretical air-fuel ratio combustion or the like, and a plurality of theoretical combustion chambers 4Q are used as rocket combustion chambers / jet combustion chambers driven by liquid oxygen, and in the compressed air combustion jet combustion theoretical combustion chamber 4Q, the conventional technology 4 As the stoichiometric air-fuel ratio combustion of double fuel, superheated steam 50 is produced aiming at 200MPa with an increased heat quantity of 3 times. Then, the superheated steam 50 is injected from the superheated steam rocket nozzle 6A of the suction flow of the peripheral air 28a, the air 28a in front is sucked and injected, and the liquid oxygen drive theoretical combustion chamber is driven as a simple injection engine 88k driven close to the existing jet engine. 4Q Combining multiple units to reach space costs 1 / 500,000 of existing technology, flying in the atmosphere with liquid oxygen 0, driving outer shaft device 60B or inner shaft device 60A extension rotor 7B, rotating output + jet Assume that the propulsion output drive rotary wing jet airplane 7q.

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, an automobile, a ship, an airplane, and the like that are united and driven, and liquid oxygen 5K is liquid-compressed to obtain an air volume compression work rate of 21/60000 volume compression work rate, and a simple gas engine 88i, a simple water injection engine 88j, and a simple injection engine Driving 88k, there is a possibility that CO2 emissions and fuel costs will be close to 1/10 in a car, ships may be close to 10 times the speed with the same fuel cost, and airplanes will cost 1500,000 to reach space. As a prime use of space, there is a possibility of making a great revolution in the use of cold energy, such as making a day trip anywhere on the planet.

0: Various energy storage cycle coalesced engine (various heat energy is compressed and recovered by heat pump as air temperature and divided into liquid air cold heat + superheated steam heat) Gravity energy rises storage spray accelerates gravitational acceleration in vacuum 0: Various energy storage cycle coalescing engine and coalescence method (various heat energy is heated by solar heat or geothermal heat, etc., and is recovered by compressing heat with a heat pump as liquid temperature, liquid air cooling + Divided and stored in superheated steam temperature ・ Used with a heat retaining device when using liquid metal under 500 ℃ ・ Shock energy is used to extend the working time by providing silicon blade coating or fluorine resin coating on turbine blades and small metal balls・ Various energy coalescing engine and various energy coalescence means that use and save the gravitational energy by ascending device) 1A: storage battery, 1B: pressure engine (oxygen pressure gear engine, oxygen pressure reciprocating engine, water pressure gear engine, water pressure reciprocating engine, etc., to make various pressure engines with a compression work rate of 1/600 by liquid compression) 1C: Alcohol, 1D: Fuel injection pump, 1F: Condensate pump, 1G: 1 to multi-stage heat pump (heat 50 is divided into hot room 3B + cold 28a is divided into cold room 3A, aiming at an infinite rise in pressure after increasing the amount of collected cold heat) 1K: Liquid fuel control valve, 1L: Fuel heating pipe, 1Q: On-off valve, 1Y: Multi-stage combustion chamber, 1b: Fuel (liquid fuel + liquefiable gas fuel) 1b: Fuel pipe (fuel injection temperature becomes optimum temperature) 1c: Liquid fuel, 1d: Mercury, 1g: Gravity acceleration part, 1h: Horizontal axis, 2: Solar heater (collecting sunlight in a straight line with a long lens to heat the hot part forming intake air 2a: Natural phenomenon high speed (A large amount of microorganisms that move to zero near the night when leftover foods with almost no change in the air move to nearby rivers will be used to increase food for humans) 2a: Acceleration of natural phenomena (In power generation, cold 28a is mixed with seawater for power generation) Supplying seawater that has been accelerated in natural phenomena to the seabed Supplying nutrients such as nitrogen, oxygen, and CO2 Increases microorganisms to increase foods such as fish and kombu 2a: Speeding up natural phenomena (in ships, nitrogen, oxygen, and CO2 in the sea) 2b: Low water resistance (air and combustion gas on the bottom of the ship) 2b: Low water resistance (air and combustion gas on the bottom of the ship) 2c: heat insulating material, 2d: long lens (convex lens cross-section is extended to a straight line and multiple lenses are used to achieve the maximum focal length lens width) 2e: water surface, 2A : Heat-resistant material, 2B: heat absorbing material, 2C: 1 to multiple-stage compression heat recovery device (heat energy is air temperature, heat pump is heat-recovered a plurality of times with a compression heat exchanger, and the rest is heated 50 + liquid cold 28a 2E: Specific critical substances (including alloys, platinum balls, gold balls, tungsten alloy powder sintered balls, silver balls, copper balls, tin balls, lead balls, zinc balls, aluminum balls, indium, cadmium, gallium, thallium, bismuth 2E: Specific critical substance (Manufacturing method reduces impact energy for smaller diameters. For example, molten steel is injected into the atmosphere to produce ultra-small diameter steel balls by high-speed collision pulverization and air cooling water cooling) 2E: Specific importance Substances (silicon resin-coated or silicon-resin-coated platinum alloy balls, coated gold alloy balls, coated tungsten alloy powder sintered balls, coated silver alloy balls, coated bismuth alloy balls, coated copper alloy balls, coated tin alloy balls, Lead-coated alloy balls, coated zinc alloy balls, coated aluminum alloy balls) 2F: Specific critical material raising device (gravity energy is increased and stored) 2H: Cold and hot seawater mixer, 2X: Air heat exchanger 2Y: Compressed air heat exchanger ( 2Z: Specific material heat exchanger (used for temperature control of liquid metal below 500 degrees) 3a: Water repellent plating, 3f: Simple multistage compressor, 3s: Simple compressor, 3t: Simple multi-stage compressor, 3u: Air turbine, 3A: Water repellent coating, 3B: Water pressure reciprocating engine, 3D: Electricity + liquid air cold heat + superheated steam heat supply equipment Nitrogen is supplied. Cars, ships and airplanes are driven. Superheated steam is supplied. Methane is injected into methane hydrate. Methane is recovered, etc. Electricity + cold energy + hot use. 3E: Specific critical substances (liquid at room temperature such as mercury and water). 3E: Oxygen pressure reciprocating engine 3G: Theoretical combustion gear engine, 3H: Reciprocating piston, 3J: Theoretical combustion reciprocating engine, 3K : External gear, 3L: Multi-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, the best engine + oxygen hydrogen increase combustion aim) 3Q : Theoretical expansion engine (Boil's law is the best engine + aiming at the maximum acceleration drive in vacuum) 3R: Theoretical gas turbine (theoretical best gas turbine whose gas volume is inversely proportional to the pressure) 3S: Theoretical steam turbine (the gas volume is 3T: Theoretical gas compressor (theoretical best gas compressor corresponding to the pressure inversely proportional to the pressure) 3U: Theoretical turbine V: Pump engine (uses existing pumps in the engine) 3X: Compressor engine (uses existing compressors in the engine) 3Y: Counter-rotating engine (engine whose gas volume is inversely proportional to pressure) 3Z: Oxygen pressure Gear engine, 3a: water-repellent plating, 3b: water-repellent coating, 4C: counter-synchronous gear, 4D: series rotating gear, 4F: combustion gas reciprocating engine, 4H: heat absorption tube (long lens 2d absorbs sunlight heat 4J: Storage battery drive wheel, 4K: Theoretical expansion engine car, 4Q: Theoretical combustion chamber (theoretical air-fuel ratio in the production of superheated steam) Combustion chamber with 4 times the existing combustion amount and 20 times pressure superheated steam injection), 4W: Theoretical compression chamber, 4Y: Theoretical combustion chamber (high temperature combustion in water vapor and target compound for pyrolysis electrolysis combustion of water 0 Aiming combustion chamber 4Z: Combustion gas gear engine, 4X: Turbine blade cross section (enlarged surface area with increased cross section) 4a: Liquid fuel pump, 4b: Liquid oxygen pump, 4c: Water pump, 4d: Gear device, 4e: Roller, 4f: Rotation Support part, 5: Air injection nozzle, 5a: High-pressure high-temperature combustion gas control valve, 5b: Compressed intake air passage, 5d: Combustion flow inner wall, 5e: Ultra-high pressure oxygen, 5h: Rectification tower exhaust pipe, 5A: Supply valve 5B: Cooling fin, 5C: Exhaust chamber 5D: Exhaust valve 5E: Air supply chamber 5F: Oxygen heating tube, 5G: Steam heating tube, 5G: High pressure high temperature water heating tube, 5H: High pressure high temperature water heating tube, 5H: High pressure High temperature superheated steam 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 and high temperature Steam, 5P: Steam control valve, 5Q: Water control valve, 5R: Superheated steam control valve, 5S: Compressed air heating pipe, 5T: Liquid oxygen control valve, 6: Final compression blade, 6A: Superheated steam rocket nozzle, 6B: Compressed air injection nozzle, 6E: specific material injection nozzle, 6F: water injection nozzle, 6G: stationary blade, 6H: drain pipe, 6L: oxygen injection nozzle, 6W: specific material accelerator (liquid ratio material 3E pressure and 6X: Fuel injection nozzle, 6X: After burner (combustion of the fuel injection cold heat 28a and the combustion flow 6Y in the suction air flow and the increase in the amount of fuel combustion) 6Y : Combustion gas injection nozzle (cooling 28a combustion flow) 6Z: Water vapor injection nozzle, 7A: Propeller, 7B: Rotary blade, 7C: Screw, 7D: Simple gas locomotive, 7E: Simple gas Kansai 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 7h: simple jet engine airplane, 7i: rotary wing airplane, 7j: rotary wing jet airplane, 7k: simple gas engine automobile, 7l: simple gas engine ship, 7m: simple gas engine airplane, 7n: simple water jet Engine ship, 7o: Simple injection engine airplane, 7p: Rotary blade airplane, 7q: Rotary blade injection airplane, 8c: Turbine blade (The straight and long turbine blades are provided on the outer surface of the cylinder for full automatic machining and weight reduction 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, 8 : Inner compression blades, 8m: Outer compression 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 Rotating blade turbine (opposite fully moving blade pusher turbine series full moving blade pusher turbine turbine biting full moving blade pusher turbine) 8S: Horizontal fully moving blade turbine (fully-automatic machining of inner and outer circumferences by providing straight and large turbine blades on the outer surface of the cylinder) 8S: Horizontal type full-blade hydrogravity turbine (existing steam turbine is a stationary blade and the damming output approaches 0, so all the blades are essential, and the work rate is 1 / 360,000 of platinum balls) 8M: Vertical-type all-blade hydrogravity turbine (6 types of cylindrical turbine blade group fitting assembly + magnetic bearing load approach 0) 8N: Specific gravity of all-type blades Mass Gravity Turbine (6 types of cylindrical turbine blade group fitting assembly + magnetic utilization bearing load approach 0) 8R: Horizontal all blade hydrogravity turbine (cylindrical turbine blade group series opposed synchronous rotation + magnetic utilization bearing load approach 0) 8S: Gravity turbine with horizontal total blade ratio critical material (cylindrical turbine blade group in series opposed synchronous rotation + close to magnetic bearing load 0) 8P: Vertical type full blade hydrogravity turbine (six types of cylindrical turbine motion) Blade group fitting assembly + Magnetic bearing load 0 approach + Super high speed peripheral speed) 8Q: Vertical type moving blade ratio critical material gravity turbine (6 types of cylindrical turbine blade group fitting assembly + magnetic bearing load 0) 8T: Horizontal full blade hydrogravity turbine (cylindrical turbine blade group serially opposed synchronous rotation + magnetic utilization bearing load 0 approach + super high speed peripheral speed) 8U: Horizontal full blade ratio is significant Material gravity Turbine (cylindrical turbine blade group in series opposed synchronous rotation + magnetic bearing load approach 0 + super high speed outer peripheral speed) 9: Wear resistant annular assembly (only the critical material flow path including 8c is made of cemented carbide with an annular manufacturing weight reduction 9b: Upper attracting lower repulsion magnet, 9A: Cylindrical annular assembly (wear-resistant cylindrical annular assembly, 6 types of moving blade group, simple structure, few parts, fully automatic processing, easy assembly, and light weight 9A: Cylindrical annular assembly (inlet fixed outer blade 60E + outer annular blade 60G + outlet fixed outer blade 60J is fitted to form a cylindrical outer moving blade group 60D, and inlet fixed inner blade 60F + inner annular blade 60H + in outlet fixed) 9B: Repulsive permanent magnet, 9C: Suction permanent magnet, 9D: Compressed air part, 9E: Vacuum part, 9M: Mating assembly part, 9Q: Vertical Parallel plate (jetting 10: hull, 10A: cabin, 10b: cockpit, 10c: control room, 10d: cabin, 10e: cargo compartment, 16: horizontal shaft plate (easy assembly) 16A: Horizontal axis, 11D: Cooling chamber dedicated to gas, 21: Solar heater (mainly used with the intake air path provided in the heat absorption pipe 4H) 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 heat (compressed air 28a with a heat pump, compressed air heat amount of superheated steam 50 warm heat + liquid oxygen 28b: Compressed air calorie, 28A: Intake air passage, 28B: Air passage inlet, 38: Rotating guide, 38a: Flight trunk, 38b: Flight wing, 38c: Flight tail , 38d: vertical wing, 38e: leading edge of the wing, 38g: water wing, 38h: floating boat, 38B: air suction jet ship (with 79S79T79Y79Z) 38C: water suction jet ship (with 79U79X) 38H: theoretical screw ship, 38J : Theoretical jet ship, 38T: theoretical jet airplane, 38U: theoretical propeller airplane, 39A: solar thermal gravity airplane, 39B: solar thermal gravity rotating airplane, 39C: solar thermal gravity helicopter, 39D: screw ship, 39G: solar thermal gravity airplane, 39H: Oxygen coalescence screw ship, 39J: oxygen coalescence injection ship, 39K: oxygen coalescence screw injection ship, 39L: oxygen coalescence injection airplane, 39M: oxygen coalescence propeller airplane, 39N: oxygen coalescence propeller injection airplane, 39P: oxygen coalescence rotorcraft, 39Q: Oxygen coalescence screen New 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, 50: Superheated steam 50: Warmth (compressed air 28a is compressed with a heat pump and divided into 50-heated superheated steam of compressed air heat + compressed air 28a cold) 50A: steam, 50a: superheated steam injection pipe, 51: air extractor, 51 : Confluence extractor (extractor for joining) 51A: Air extraction chamber, 52a: High temperature water 52a: Deep sea water, 52b: High temperature water, 52d: Hot heat (change from 50) 52e: Cold heat (change from 28a) 55B : Transmission, 60A: Inner shaft device (equipment with turbine blades) 60B: Outer shaft device (equipment with turbine blades) 60C: Cylindrical inner blade group (anti-resistance) 60D: Cylindrical outer rotor blade group (Fully automatic machining easy assembly including wear-resistant cylindrical annular assembly fixed blade group) 60E : Outlet fixed outer wing (inlet wing for annular assembly fixing outer rotor blade group) 60F: Entrance fixed inner wing (inlet wing for annular assembly fixing inner rotor blade group) 60G: Outer annular blade (outer rotor blade group annular assembly) 60H: Inner annular blade (intermediate blade for annular assembly of inner blade group) 60J: Outlet fixed outer blade (exit blade for annular assembly fixing outer blade group) 60K: Outlet fixed inner blade (inner blade) 76: Gear unit (including magnetic friction power transmission device) 77B: Rocket outer box, 77C: Counter-reversing machine outer box, 77F: Injection unit outer box, 77G: Cylindrical rotating unit, 77a: outer casing of turbine, 77b: compressor Box 80: Bearing (including magnetic bearing + air bearing) 80a: Thrust bearing (including magnetic bearing + air bearing) 80A: Joint, 80B: Fastener, 80Y: Liquid air suction water jet (high pressure high temperature combustion chamber 5M high pressure high temperature Receive water vapor chamber 5N and inject and burn multiple times to 5M, heat and inject 5N multiple times from the inner and outer peripheries, and suck and inject water by air suction and injection) 80Z: Liquid air suction water Jet (high-pressure high-temperature combustion chamber 5M receiving high-pressure high-temperature steam chamber 5N, fuel injection combustion into 5M multiple times, and 5N is heated and injected multiple times from the inner and outer peripheries, and air suction flow is also applied to multiple locations. Fuel injection combustion injection, air suction injection and water suction injection) 84: Counter-rotating magnetic friction device (a device that rotates the inner rotor blade group and the outer rotor blade group at substantially the same speed in opposite directions) 84Y : Counter rotating gear device ( 85: Counter-rotating magnetic device (magnet-utilized gear height is slight to non-contact and reciprocally rotated with the horizontal shaft 1h gear) 85Y: Counter-rotating gear device (with the existing horizontal shaft 1h gear) 88a: simple gas engine, 88c: simple water injection engine, 88d: simple gas engine, 88f: simple injection engine, 88e: simple water injection engine, 88g: liquid oxygen production machine 88h: liquid oxygen production machine, 88i: simple gas engine, 88j: simple water injection engine, 88k: simple injection engine, 88A: oxygen combined air injection unit (rocket injection + jet combustion + steam injection and combined injection) 88B: Oxygen combined air injection unit (ultra-high pressure rocket combustion + jet combustion + superheated steam injection suction) 88C: theoretical air injection unit, 88M: theoretical water injection unit, 88K: oxygen combination Water injection unit (rocket combustion + jet combustion + steam injection and combined injection) 88L: oxygen combined water injection unit (super high pressure rocket combustion + jet combustion + superheated steam injection suction) 95a: combustion gas reservoir, 95b: compressed air reservoir, 95c: Superheated steam reservoir, 103: Cold heat recovery device,

Claims (417)

  The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronized rotation A horizontal full rotor blade having a series of co-rotating gears (4D) between the horizontal shafts (16A) and rotating in the same direction in the same direction in the vertical direction so that the bearing load is close to 0 and the super-high speed circumferential speed is achieved. Specific energy gravity turbine (8U) 1-20 sets of power generation electric product drive + both center support bearing load 0 approach counter-rotating production compressed air (28a) drive combined various energy storage cycle coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. A horizontal full rotor blade having a series of co-rotating gears (4D) between the horizontal shafts (16A) and rotating in the same direction in the same direction in the vertical direction so that the bearing load is close to 0 and the super-high speed circumferential speed is achieved. Specific energy material gravity turbine (8U) 21 to 40 sets of power generation electric product driving + both center support bearing load 0 approaching counter-rotating production compressed air (28a) driving combined various energy storage cycle coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. A horizontal all blade having a series rotating gear (4D) between the horizontal shafts (16A) and rotating in the same vertical direction at the same speed in each pair so that the bearing load is close to 0 and the super high speed circumferential speed is achieved. Specific energy material gravity turbine (8U) 41-60 sets of power generation electric product drive + both center support bearing load 0 approach counter-rotating production compressed air (28a) drive combined various energy storage cycle coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. A horizontal full rotor blade having a series of co-rotating gears (4D) between the horizontal shafts (16A) and rotating in the same direction in the same direction in the vertical direction so that the bearing load is close to 0 and the super-high speed circumferential speed is achieved. Specific energy gravitational turbine (8U) 61-80 sets of power generation electric product drive + both center support bearing load 0 approach counter-rotating production compressed air (28a) drive combined various energy storage cycle coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. A horizontal full rotor blade having a series of co-rotating gears (4D) between the horizontal shafts (16A) and rotating in the same direction in the same direction in the vertical direction so that the bearing load is close to 0 and the super-high speed circumferential speed is achieved. Specific energy material gravity turbine (8U) 81 to 100 sets of power generation electric product drive + both center support bearing load 0 approaching counter-rotating production compressed air (28a) drive combined various energy storage cycle coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. A horizontal full rotor blade having a series of co-rotating gears (4D) between the horizontal shafts (16A) and rotating in the same direction in the same direction in the vertical direction so that the bearing load is close to 0 and the super-high speed circumferential speed is achieved. Specific energy material gravity turbine (8U) 101-120 generator power generation electric product drive + both center support bearing load 0 approach counter-rotating production compressed air (28a) drive combined various energy storage cycle coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. A horizontal full rotor blade having a series of co-rotating gears (4D) between the horizontal shafts (16A) and rotating in the same direction in the same direction in the vertical direction so that the bearing load is close to 0 and the super-high speed circumferential speed is achieved. Specific energy material gravity turbine (8U) 121-140 set generation electric product drive + both-side center support bearing load 0 approaching counter-rotating production compressed air (28a) drive combined various energy storage cycle coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. A horizontal full rotor blade having a series of co-rotating gears (4D) between the horizontal shafts (16A) and rotating in the same direction in the same direction in the vertical direction so that the bearing load is close to 0 and the super-high speed circumferential speed is achieved. Specific energy material gravity turbine (8U) 141 to 160 sets of power generation electric product drive + both center support bearing load 0 approaching counter-rotating production compressed air (28a) drive combining various energy storage cycle coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. A horizontal full rotor blade having a series of co-rotating gears (4D) between the horizontal shafts (16A) and rotating in the same direction in the same direction in the vertical direction so that the bearing load is close to 0 and the super-high speed circumferential speed is achieved. Specific energy material gravity turbine (8U) 161-180 sets of power generation electric product drive + both center support bearing load 0 approach counter-rotating production compressed air (28a) drive combined various energy storage cycle coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. A horizontal full rotor blade having a series of co-rotating gears (4D) between the horizontal shafts (16A) and rotating in the same direction in the same direction in the vertical direction so that the bearing load is close to 0 and the super-high speed circumferential speed is achieved. Specific energy material gravity turbine (8U) 181 to 200 sets of power generation electric product drive + both center support bearing load 0 approach counter-rotating production compressed air (28a) drive combined various energy storage cycle coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. Magnetic bearing load that is provided with a series of same rotating gears (4D) between horizontal axes (16A), and is driven by injection with specific material (3E) Mach 1-30 by rotating in the same direction in the same vertical direction. Horizontal approaching blade ratio critical material gravity turbine (8U) 1-20 sets driving electric product drive with 0 approach + super high speed circumferential speed + both sides center support bearing load 0 approach counter-rotating production compressed air (28a) drive Various energy storage cycle coalescence engines and coalescence methods to be coalesced.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. Magnetic bearing load that is provided with a series of same rotating gears (4D) between horizontal axes (16A), and is driven by injection with specific material (3E) Mach 1-30 by rotating in the same direction in the same vertical direction. Horizontal approaching blade ratio critical material gravity turbine (8U) 21 to 40 sets of power generation electrical product drive with 0 approaching + super high speed circumferential speed + both sides center support bearing load 0 approaching counter-rotating production compressed air (28a) drive Various energy storage cycle coalescence engines and coalescence methods to be coalesced.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. Magnetic bearing load that is provided with a series of same rotating gears (4D) between horizontal axes (16A), and is driven by injection with specific material (3E) Mach 1-30 by rotating in the same direction in the same vertical direction. Horizontal approaching blade ratio critical material gravity turbine (8U) 41-60 sets driven by electrical approach to zero approach + super high speed circumferential speed + both sides center support bearing load 0 approach counter rotating production compressed air (28a) drive Various energy storage cycle coalescence engines and coalescence methods to be coalesced.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. Magnetic bearing load that is provided with a series of same rotating gears (4D) between horizontal axes (16A), and is driven by injection with specific material (3E) Mach 1-30 by rotating in the same direction in the same vertical direction. Horizontal approaching blade ratio critical material gravity turbine (8U) 61-80 sets generating electric product drive with 0 approach + super high speed circumferential speed + both sides center support bearing load 0 approach counter rotating manufactured compressed air (28a) drive Various energy storage cycle coalescence engines and coalescence methods to be coalesced.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. Magnetic bearing load that is provided with a series of same rotating gears (4D) between horizontal axes (16A), and is driven by injection with specific material (3E) Mach 1-30 by rotating in the same direction in the same vertical direction. Horizontal approaching blade ratio critical material gravity turbine (8U) 81-100 set generating electric product drive with 0 approach + super high speed circumferential speed + both sides center support bearing load 0 approach counter-rotating production compressed air (28a) drive Various energy storage cycle coalescence engines and coalescence methods to be coalesced.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. Magnetic bearing load that is provided with a series of same rotating gears (4D) between horizontal axes (16A), and is driven by injection with specific material (3E) Mach 1-30 by rotating in the same direction in the same vertical direction. Horizontal approaching blade ratio critical material gravity turbine (8U) 101-120 sets driven by zero approach + ultra high speed circumferential speed + both sides center support bearing load 0 approach counter rotating manufactured compressed air (28a) drive Various energy storage cycle coalescence engines and coalescence methods to be coalesced.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. Magnetic bearing load that is provided with a series of same rotating gears (4D) between horizontal axes (16A), and is driven by injection with specific material (3E) Mach 1-30 by rotating in the same direction in the same vertical direction. Horizontal approaching blade ratio critical material gravity turbine (8U) 121-140 sets driven by zero approach + ultra high speed circumferential speed + both-side center support bearing load 0 approach counter rotating manufactured compressed air (28a) drive Various energy storage cycle coalescence engines and coalescence methods to be coalesced.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. Magnetic bearing load that is provided with a series of same rotating gears (4D) between horizontal axes (16A), and is driven by injection with specific material (3E) Mach 1-30 by rotating in the same direction in the same vertical direction. Horizontal approaching blade ratio critical material gravity turbine (8U) 141-160 set with 0 approaching + super high speed circumferential speed power generation electric product drive + both sides center support bearing load 0 approaching counter-rotating production compressed air (28a) drive Various energy storage cycle coalescence engines and coalescence methods to be coalesced.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. Magnetic bearing load that is provided with a series of same rotating gears (4D) between horizontal axes (16A), and is driven by injection with specific material (3E) Mach 1-30 by rotating in the same direction in the same vertical direction. Horizontal approaching blade ratio critical material gravity turbine (8U) 161-180 sets driven to zero approach + super high speed circumferential speed + both sides center support bearing load 0 approach counter rotating manufactured compressed air (28a) drive Various energy storage cycle coalescence engines and coalescence methods to be coalesced.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. Magnetic bearing load that is provided with a series of same rotating gears (4D) between horizontal axes (16A), and is driven by injection with specific material (3E) Mach 1-30 by rotating in the same direction in the same vertical direction. Horizontal approaching blade ratio critical material gravity turbine (8U) 181 to 200 sets driven by zero approach + ultra high speed circumferential speed + both-side center support bearing load 0 approach counter rotating manufactured compressed air (28a) drive Various energy storage cycle coalescence engines and coalescence methods to be coalesced.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and a pair of vertical rotations in the same direction and rotation at the same speed, aiming at the specific material (3E) Mach 30 and the injection ratio material (2E). Mixed injection acceleration drive magnetically utilized bearing load approaching 0 + ultra-high speed peripheral speed blades critical material gravity turbine (8U) 1-20 sets generator electric product drive + both sides center support bearing load approaching 0 approach double Various energy storage cycle merging engines and merging methods for merging driven inverted compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and a pair of vertical rotations in the same direction and rotation at the same speed, aiming at the specific material (3E) Mach 30 and the injection ratio material (2E). Mixed magnetic-acceleration driven magnetic drive bearing load approaching 0 + ultra-high speed peripheral blade ratio critical material gravity turbine (8U) 21-40 sets generator electric product drive + both sides center support bearing load approaching 0 approach double Various energy storage cycle coalescing engines and coalescence methods for coalescence of inverted manufacturing compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and a pair of vertical rotations in the same direction and rotation at the same speed, aiming at the specific material (3E) Mach 30 and the injection ratio material (2E). Mixed magnetic-acceleration driven magnetically driven bearing load approaching 0 + ultra-high speed peripheral blade ratio critical material gravity turbine (8U) 41-60 sets generating electric product drive + double-sided center support bearing load approaching 0 approach double Various energy storage cycle merging engines and merging methods for merging driven inverted compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and a pair of vertical rotations in the same direction and rotation at the same speed, aiming at the specific material (3E) Mach 30 and the injection ratio material (2E). Mixed injection acceleration drive magnetically utilized bearing load approaching 0 + super high speed circumferential speed with a full blade ratio critical material gravity turbine (8U) 61-80 sets power generation electric product drive + both sides center support bearing load approaching 0 approach double Various energy storage cycle merging engines and merging methods for merging driven inverted compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and a pair of vertical rotations in the same direction and rotation at the same speed, aiming at the specific material (3E) Mach 30 and the injection ratio material (2E). Mixed injection acceleration driven magnetically utilized bearing load approaching 0 + ultra-high speed peripheral blade ratio critical material gravity turbine (8U) 81-100 sets generator electric product drive + both sides center support bearing load approaching 0 approach double Various energy storage cycle coalescing engines and coalescence methods for coalescence of inverted manufacturing compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronized rotation , With the same rotation gear (4D) in series between the horizontal axes (16A), and a pair of vertical rotations in the same direction and rotation at the same speed, aiming at the specific material (3E) Mach 30 and the injection ratio material (2E). Mixed magnetic-acceleration driven magnetic bearing load approaching 0 + ultra-high speed peripheral blade ratio critical material gravity turbine (8U) 101-120 set power generation electric product drive + double-side center support bearing load approaching 0 approach double Various energy storage cycle merging engines and merging methods for merging driven inverted compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and a pair of vertical rotations in the same direction and rotation at the same speed, aiming at the specific material (3E) Mach 30 and the injection ratio material (2E). Mixed magnetic-acceleration driven magnetic bearing load approaching 0 + ultra-high speed peripheral blade ratio critical material gravity turbine (8U) 121-140 set generator electric product drive + double-sided center support bearing load approaching 0 approach double Various energy storage cycle merging engines and merging methods for merging driven inverted compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and a pair of vertical rotations in the same direction and rotation at the same speed, aiming at the specific material (3E) Mach 30 and the injection ratio material (2E). Mixed injection acceleration drive magnetically utilized bearing load approaching 0 + ultra-high speed peripheral speed blades critical material gravity turbine (8U) 141-160 sets generator electric product drive + both sides center support bearing load approaching 0 approach double Various energy storage cycle merging engines and merging methods for merging driven inverted compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and a pair of vertical rotations in the same direction and rotation at the same speed, aiming at the specific material (3E) Mach 30 and the injection ratio material (2E). Mixed injection acceleration drive using magnetic bearing load approaching 0 + ultra-high speed peripheral blade ratio critical material gravity turbine (8U) 161-180 set generator electric product drive + both sides center support bearing load approaching 0 approach double Various energy storage cycle merging engines and merging methods for merging driven inverted compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and the same rotation speed in the same vertical direction in each pair, and the injection ratio critical substance (2E) with the aim of the specific critical substance (3E) Mach 30 Mixed injection acceleration driven magnetically utilized bearing load approaching 0 + ultra-high speed peripheral blade ratio critical material gravity turbine (8U) 181 to 200 sets generator electric product drive + both sides center support bearing load approaching 0 approach double Various energy storage cycle merging engines and merging methods for merging driven inverted compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , Equipped with a series rotation gear (4D) between the horizontal axes (16A) and rotating in the same direction in the same vertical direction, allowing cutting of the entire inner diameter. Various types of energy storage to combine the horizontal-type full-blade ratio critical material gravity turbine (8U) 1 to 20 generator electric product drive + both-side center support bearing load 0 approach counter-rotating production compressed air (28a) drive with peripheral speed Cycle coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , Equipped with a series rotation gear (4D) between the horizontal axes (16A) and rotating in the same direction in the same vertical direction, allowing cutting of the entire inner diameter. Various types of energy conservation to combine the peripheral full-blade ratio critical material gravity turbine (8U) 21 to 40 sets of power generation electrical product drive + both-side center support bearing load 0 approach counter-rotating production compressed air (28a) drive Cycle coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , Equipped with a series rotation gear (4D) between the horizontal axes (16A) and rotating in the same direction in the same vertical direction, allowing cutting of the entire inner diameter. Various types of energy conservation to combine the peripheral type moving blade ratio critical gravity gravity turbine (8U) 41-60 generator power product drive + both-side center support bearing load 0 approach counter-rotating production compressed air (28a) drive with peripheral speed Cycle coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , Equipped with a series rotation gear (4D) between the horizontal axes (16A) and rotating in the same direction in the same vertical direction, allowing cutting of the entire inner diameter. Various types of energy conservation to combine the peripheral type moving blade ratio critical material gravity turbine (8U) 61-80 generator power product drive + both-side center support bearing load 0 approach counter-rotating production compressed air (28a) drive with peripheral speed Cycle coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , Equipped with a series rotation gear (4D) between the horizontal axes (16A) and rotating in the same direction in the same vertical direction, allowing cutting of the entire inner diameter. Various types of energy conservation to combine the peripheral full-blade ratio critical material gravity turbine (8U) 81-100 power generation electrical product drive + both-side center support bearing load 0 approach counter-rotating production compressed air (28a) drive Cycle coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , Equipped with a series rotation gear (4D) between the horizontal axes (16A) and rotating in the same direction in the same vertical direction, allowing cutting of the entire inner diameter. Various types of energy storage to combine the peripheral full-blade ratio critical material gravity turbine (8U) 101-120 generator electric product drive + both-side center support bearing load 0 approach counter-rotating production compressed air (28a) drive Cycle coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , Equipped with a series rotation gear (4D) between the horizontal axes (16A) and rotating in the same direction in the same vertical direction, allowing cutting of the entire inner diameter. Various types of energy storage to combine the horizontal full-blade ratio critical material gravity turbine (8U) 121-140 set generator electric product drive + both-side center support bearing load 0 approach counter-rotating production compressed air (28a) drive with peripheral speed Cycle coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , Equipped with a series rotation gear (4D) between the horizontal axes (16A) and rotating in the same direction in the same vertical direction, allowing cutting of the entire inner diameter. Various types of energy storage to combine the horizontal full-blade ratio critical material gravity turbine (8U) 141 to 160 sets of power generation electric product drive + both-side center support bearing load 0 approach counter-rotating production compressed air (28a) drive Cycle coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , Equipped with a series rotation gear (4D) between the horizontal axes (16A) and rotating in the same direction in the same vertical direction, allowing cutting of the entire inner diameter. Various types of energy conservation to combine the peripheral type moving blade ratio critical material gravity turbine (8U) 161-180 sets of power generation electrical product drive + both sides center support bearing load 0 approach counter-rotating production compressed air (28a) drive Cycle coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , Equipped with a series rotation gear (4D) between the horizontal axes (16A) and rotating in the same direction in the same vertical direction, allowing cutting of the entire inner diameter. Various types of energy conservation to combine the peripheral type moving blade ratio critical material gravity turbine (8U) 181 to 200 sets of power generation electrical product drive + both-side center support bearing load 0 approach counter-rotating production compressed air (28a) drive with peripheral speed Cycle coalescence engine and coalescence method.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , Equipped with a series rotation gear (4D) between the horizontal axes (16A), rotating in the same direction in the same vertical direction and rotating at the same speed, and cutting the entire inner diameter by spraying with specific material (3E) Mach 1-30 Largest experimentally used magnetic bearing load of 0 approach + horizontal full blade ratio critical material gravity turbine (8U) 1 to 20 sets driven by super high speed circumferential speed + both-side center support bearing load 0 approach double reversal Various energy storage cycle coalescence engines and coalescence methods for coalescence of manufacturing compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , Equipped with a series rotation gear (4D) between the horizontal axes (16A), rotating in the same direction in the same vertical direction and rotating at the same speed, and cutting the entire inner diameter by spraying with specific material (3E) Mach 1-30 Largest experimentally used magnetic bearing load of 0 approach + horizontal high blade ratio critical material gravity turbine (8U) 21 to 40 sets driven by super high speed circumferential speed + both sides center support bearing load 0 approach double reversal Various energy storage cycle coalescence engines and coalescence methods for coalescence of production compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , Equipped with a series rotation gear (4D) between the horizontal axes (16A), rotating in the same direction in the same vertical direction and rotating at the same speed, and cutting the entire inner diameter by spraying with specific material (3E) Mach 1-30 Largest experimentally used magnetic bearing load of 0 approach + horizontal high blade ratio critical material gravity turbine (8U) 41-60 sets driven by super high speed circumferential speed + both sides center support bearing load 0 approach double reversal Various energy storage cycle coalescence engines and coalescence methods for coalescence of production compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronized rotation , Equipped with a series rotation gear (4D) between the horizontal axes (16A), rotating in the same direction in the same vertical direction and rotating at the same speed, and cutting the entire inner diameter by spraying with specific material (3E) Mach 1-30 Largest experimentally used magnetic bearing load of 0 approach + horizontal high-speed blade ratio critical material gravity turbine (8U) 61 to 80 sets of power generation electric product drive with super high speed circumferential speed + double-side center support bearing load 0 approach double reversal Various energy storage cycle coalescence engines and coalescence methods for coalescence of production compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , Equipped with a series rotation gear (4D) between the horizontal axes (16A), rotating in the same direction in the same vertical direction and rotating at the same speed, and cutting the entire inner diameter by spraying with specific material (3E) Mach 1-30 Largest experimental diameter bearing using magnetic force 0 approach + ultra-high speed circumferential blade ratio critical material gravity turbine (8U) 81-100 sets of power generation electric product drive + both sides center support bearing load 0 approach double reversal Various energy storage cycle coalescence engines and coalescence methods for coalescence of production compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , Equipped with a series rotation gear (4D) between the horizontal axes (16A), rotating in the same direction in the same vertical direction and rotating at the same speed, and cutting the entire inner diameter by spraying with specific material (3E) Mach 1-30 Largest experimental diameter magnetic bearing load approaching 0 + ultra-high speed circumferential speed with a full blade ratio critical material gravity turbine (8U) 101-120 generator drive electric product drive + both sides center support bearing load 0 approaching double reversal Various energy storage cycle coalescence engines and coalescence methods for coalescence of production compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , Equipped with a series rotation gear (4D) between the horizontal axes (16A), rotating in the same direction in the same vertical direction and rotating at the same speed, and cutting the entire inner diameter by spraying with specific material (3E) Mach 1-30 Largest experimental diameter magnetic bearing load approaching 0 + ultra-high speed circumferential speed with full blade ratio critical material gravity turbine (8U) 121-140 generator drive + both-side center support bearing load 0 approaching double reversal Various energy storage cycle coalescence engines and coalescence methods for coalescence of production compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , Equipped with a series rotation gear (4D) between the horizontal axes (16A), rotating in the same direction in the same vertical direction and rotating at the same speed, and cutting the entire inner diameter by spraying with specific material (3E) Mach 1-30 Largest experimental diameter bearing using magnetic force 0 approach + ultra-high speed circumferential blade ratio critical material gravity turbine (8U) 141-160 sets generator electric product drive + both sides center support bearing load 0 approach double reversal Various energy storage cycle coalescence engines and coalescence methods for coalescence of production compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , Equipped with a series rotation gear (4D) between the horizontal axes (16A), rotating in the same direction in the same vertical direction and rotating at the same speed, and cutting the entire inner diameter by spraying with specific material (3E) Mach 1-30 Largest experimental diameter magnetic bearing load approaching 0 + ultra-high speed circumferential speed with a full blade ratio critical material gravity turbine (8U) 161-180 set power generation electric product drive + both sides center support bearing load 0 approaching double reversal Various energy storage cycle coalescence engines and coalescence methods for coalescence of production compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , Equipped with a series rotation gear (4D) between the horizontal axes (16A), rotating in the same direction in the same vertical direction and rotating at the same speed, and cutting the entire inner diameter by spraying with specific material (3E) Mach 1-30 Largest experimental diameter bearings using magnetic bearings approaching zero + ultra-high speed circumferential speed with a full blade ratio critical material gravity turbine (8U) 181 to 200 generators driven electric product drive + double-side center support bearings approaching zero approaching double reversal Various energy storage cycle coalescence engines and coalescence methods for coalescence of production compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and a pair of vertical rotations in the same direction and rotation at the same speed, aiming at the specific material (3E) Mach 30 and the injection ratio material (2E). Mixed injection acceleration driven inside diameter can be cut all the way Experiment using the maximum diameter magnetic bearing load close to 0 + ultra-high speed peripheral blade ratio critical material gravity turbine (8U) 1 to 20 sets of power generation electric product drive + both sides Various energy storage cycle coalescence engines and coalescence methods for coalescence of center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and a pair of vertical rotations in the same direction and rotation at the same speed, aiming at the specific material (3E) Mach 30 and the injection ratio material (2E). Mixed jet acceleration driven inside diameter can be cut all the way Experiment using the maximum diameter magnetic bearing load close to 0 + ultra-high speed circumferential speed of all blades critical material gravity turbine (8U) 21 to 40 sets Driven electric product drive + both sides Various energy storage cycle coalescence engines and coalescence methods for coalescence of center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and a pair of vertical rotations in the same direction and rotation at the same speed, aiming at the specific material (3E) Mach 30 and the injection ratio material (2E). Mixed injection acceleration driven inside diameter can be cut all the way Experiment using the maximum diameter magnetic bearing load close to 0 + ultra-high speed circumferential speed of all blades critical material gravity turbine (8U) 41-60 sets drive electric power product drive + both sides Various energy storage cycle coalescence engines and coalescence methods for coalescence of center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and a pair of vertical rotations in the same direction and rotation at the same speed, aiming at the specific material (3E) Mach 30 and the injection ratio material (2E). Mixed injection acceleration driven inside diameter can be cut all the way Experiment using the maximum diameter magnetic bearing load close to 0 + ultra-high speed circumferential speed of all moving blade ratio critical material gravity turbine (8U) 61-80 sets power generation electric product drive + both sides Various energy storage cycle coalescence engines and coalescence methods for coalescence of center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and a pair of vertical rotations in the same direction and rotation at the same speed, aiming at the specific material (3E) Mach 30 and the injection ratio material (2E). Mixed injection acceleration drive possible to cut the entire inner surface of the experiment. Use of the maximum diameter magnetic bearing load approaching 0 + ultra-high speed peripheral blade ratio critical material gravity turbine (8U) 81 to 100 sets of power generation electric product drive + both sides Various energy storage cycle coalescence engines and coalescence methods for coalescence of center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and a pair of vertical rotations in the same direction and rotation at the same speed, aiming at the specific material (3E) Mach 30 and the injection ratio material (2E). Mixed injection acceleration driven inside diameter can be cut all the way Experiment using the maximum diameter magnetic bearing load approaching 0 + ultra-high speed peripheral blade ratio critical material gravity turbine (8U) 101-120 set generator electric product drive + both sides Various energy storage cycle coalescence engines and coalescence methods for coalescence of center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and a pair of vertical rotations in the same direction and rotation at the same speed, aiming at the specific material (3E) Mach 30 and the injection ratio material (2E). Mixed injection acceleration driven inside diameter can be cut all the way Experiment using the maximum diameter magnetic bearing load approaching 0 + super high speed circumferential speed ratio of all blades critical gravity gravity turbine (8U) 121-140 set power generation electric product drive + both sides Various energy storage cycle coalescence engines and coalescence methods for coalescence of center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and a pair of vertical rotations in the same direction and rotation at the same speed, aiming at the specific material (3E) Mach 30 and the injection ratio material (2E). Mixed injection acceleration drive possible to cut the entire inner diameter of the experiment. Use of the maximum diameter magnetic bearing load approaching 0 + ultra-high speed circumferential speed of all moving blades ratio critical material gravity turbine (8U) 141-160 set power generation electric product drive + both sides Various energy storage cycle coalescence engines and coalescence methods for coalescence of center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and a pair of vertical rotations in the same direction and rotation at the same speed, aiming at the specific material (3E) Mach 30 and the injection ratio material (2E). Mixed injection acceleration driven inside diameter can be cut all-around Experiment using the maximum diameter magnetic bearing load close to 0 + ultra-high speed circumferential speed of all blades critical material gravity turbine (8U) 161-180 set power generation electric product drive + both sides Various energy storage cycle coalescence engines and coalescence methods for coalescence of center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) drive.   The horizontal shaft (16A) is fixed to the both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and the horizontal shaft (16A) is provided with a counter-synchronous gear (4C) for one set of counter-synchronous rotation. , With the same rotation gear (4D) in series between the horizontal axes (16A), and a pair of vertical rotations in the same direction and rotation at the same speed, aiming at the specific material (3E) Mach 30 and the injection ratio material (2E). Mixed injection acceleration driven inside diameter can be cut all the way Experiment using the largest diameter magnetic bearing load close to 0 + ultra-high speed circumferential speed of all blades critical material gravity turbine (8U) 181 to 200 sets Driven electric product drive + both sides Various energy storage cycle coalescence engines and coalescence methods for coalescence of center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) drive.   Cylindrical turbine blade group (8A) with a horizontal shaft (16A) fixed on both sides by a horizontal shaft plate (16) as one set, and an opposed series full blade impeller turbine. Combined with various types of energy conservation cycle to combine the horizontal full-blade ratio critical material gravity turbine (8U) 1-20 sets of power generation electric product drive + both-side center support bearing load 0 approach counter-rotating production compressed air (28a) drive Organization and coalescence method.   Cylindrical turbine blade group (8A) with a horizontal shaft (16A) fixed on both sides by a horizontal shaft plate (16) as one set, and an opposed series full blade impeller turbine. Combined with various types of energy storage cycle to combine the horizontal type rotor blade critical material gravity turbine (8U) 21 to 40 sets of power generation electric product drive + double-sided center support bearing load 0 approach counter-rotating production compressed air (28a) drive Organization and coalescence method.   Cylindrical turbine blade group (8A) with a horizontal shaft (16A) fixed on both sides by a horizontal shaft plate (16) as one set, and an opposed series full blade impeller turbine. Combined various energy storage cycle coalescence of horizontal full blade ratio critical material gravity turbine (8U) 41-60 sets of power generation electrical product drive + double-side center support bearing load 0 approach counter-rotating production compressed air (28a) drive Organization and coalescence method.   Cylindrical turbine blade group (8A) with a horizontal shaft (16A) fixed on both sides by a horizontal shaft plate (16) as one set, and an opposed series full blade impeller turbine. Combined various energy conservation cycle to make the combined of full horizontal blade ratio material gravity turbine (8U) 61-80 power generation electric product drive + both sides center support bearing load 0 approach counter rotating production compressed air (28a) drive Organization and coalescence method.   Cylindrical turbine blade group (8A) with a horizontal shaft (16A) fixed on both sides by a horizontal shaft plate (16) as one set, and an opposed series full blade impeller turbine. Combined with various types of energy storage cycle to combine the horizontal full-blade ratio critical material gravity turbine (8U) 81-100 power generation electric product drive + both sides center support bearing load 0 approach counter-rotating production compressed air (28a) drive Organization and coalescence method.   Cylindrical turbine blade group (8A) with a horizontal shaft (16A) fixed on both sides by a horizontal shaft plate (16) as one set, and an opposed series full blade impeller turbine. Combined with various types of energy storage cycle to combine the horizontal full-blade ratio critical material gravity turbine (8U) 101-120 generator power generation electric product drive + both sides center support bearing load 0 approach counter-rotating production compressed air (28a) drive Organization and coalescence method.   Cylindrical turbine blade group (8A) with a horizontal shaft (16A) fixed on both sides by a horizontal shaft plate (16) as one set, and an opposed series full blade impeller turbine. Combined with various types of energy conservation cycle to combine the horizontal type moving blade ratio critical material gravity turbine (8U) 121-140 set generator electric product drive + both sides center support bearing load 0 approach counter rotating production compressed air (28a) drive Organization and coalescence method.   Cylindrical turbine blade group (8A) with a horizontal shaft (16A) fixed on both sides by a horizontal shaft plate (16) as one set, and an opposed series full blade impeller turbine. Combined various energy storage cycle to combine the horizontal full blade ratio material gravity turbine (8U) 141-160 generator power generation electric product drive + both sides center support bearing load 0 approach counter-rotating production compressed air (28a) drive Organization and coalescence method.   Cylindrical turbine blade group (8A) with a horizontal shaft (16A) fixed on both sides by a horizontal shaft plate (16) as one set, and an opposed series full blade impeller turbine. Combined various energy conservation cycle to combine the horizontal full-blade ratio critical material gravity turbine (8U) 161-180 generator power generation electric product drive + both sides center support bearing load 0 approach counter-rotating production compressed air (28a) drive Organization and coalescence method.   Cylindrical turbine blade group (8A) with a horizontal shaft (16A) fixed on both sides by a horizontal shaft plate (16) as one set, and an opposed series full blade impeller turbine. Combined with various types of energy conservation cycle to combine the following: Institution and coalescence method.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a series full blade impeller turbine is used. 1 to 20 sets of horizontal full blade ratio critical material gravity turbine (power generation electric product drive + double-side center support bearing load 0 approach counter-rotating production compressed air (28a) drive combined with various energy conservation cycle coalescence engine And coalescing method.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a series full blade impeller turbine is used. Combined engine with a horizontal full-blade ratio critical material gravity turbine (8U) 21 to 40 generator electric product drive + double-side center support bearing load 0 approach counter-rotating production compressed air (28a) drive And coalescing method.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a series full blade impeller turbine is used. Horizontal full blade ratio critical material gravity turbine (8U) 41-60 sets of power generation electric product drive + double-sided center support bearing load 0 approach counter-rotating production compressed air (28a) drive combined various energy conservation cycle coalescence engine And coalescing method.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a series full blade impeller turbine is used. Horizontal full blade ratio critical material gravity turbine (8U) 61-80 sets of power generation electric product drive + double side center support bearing load 0 approach counter rotating manufactured compressed air (28a) drive combined with various energy conservation cycle coalescence engine And coalescing method.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a series full blade impeller turbine is used. Combined engine with a horizontal full-blade ratio critical material gravity turbine (8U) 81 to 100 generator power generation electric product drive + double-side center support bearing load 0 approaching counter-rotating production compressed air (28a) drive And coalescing method.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a series full blade impeller turbine is used. Combined engine with various full-blade blade ratio critical material gravity turbine (8U) 101-120 power generation electric product drive + double-side center support bearing load 0 approach counter-rotating production compressed air (28a) drive And coalescing method.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a series full blade impeller turbine is used. Horizontal full blade ratio critical material gravity turbine (8U) 121-140 generator power generation electric product drive + double-side center support bearing load 0 approach counter-rotating production compressed air (28a) drive combined various energy conservation cycle coalescence engine And coalescing method.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a series full blade impeller turbine is used. Combined engine with a horizontal full-blade ratio critical material gravity turbine (8U) 141-160 generator power generation electric product drive + double-side center support bearing load 0 approach counter-rotating production compressed air (28a) drive And coalescing method.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a series full blade impeller turbine is used. Horizontal all blade ratio critical material gravity turbine (8U) 161-180 sets of power generation electric product drive + both center support bearing load 0 approach counter-rotating production compressed air (28a) drive combined various energy conservation cycle coalescence engine And coalescing method.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a series full blade impeller turbine is used. Combined engine with various full-blade blade ratio critical material gravity turbine (8U) 181 to 200 generator power generation electric product drive + double-side center support bearing load 0 approach counter-rotating production compressed air (28a) drive And coalescing method.   Cylindrical turbine blade group (8A) horizontal shaft (16A) fixed on both sides with horizontal shaft plate (16), one set of two, using a bite series full blade impeller turbine, approaching magnetic bearing load 0 approach + super high speed circumference Horizontal full blade ratio critical material gravity turbine (8U) 1 to 20 sets of power generation electric product drive + double-sided center support bearing load 0 approach counter-rotating production compressed air (28a) drive combined various energy storage cycles Merger engine and merger method.   Cylindrical turbine blade group (8A) horizontal shaft (16A) fixed on both sides with horizontal shaft plate (16), one set of two, using a bite series full blade impeller turbine, approaching magnetic bearing load 0 approach + super high speed circumference Horizontal full blade ratio critical material gravity turbine (8U) 21-40 sets of power generation electrical product drive + double side center support bearing load 0 approach counter-rotating production compressed air (28a) drive combined various energy storage cycles Merger engine and merger method.   Cylindrical turbine blade group (8A) horizontal shaft (16A) fixed on both sides with horizontal shaft plate (16), one set of two, using a bite series full blade impeller turbine, approaching magnetic bearing load 0 approach + super high speed circumference Horizontal full blade ratio critical material gravity turbine (8U) 41-60 sets of power generation electrical product drive + double-sided center support bearing load 0 approach counter-rotating production compressed air (28a) drive combined with various speeds Merger engine and merger method.   Cylindrical turbine blade group (8A) horizontal shaft (16A) fixed on both sides with horizontal shaft plate (16), one set of two, using a bite series full blade impeller turbine, approaching magnetic bearing load 0 approach + super high speed circumference Horizontal full blade ratio critical material gravity turbine (8U) 61-80 sets of power generation electric product drive + double-side center support bearing load 0 approach counter-rotating production compressed air (28a) drive combined with various speeds Merger engine and merger method.   Cylindrical turbine blade group (8A) horizontal shaft (16A) fixed on both sides with horizontal shaft plate (16), one set of two, using a bite series full blade impeller turbine, approaching magnetic bearing load 0 approach + super high speed circumference Horizontal full blade ratio material gravity turbine (8U) 81-100 sets of power generation electric product drive + double side center support bearing load 0 approach counter rotating production compressed air (28a) drive combined with various speeds Merger engine and merger method.   Cylindrical turbine blade group (8A) horizontal shaft (16A) fixed on both sides with horizontal shaft plate (16), one set of two, using a bite series full blade impeller turbine, approaching magnetic bearing load 0 approach + super high speed circumference Horizontal total blade ratio critical material gravity turbine (8U) 101-120 sets of power generation electric product drive + double-sided center support bearing load 0 approach counter-rotating production compressed air (28a) drive combined with various speeds Merger engine and merger method.   Cylindrical turbine blade group (8A) horizontal shaft (16A) fixed on both sides with horizontal shaft plate (16), one set of two, using a bite series full blade impeller turbine, approaching magnetic bearing load 0 approach + super high speed circumference Horizontal full blade ratio critical material gravity turbine (8U) 121-140 set generator electric product drive + both sides center support bearing load 0 approach counter-rotating production compressed air (28a) drive combined with various speeds Merger engine and merger method.   Cylindrical turbine blade group (8A) horizontal shaft (16A) fixed on both sides with horizontal shaft plate (16), one set of two, using a bite series full blade impeller turbine, approaching magnetic bearing load 0 approach + super high speed circumference Horizontal total blade ratio critical material gravity turbine (8U) 141 to 160 sets of power generation electric product drive + double-side center support bearing load 0 approach counter-rotating production compressed air (28a) drive combined various energy storage cycles Merger engine and merger method.   Cylindrical turbine blade group (8A) horizontal shaft (16A) fixed on both sides with horizontal shaft plate (16), one set of two, using a bite series full blade impeller turbine, approaching magnetic bearing load 0 approach + super high speed circumference Horizontal total blade ratio critical material gravity turbine (8U) 161-180 sets of power generation electric product drive + both sides center support bearing load 0 approaching counter-rotating production compressed air (28a) driving combined various energy storage cycles Merger engine and merger method.   Cylindrical turbine blade group (8A) horizontal shaft (16A) fixed on both sides with horizontal shaft plate (16), one set of two, using a bite series full blade impeller turbine, approaching magnetic bearing load 0 approach + super high speed circumference Various energy storage cycles to combine the speed of the horizontal full blade ratio critical material gravity turbine (8U) 181 to 200 sets of power generation electric product drive + double-side center support bearing load 0 approaching counter-rotating production compressed air (28a) drive Merger engine and merger method.   Horizontally-moving blade ratio critical material gravity turbine (8U) extreme with solar heater (21) provided with buoyancy on the water surface and solar heated air with magnetic bearing load approaching 0 + super high speed circumferential speed Compressed one or more times with a simple compressor (3 s) of low-cost power generation electric drive, and heat-recovered liquid oxygen production machine (88h) with a high-pressure high-temperature water heating pipe (5H) for each compression, Liquid energy cold heat + hot water to superheated steam heat supply equipment (3D) feed drive + double-sided center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) drive coalescence various coalescence engines and coalescence methods.   A solar heater (21) is provided with buoyancy on the water surface, and a rotation support part (4f) for controlling rotation of the sunlight at right angles from east to west is provided, and the solar heating air is used as a magnetic bearing load. Horizontally moving blade ratio critical material gravity turbine (8U) with zero approach + super high speed circumferential speed (8U) Compressed one or more times with a simple compressor (3s) of extremely inexpensive power generation electric drive, high pressure hot water for each compression Heat recovery liquid oxygen production machine (88h) heat production with heating tube (5H), electricity + liquid air cold heat + hot water to superheated steam temperature heat supply equipment (3D) feed drive + both sides center support bearing load 0 approach 2 Various energy storage cycle coalescing engines and coalescence methods for driving inversion manufactured compressed air (28a) drive coalescence.   The solar heater (21) is provided with buoyancy on the water surface, and includes a rotation support part (4f) that controls rotation of the sunlight at a right angle from east to west, and includes a gear device (4d) and a roller (4e). ) As a cylindrical rotating part (77G), a device for controlling rotation of sunlight at a right angle in the vertical direction, and a horizontal full-blade ratio critical material gravity with solar-heated air approaching a magnetic bearing load of 0 and an ultra-high speed circumferential speed. Turbine (8U) Extremely inexpensive power generation electric drive, simple compressor (3s) compressed one or more times, and at each compression heat recovery liquid oxygen production machine (88h) heat production with high pressure high temperature water heating pipe (5H) Electricity + Liquid air cold heat + High temperature water to superheated steam heat supply equipment (3D) Feed drive + Both-side center support bearing load 0 approaching counter-rotating production Compressed air (28a) drive coalescence engine And coalescing 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) Compressed one or more times, heat recovery liquid oxygen production machine (88h) heat production with high pressure high temperature water heating pipe (5H) for each compression, electricity + liquid air cold heat + high temperature water to superheated steam heat supply equipment (3D ) Feed drive + center support shaft on both sides Various energy saving cycles combined engine and coalescence method to load 0 close counterrotating producing compressed air (28a) driven coalescence.   The solar heater (21) is provided with buoyancy on the water surface, and includes a rotation support part (4f) that controls rotation of the sunlight at a right angle from east to west, and includes a gear device (4d) and a roller (4e). ) As a cylindrical rotating part (77G) as a device for controlling the rotation of sunlight at a right angle in the vertical direction, and as a device for controlling rotation at a right angle in the east-west direction by using buoyancy. The air (28a) temperature is maximized, and the external air (28a) is also heated. Each air passage (28A) is a high temperature selective suction. Gravity turbine (8U) Extremely inexpensive power generation Electric drive, compressed by simple compressor (3s) one or more times, heat recovery liquid oxygen production machine (88h) heat production by high pressure high temperature water heating pipe (5H) for each compression Electric + liquid air Hot + hot water - superheated steam heat supply facilities (3D) feed drive + sides center support bearing various energy storage cycles combined engine and coalescence method to load 0 close counterrotating producing compressed air (28a) driven coalescence.   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, and heat-recovered liquid oxygen production machine (88h) with a high-pressure high-temperature water heating pipe (5H) for each compression, + Liquid air cold heat + High temperature water to superheated steam heat supply equipment (3D) feed drive + Double-sided center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) drive coalescence various coalescence engines and coalescence methods.   The solar heater (21) is provided with a circular railroad on a flat ground, and includes a rotation support portion (4f) for controlling and rotating the sunlight at a right angle from east to west, and the solar heating air is used as a magnetic bearing. Horizontal all-blade ratio critical material gravity turbine (8U) with zero load approach + super high speed circumferential speed (8U) Compressed one or more times with a simple compressor (3s) of extremely inexpensive power generation electric drive, high pressure and high temperature for each compression Heat recovery liquid oxygen production machine (88h) heat production with water heating pipe (5H), electricity + liquid air cooling + hot water to superheated steam temperature supply equipment (3D) feed drive + both sides center support bearing load 0 approach Various energy storage cycle coalescing engine and coalescence method for driving counter rotating manufactured compressed air (28a) drive coalescence.   The solar heater (21) is provided with a circular railroad on a flat ground, and includes a rotation support portion (4f) for controlling rotation of the sunlight at a right angle from east to west, and a gear device (4d) and a roller ( 4e) As a cylindrical rotating part (77G), it is a device that controls the rotation of sunlight at a right angle in the vertical direction. Gravity turbine (8U) Extremely inexpensive power generation Electric drive, compressed by simple compressor (3s) one or more times, heat recovery liquid oxygen production machine (88h) heat production by high pressure high temperature water heating pipe (5H) for each compression Electricity, liquid air cooling + hot water to superheated steam temperature supply equipment (3D) feed drive + both sides center support bearing load 0 approaching counter-rotating production compressed air (28a) drive coalescence Organization 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) is used as a cylindrical rotating part (77G) as a device for controlling and rotating sunlight at a right angle in the vertical direction, and as a device for controlling rotation at a right angle in the east and west direction by using a circular railway, sunlight is linearly centered on the heat absorption tube (4H). Irradiated internal air (28a) maximum temperature, magnetically utilized bearing load approaching 0 + super-high speed circumferential speed horizontal full blade ratio critical material gravity turbine (8U) extremely low cost electric drive, simple compressor (3s ) 1 to several times, and at each compression, heat recovery liquid oxygen production machine (88h) is produced with a high-pressure high-temperature water heating pipe (5H), and electricity + liquid air cold heat + high-temperature water to superheated steam heat supply equipment (3D) Feed drive + both sides Various energy saving cycles combined engine and coalescence process for the support bearing load 0 close counterrotating producing compressed air (28a) driven coalescence.   The solar heater (21) is provided with a circular railroad on a flat ground, and includes a rotation support portion (4f) for controlling rotation of the sunlight at a right angle from east to west, and a gear device (4d) and a roller ( 4e) is used as a cylindrical rotating part (77G) as a device for controlling and rotating sunlight at a right angle in the vertical direction, and as a device for controlling rotation at a right angle in the east and west direction by using a circular railway, sunlight is linearly centered on the heat absorption tube (4H). Horizontal all-blade specific gravity with maximum magnetic bearing load approaching 0 + super high speed circumferential speed, with the highest temperature of the irradiated internal air (28a), and the external air (28a) also heating each air passage (28A) high temperature selective suction Large material gravity turbine (8U) Compressed one or more times with a simple compressor (3s) of extremely inexpensive power generation electric drive, and heat recovery liquid oxygen production machine (88h) with high-pressure high-temperature water heating pipe (5H) for each compression Thermal production, electricity + Body air cold + hot water - superheated steam heat supply facilities (3D) feed drive + sides center support bearing load 0 close counterrotating producing compressed air (28a) various energy conservation cycle combined engine and coalescence process for the driving coalesce.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Liquid oxygen (5K) receiving drive + both center support bearing load 0 approaching counter-rotating production compressed air (28a) driven various energy storage cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Liquid oxygen (5K) superheated steam (50) receiving drive + both center support bearing load 0 approaching counter-rotating production compressed air (28a) driven various energy storage cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Liquid oxygen (5K) superheated steam (50) received in multiple theoretical combustion chambers (4Q) + Double-side center support bearing load 0 approaching counter-rotating production Compressed air (28a) Driven by various energy storage cycle coalescing 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) ) Liquid oxygen (5K) superheated steam (50) is supplied to a plurality of theoretical combustion chambers (4Q) combined drive + both-side center support bearing load 0 approaching counter-rotating production compressed air (28a) and various energy storage cycle combined 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) ) Liquid oxygen (5K) superheated steam (50) in multiple theoretical combustion chambers (4Q) Combined rocket combustion drive + Double-side center support bearing load 0 approaching counter-rotating production Compressed air (28a) Driven by various energy storage cycle coalescence Organization and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Liquid oxygen (5K) superheated steam (50) is supplied to multiple theoretical combustion chambers (4Q) Combined rocket combustion additional drive + Double-side center support bearing load 0 approaching counter-rotating production Compressed air (28a) driven various energy storage cycles Merger engine and merger method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Liquid oxygen (5K) superheated steam (50) in multiple theoretical combustion chambers (4Q) Combined rocket combustion + jet combustion drive + both sides center support bearing load 0 approach counter-rotating production compressed air (28a) 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) ) Liquid oxygen (5K) superheated steam (50) received in multiple theoretical combustion chambers (4Q), rocket combustion, others are jet combustion + both sides center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) Energy conservation cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Liquid oxygen (5K) superheated steam (50) is received in multiple theoretical combustion chambers (4Q) by rocket combustion, and the other theoretical combustion chambers (4Q) are jet combustion + double-sided center support bearing load 0 approaching counter-rotating production compression 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) ) Liquid oxygen (5K) superheated steam (50) is received in multiple theoretical combustion chambers (4Q) by rocket combustion, and the other theoretical combustion chambers (4Q) are jet combustion driven + double-sided center support bearing load close to zero Various energy storage cycle coalescence engine and coalescence method for burning compressed air (28a).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) 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 + Both-side center support bearing load 0 approaching counter-rotating manufactured compressed air (28a ) Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88i) as a combustion 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 + both sides center support bearing load 0 approaching counter-rotating production compressed air (28a) combustion as simple gas engine (88i) Various energy storage cycle coalescence engines and coalescence methods for driving and driving a car.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) combustion as simple gas engine (88i) Various energy storage cycle coalescence engines and coalescence methods for driving and driving an automobile.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) 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 + Both-side center support bearing load 0 approaching counter-rotating manufactured compressed air (28a ) Various energy storage cycle coalescence engines and coalescence methods for storing in a simple gas engine (88i) drive generator (1) drive accumulator (1A) as combustion and driving the battery drive wheel (4J) rotating simple gas engine automobile (7k).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 bearing load 0 approaching counter-rotating production compressed air (28a) combustion as simple gas engine (88i) Various energy storage cycle coalescence engines and coalescence methods for storing power in a drive generator (1) drive battery (1A) and driving the battery drive wheel (4J) rotating simple gas engine vehicle (7k).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) combustion as simple gas engine (88i) Drive generator (1) Various energy storage cycle coalescence engine and coalescence method for storing in the drive battery (1A) and driving the battery drive wheel (4J) rotating simple gas engine vehicle (7k).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 + Both-side center support bearing load 0 approaching counter-rotating manufactured compressed air (28a ) Simple gas engine (88i) driven generator as combustion (1) Various energy storage to drive a simple gas engine car (7k) capable of rotating the storage battery drive wheel (4J) and normal wheel by accumulating in the drive storage battery (1A) 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 + both sides center support bearing load 0 approaching counter-rotating production compressed air (28a) combustion as simple gas engine (88i) Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine vehicle (7k) capable of rotating a storage battery drive wheel (4J) and rotating a normal wheel by accumulating in a drive generator (1) drive storage battery (1A).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) combustion as simple gas engine (88i) Drive generator (1) Various energy storage cycle coalescence engine and coalescence method for driving a simple gas engine vehicle (7k) capable of rotating in the battery drive wheel (4J) and normal wheel by accumulating in the drive accumulator (1A) .   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) 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 + Both-side center support bearing load 0 approaching counter-rotating manufactured compressed air (28a ) Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88i) as combustion and driving a simple gas engine automobile (7k).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 + Both-side center support bearing load 0 approaching counter-rotating manufactured compressed air (28a ) Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88i) as combustion and driving a screw (7C) rotating ship.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approaching counter-rotating production compressed air (28a) combustion as simple gas engine (88i) Various energy storage cycle coalescence engine and coalescence method for driving and driving a screw (7C) rotating ship.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) combustion as simple gas engine (88i) Various energy storage cycle coalescence engines and coalescence methods for driving and driving a screw (7C) rotating ship.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) 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 + Both-side center support bearing load 0 approaching counter-rotating manufactured compressed air (28a ) Various energy storage cycle coalescing engines and coalescence methods for driving a simple gas engine (88i) 1 to plural and driving a screw (7C) plural revolutions as a combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approaching counter-rotating production compressed air (28a) combustion as simple gas engine (88i) 1. Various energy storage cycle coalescing engine and coalescence method for driving a plurality of screws and driving a screw (7C) a plurality of rotations.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) combustion as simple gas engine (88i) Various energy storage cycle coalescence engines and coalescence methods that drive 1 to plural and drive 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) Ultra high pressure fuel combustion + Both-side center support bearing load 0 approaching counter-rotating manufactured compressed air (28a ) Various energy storage cycle coalescing engine and coalescence method for driving a simple gas engine (88i) 1 to multiple as combustion and driving a screw (7C) multi-turn simple gas engine ship (71).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 bearing load 0 approaching counter-rotating production compressed air (28a) combustion as simple gas engine (88i) Various energy storage cycle coalescing engine and coalescence method for driving one or more and driving a screw (7C) multiple rotation simple gas engine ship (7l).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) combustion as simple gas engine (88i) Various energy storage cycle coalescence engines and coalescence methods that drive 1 to plural and drive a screw (7C) multiple rotation simple gas engine ship (71).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 + Both-side center support bearing load 0 approaching counter-rotating manufactured compressed air (28a ) Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88i) as combustion and driving a simple gas engine ship (71).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 + Both-side center support bearing load 0 approaching counter-rotating manufactured compressed air (28a ) Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88i) as combustion and driving an injection propulsion ship such as a screw (7C) rotating simple water injection engine (88j).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 bearing load 0 approaching counter-rotating production compressed air (28a) combustion as simple gas engine (88i) Various energy storage cycle coalescence engines and coalescence methods for driving and driving a propulsion propulsion ship such as a screw (7C) rotating simple water injection engine (88j).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) combustion as simple gas engine (88i) Various energy storage cycle coalescence engines and coalescence methods for driving and driving a propulsion vessel such as a screw (7C) rotating simple water injection engine (88j).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 + Both-side center support bearing load 0 approaching counter-rotating manufactured compressed air (28a ) Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88i) 1 to a plurality of combustion and driving an injection propulsion ship such as a screw (7C) multiple rotation simple water injection engine (88j).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 bearing load 0 approaching counter-rotating production compressed air (28a) combustion as simple gas engine (88i) Various energy storage cycle coalescing engines and coalescence methods for driving one or more to drive an injection propulsion ship such as a screw (7C) multi-turn simple water injection engine (88j).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) combustion as simple gas engine (88i) Various energy storage cycle coalescence engines and coalescence methods for driving one or more to drive an injection propulsion ship such as a screw (7C) multiple rotation simple water injection engine (88j).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 + Both-side center support bearing load 0 approaching counter-rotating manufactured compressed air (28a ) Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88i) 1 to a plurality of combustion and driving an injection propulsion screw injection ship such as a screw (7C) multiple rotation simple water injection engine (88j).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 bearing load 0 approaching counter-rotating production compressed air (28a) combustion as simple gas engine (88i) Various energy storage cycle coalescing engines and coalescence methods for driving one or more to drive a screw (7C) multi-turn simple water injection engine (88j), etc.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) combustion as simple gas engine (88i) Various energy storage cycle coalescence engines and coalescence methods that drive one or more and drive a screw (7C) multi-rotation simple water injection engine (88j), 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) Ultra high pressure fuel combustion + Both-side center support bearing load 0 approaching counter-rotating manufactured compressed air (28a ) Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88i) as combustion and driving an injection propulsion screw injection ship such as a simple water injection engine (88j).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression (4Q) Multiple ultra-high pressure fuel combustion injection propulsion + Double-side center support bearing load 0 approaching counter-rotating production compression Various energy storage cycle coalescence engines and coalescence methods for driving an injection propulsion ship such as a simple water injection engine (88j) in which air (28a) is burned.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 that receives cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) multiple ultra high pressure fuel combustion injection propulsion + both sides center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) combustion Various energy storage cycle coalescence engines and coalescence methods for driving an injection propulsion ship such as an injection engine (88j).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) multiple ultra high pressure fuel combustion injection propulsion + both side center support bearing load 0 approaching counter-rotating production compressed air (28a) combustion Various energy storage cycle coalescing engines and coalescence methods for driving an injection propulsion ship such as a simple water injection engine (88j).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 sets the compression volume to 21/60000 of air compression. Various energy storage cycle coalescing engines and coalescence methods for driving an injection propulsion ship such as a simple water injection engine (88j) that uses compressed air (28a) combustion in close counter-rotating production.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) equipped with air suction flow path, multiple ultra high pressure fuel combustion injection propulsion + both sides center support bearing load 0 approach counter-rotating manufactured compressed air (28a ) Various energy storage cycle coalescing engines and coalescence methods for driving an injection propulsion ship such as a simple water injection engine (88j) as a combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) equipped with air suction flow path, multiple ultra high pressure fuel combustion injection propulsion + both sides center support bearing load 0 approaching counter reversal manufacturing compression Various energy storage cycle coalescence engines and coalescence methods for driving an injection propulsion ship such as a simple water injection engine (88j) in which air (28a) is burned.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 sets the compression volume to 21/60000 of air compression. Various energy storage cycle coalescence engines and coalescence methods for driving a simple water injection engine (88j), such as a simple water injection engine (88j), which is driven by a near counter-rotating manufactured compressed air (28a), and a ship (7n).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) equipped with air suction flow path, multiple ultra high pressure fuel combustion injection propulsion + both sides center support bearing load 0 approach counter-rotating manufactured compressed air (28a ) Combustion simple water injection engine (88j), etc. Injection propulsion simple water injection engine Ship (7n) 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) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) equipped with air suction flow path, multiple ultra high pressure fuel combustion injection propulsion + both sides center support bearing load 0 approaching counter reversal manufacturing compression Various energy storage cycle coalescence engines and coalescence methods for driving a simple water injection engine (88j), such as a simple water injection engine (88j), and a ship (7n) driven by air (28a) combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) which receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression + both center support bearing load 0 approaching counter-rotating production compressed air (28a) combustion Various energy storage cycle coalescence engines and coalescence methods for driving a simple water injection engine (88j), etc., and a simple water injection engine ship (7n).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of the air compression (4Q) Multiple ultra-high pressure fuel combustion injection propulsion + Double-side center support bearing load 0 approaching counter-rotating production compression Various energy storage cycle coalescing engine and coalescence method for making a simple injection engine (88k) injection propulsion airplane with 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) ) Simple injection with cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) multiple ultra high pressure fuel combustion injection propulsion + both sides center support bearing load 0 approaching counter-rotating production compressed air (28a) combustion Various energy storage cycle coalescing engines and coalescence methods for engine (88k) injection 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) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) multiple ultra high pressure fuel combustion injection propulsion + both side center support bearing load 0 approaching counter-rotating production compressed air (28a) combustion Various energy storage cycle coalescing engine and coalescence method to make a simple injection engine (88k) 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) ) Theoretical combustion chamber (4Q) which receives cheaper liquid oxygen (5K) and sets the compression volume to 21/60000 of air compression. Various energy storage cycle coalescing engine and coalescence method for making a simple injection engine (88k) injection propulsion airplane with combustion in close counter-rotating production compressed air (28a).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) equipped with air suction flow path, multiple ultra high pressure fuel combustion injection propulsion + both sides center support bearing load 0 approach counter-rotating manufactured compressed air (28a ) Combustion simple injection engine (88k) various energy storage cycle coalescing engine and coalescence method for injection propulsion airplane.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) equipped with air suction flow path, multiple ultra high pressure fuel combustion injection propulsion + both sides center support bearing load 0 approaching counter reversal manufacturing compression Various energy storage cycle coalescing engine and coalescence method for making a simple injection engine (88k) injection propulsion airplane with air (28a) combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) which receives cheaper liquid oxygen (5K) and sets the compression volume to 21/60000 of air compression. A simple injection engine (88k) injection propulsion simple injection engine plane (7o) driven by close counter-rotating manufactured compressed air (28a) combustion, and various energy storage cycle combination engines and combination 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) + electricity, theoretical combustion chamber (4Q) equipped with air suction flow path, multiple ultra high pressure fuel combustion injection propulsion + both sides center support bearing load 0 approach counter-rotating manufactured compressed air (28a ) Combustion simple injection engine (88k) injection propulsion simple injection engine airplane (7o) 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, theoretical combustion chamber (4Q) equipped with air suction flow path, multiple ultra high pressure fuel combustion injection propulsion + both sides center support bearing load 0 approaching counter reversal manufacturing compression Simple engine (88k) injection propulsion simple injection engine plane (7o) driven by air (28a) combustion 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) which receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression + both center support bearing load 0 approaching counter-rotating production compressed air (28a) combustion Various energy storage cycle coalescence engine and coalescence method for driving simple injection engine (88k) injection propulsion simple injection airplane (7o).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 + Both-side center support bearing load 0 approaching counter-rotating manufactured compressed air (28a ) Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88i) as combustion and driving a propeller (7A) rotating airplane.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approaching counter-rotating production compressed air (28a) combustion as simple gas engine (88i) Various energy storage cycle merging engines and merging methods for driving and driving a propeller (7A) rotating airplane.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) combustion as simple gas engine (88i) Various energy storage cycle coalescence engines and coalescence methods for driving and propeller (7A) rotating airplane drive.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) 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 + Both-side center support bearing load 0 approaching counter-rotating manufactured compressed air (28a ) Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88i) 1 to a plurality of propellers (7A) to drive a multi-rotation airplane as combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approaching counter-rotating production compressed air (28a) combustion as simple gas engine (88i) Various energy storage cycle coalescing 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 + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) combustion as simple gas engine (88i) Various energy storage cycle coalescing engines and coalescence methods for driving one to 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) ) 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 + Both-side center support bearing load 0 approaching counter-rotating manufactured compressed air (28a ) Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88i) 1 to multiple propulsion (7A) multiple rotation simple gas engine airplane (7m) as combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approaching counter-rotating production compressed air (28a) combustion as simple gas engine (88i) 1. Various energy storage cycle coalescing engine and coalescence method for driving a plurality of propellers (7A) and a multi-turn simple gas engine airplane (7m).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) combustion as simple gas engine (88i) Various energy storage cycle coalescing engines and coalescence methods in which one to plural driving and propeller (7A) plural rotation simple gas engine airplane (7m) are 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) ) 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 + Both-side center support bearing load 0 approaching counter-rotating manufactured compressed air (28a ) Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88i) as combustion and driving a propeller (7A) rotating simple gas engine airplane (7m).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 + Both-side center support bearing load 0 approaching counter-rotating manufactured compressed air (28a ) A simple gas engine (88i) driven rotor blade (7B) as a combustion and various energy storage cycle coalescing engines and coalescence methods that rotate and drive an airplane.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approaching counter-rotating production compressed air (28a) combustion as simple gas engine (88i) Various energy storage cycle coalescing engine and coalescence method for driving a rotating rotor blade (7B) 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 + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) combustion as simple gas engine (88i) Drive rotor (7B) Various energy storage cycle coalescence engine and coalescence method for rotating and driving an airplane.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression (4Q) Ultra high pressure fuel combustion + Both-side center support bearing load 0 approaching counter-rotating manufactured compressed air (28a ) Simple gas engine (88i) 1 to multiple drive rotor blades (7B) as combustion, various energy storage cycle coalescing engine and coalescence method for driving the airplane by plural revolutions.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approaching counter-rotating production compressed air (28a) combustion as simple gas engine (88i) 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 + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) combustion as simple gas engine (88i) 1 to multiple drive rotor blades (7B) various energy storage cycle coalescing engines and coalescing methods for driving the aircraft by plural revolutions.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression (4Q) Ultra high pressure fuel combustion + Both-side center support bearing load 0 approaching counter-rotating manufactured compressed air (28a ) Various energy storage cycle coalescing engines and coalescing methods for driving a simple gas engine (88i) 1 to a multi-drive rotor blade (7B) and driving a rotor blade airplane (7p) as a combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approaching counter-rotating production compressed air (28a) combustion as simple gas engine (88i) 1-multiple drive rotors (7B) various energy storage cycle coalescing engines and coalescing methods for driving a rotorcraft (7p) with multiple revolutions.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) combustion as simple gas engine (88i) 1 to multiple drive rotor blades (7B) various energy storage cycle coalescing engines and coalescence methods for driving the rotor blade airplane (7p) with multiple rotations.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) 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 + Both-side center support bearing load 0 approaching counter-rotating manufactured compressed air (28a ) Various energy storage cycle coalescence engine and coalescence method for driving a simple gas engine (88i) driven rotor blade (7B) as a combustion and rotating the rotor blade airplane (7p).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 + Both-side center support bearing load 0 approaching counter-rotating manufactured compressed air (28a ) Various energy storage cycle coalescing engine and coalescence method for rotating simple gas engine (88i) driving propeller (7A) as combustion and driving simple injection engine (88k) 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 + both sides center support bearing load 0 approaching counter-rotating production compressed air (28a) combustion as simple gas engine (88i) Various energy storage cycle coalescence engine and coalescence method for driving propeller (7A) to rotate and driving simple injection engine (88k) injection propulsion airplane.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) combustion as simple gas engine (88i) A driving propeller (7A), a simple injection engine (88k), and various energy storage cycle combining engines and combining 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) Ultra high pressure fuel combustion + Both-side center support bearing load 0 approaching counter-rotating manufactured compressed air (28a ) A simple gas engine (88i) 1 to a multiple drive propeller (7A) as a combustion, a simple injection engine (88k) injection propulsion airplane driving various energy storage cycle coalescence engine and a 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 + both sides center support bearing load 0 approaching counter-rotating production compressed air (28a) combustion as simple gas engine (88i) 1-multiple drive propeller (7A) various energy storage cycle coalescing engine and coalescence method for driving a simple injection engine (88k) injection propulsion airplane with multiple rotations.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) combustion as simple gas engine (88i) 1 to multiple drive propellers (7A) various rotations and simple injection engines (88k) various energy storage cycle coalescence engines and coalescence 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) Ultra high pressure fuel combustion + Both-side center support bearing load 0 approaching counter-rotating manufactured compressed air (28a ) Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88i) 1 to a multiple drive propeller (7A) as combustion and driving a simple injection engine (88k) injection propulsion simple gas engine airplane (7m) 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) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approaching counter-rotating production compressed air (28a) combustion as simple gas engine (88i) 1-multiple drive propeller (7A) various energy storage cycle coalescing engine and coalescence method for driving multiple injections, simple injection engine (88k) injection propulsion simple gas engine airplane (7m), etc.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) combustion as simple gas engine (88i) 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 (88k) injection propulsion simple gas engine airplanes (7m), 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) Ultra high pressure fuel combustion + Both-side center support bearing load 0 approaching counter-rotating manufactured compressed air (28a ) Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88i) drive propeller (7A) as combustion and driving a simple injection engine (88k) injection propulsion simple gas engine airplane (7m) and the like.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression (4Q) Ultra high pressure fuel combustion + Both-side center support bearing load 0 approaching counter-rotating manufactured compressed air (28a ) Various energy storage cycle coalescing engines and coalescence methods, in which combustion is performed and high pressure high temperature combustion gas (5M) is injected to drive a simple gas engine (88i).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 bearing load 0 approaching counter-rotating production compressed air (28a) combustion, high pressure high temperature combustion gas ( 5M) and a simple gas engine (88i) to drive 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) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double side center support bearing load 0 approaching counter-rotating production compressed air (28a) combustion, high pressure and high temperature Various energy storage cycle coalescence engines and coalescence methods for injecting combustion gas (5M) and driving a simple gas engine (88i).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 + Both-side center support bearing load 0 approaching counter-rotating manufactured compressed air (28a ) Various energy storage cycle coalescence engines and coalescence methods driven by a simple gas engine (88i) in which combustion is performed and high pressure high temperature combustion gas (5M) is injected and the horizontal axis (1h) is double-reversed.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approaching counter-rotating production compressed air (28a) combustion, high pressure high temperature combustion gas ( 5M) is injected, and the horizontal axis (1h) is a simple gas engine (88i) 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 + double side center support bearing load 0 approaching counter-rotating production compressed air (28a) combustion, high pressure and high temperature Various energy storage cycle coalescence engine and coalescence method driven by a simple gas engine (88i) which injects combustion gas (5M) and inverts the horizontal axis (1h).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) 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 + Both-side center support bearing load 0 approaching counter-rotating manufactured compressed air (28a ) Various energy storage cycle coalescence engines and coalescence methods, in which high pressure high temperature combustion gas (5M) is injected and the horizontal axis (1h) is driven by a plurality of contra-rotating simple gas engines (88i).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 bearing load 0 approaching counter-rotating production compressed air (28a) combustion, high pressure high temperature combustion gas ( 5M) and various energy storage cycle coalescence engines and coalescence methods for driving a horizontal axis (1h) a plurality of counter-rotating simple gas engines (88i).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 bearing load 0 approaching counter-rotating production compressed air (28a) combustion, high pressure and high temperature Various energy storage cycle coalescence engines and coalescence methods in which combustion gas (5M) is injected to drive a plurality of simple gas engines (88i) on 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) ) 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 + Both-side center support bearing load 0 approaching counter-rotating manufactured compressed air (28a ) Various energy storage cycle coalescence engines and coalescence methods, in which high pressure high temperature combustion gas (5M) is injected and the horizontal axis (1h) is driven by a plurality of contra-rotating simple gas engines (88i).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 + Both-side center support bearing load 0 approaching counter-rotating manufactured compressed air (28a ) Various energy storage cycle coalescing engines and coalescence methods that make a simple gas engine (88i) as combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approaching counter-rotating production compressed air (28a) combustion as simple gas engine (88i) Various energy storage cycle coalescence engines and coalescence methods.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) combustion as simple gas engine (88i) 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 + Both-side center support bearing load 0 approaching counter-rotating manufactured compressed air (28a ) Various energy storage cycle coalescing engines and coalescence methods for a simple gas engine (88i) that maximizes combustion speed.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Simple gas that receives cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double-sided center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) combustion and maximum speed Various energy storage cycle coalescing engines and coalescence methods for the engine (88i).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 bearing load 0 approaching counter-rotating manufactured compressed air (28a) combustion to maximum speed Various energy storage cycle coalescence engine and coalescence method to make a simple gas engine (88i).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 + Both-side center support bearing load 0 approaching counter-rotating manufactured compressed air (28a ) Various energy storage cycle coalescing engine and coalescence method for a simple gas engine (88i) with maximum driving speed as combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) super high pressure fuel combustion + double-sided center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) combustion to the maximum driving speed Various energy storage cycle coalescence engine and coalescence method for gas engine (88i).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 bearing load 0 approaching counter-rotating manufactured compressed air (28a) combustion, maximum driving speed Various energy storage cycle coalescence engine and coalescence method to be a simple gas engine (88i).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 + Both-side center support bearing load 0 approaching counter-rotating manufactured compressed air (28a ) Various energy storage cycle coalescing engine and coalescence method to make a simple gas engine (88i) with maximum speed as combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber 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-side center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) Combustion 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) ) 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. Combustion chamber (4Q) + both center support bearing load 0 approaching counter-rotating production compressed air (28a) Combustion engine for various energy storage cycles and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + 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 engines and coalescence methods for burning the combustion chamber (4Q) + both sides center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K), 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 coalescing engine and coalescence method for burning inversion manufactured compressed air (28a).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) + 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) + approach both sides center support bearing load 0 Various energy storage cycle coalescing engine and coalescence method for burning counter-rotating manufactured compressed air (28a).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) 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 coalescing engine and coalescence method for burning compressed air (28a) with zero load approaching counter-rotating production.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K), 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 the reverse production 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) + 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) + approach both sides center support bearing load 0 Various energy storage cycle coalescence engines and coalescence methods that open the contra-rotating manufactured compressed air (28a) combustion oxygen injection nozzle (6L) + fuel injection nozzle (6X) + superheated steam injection nozzle (6A).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) 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 load 0 approaching counter-rotating production 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 close counter-rotating manufactured 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 Centered support bearing load 0 approaching counter-rotating production Compressed air (28a) Two kinds of theoretical combustion chambers (4Q) to burn 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) + 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 sides center support bearing load 0 approaching counter-rotating production Compressed air (28a) Two types of theoretical combustion chambers (4Q) to burn 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) + 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-sided center support bearing load 0 approaching counter-rotating production compressed air (28a) to make two kinds of theoretical combustion chambers (4Q), 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 + Both-side center support bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion 2 types of theoretical combustion chamber (4Q) Various energy storage cycle coalescing engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) + electricity, open heated oxygen injection nozzle (6L) + fuel injection nozzle (6X) + superheated steam injection nozzle (6A) to the optimum temperature + heat superheated steam (50) High temperature + Both side center support bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion 2 types of theoretical combustion chamber (4Q) Various energy storage cycle coalescing engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) + electricity + hot water, open heated oxygen injection nozzle (6L) + fuel injection nozzle (6X) + superheated steam injection nozzle (6A) to the optimum temperature + superheated steam (50 ) Is heated to high temperature + both-side center support bearing load 0 approaching counter-rotating production compressed air (28a) combustion 2 types of theoretical combustion chamber (4Q) various energy storage cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K), open heated oxygen injection nozzle (6L) + fuel injection nozzle (6X) + superheated steam injection nozzle (6A) to the optimum temperature + heat superheated steam (50) + Double-sided center support bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion 2 types of theoretical combustion chamber (4Q) Various energy storage cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) + electricity, open heated oxygen injection nozzle (6L) + fuel injection nozzle (6X) + superheated steam injection nozzle (6A) to the optimum temperature + heat superheated steam (50) + Both-side center support bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion 2 types of theoretical combustion chamber (4Q) Various energy storage cycle coalescing engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) + electricity + hot water, open heated oxygen injection nozzle (6L) + fuel injection nozzle (6X) + superheated steam injection nozzle (6A) to the optimum temperature + superheated steam (50 ) + Both sides center support bearing load 0 approaching counter-rotating production compressed air (28a) Combustion 2 types of theoretical combustion chamber (4Q) various energy storage cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + hot water, open heated oxygen injection nozzle (6L) + fuel injection nozzle (6X) + superheated steam injection nozzle (6A) to the optimum temperature. Heating peripheral superheated steam (50) including received superheated steam by combustion at ℃ or higher + Both sides center support bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion 2 types of theoretical combustion chamber (4Q) 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) ) Receiving cheaper liquid oxygen (5K), high-pressure high-temperature combustion gas (5M) with multiple theoretical combustion chambers (4Q) Accelerated injection + double-side center support bearing load 0 approach counter-rotating manufactured compressed air (28a) Various energy storage cycle coalescence engine and coalescence method in a simple water injection engine (88j) for combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Received cheaper liquid oxygen (5K) + electricity, high-pressure high-temperature combustion gas (5M) injection accelerated injection with multiple theoretical combustion chambers (4Q) + double-side center support bearing load 0 approaching counter-rotating manufactured compressed air ( 28a) Combining various energy storage cycle engines and combining methods in a simple water injection engine (88j) for combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, high pressure high temperature combustion gas (5M) injection acceleration injection with multiple theoretical combustion chambers (4Q) + double side center support bearing load 0 approaching counter-rotating Compressed air (28a) combustion simple water injection engine (88j) 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) and use high pressure high temperature combustion gas (5M) with multiple theoretical combustion chambers (4Q) (4Q) oxygen + fuel + superheated steam on the inner wall + Both energy saving cycle coalescence engine and coalescence method made into a simple water injection engine (88j) combusting compressed air (28a) on both sides center support bearing load 0 approaching counter-rotating production.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, and heating the oxygen + fuel + superheated steam on the inner wall (4Q) with high pressure and high temperature combustion gas (5M) with multiple theoretical combustion chambers (4Q) Use + Double-sided center support bearing load 0 approaching counter-rotating production Compressed air (28a) Simple water injection engine (88j) combusting 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) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, high pressure high temperature combustion gas (5M) with multiple theoretical combustion chambers (4Q) (4Q) inner wall oxygen + fuel + superheated steam at optimum temperature Heating and use + both center support bearing load 0 approaching counter-rotating production compressed air (28a) various energy storage cycle coalescing engine and coalescence method for combusting simple water injection engine (88j).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 a simple water injection engine (88j) for theoretical combustion chamber (4Q) combustion + both center support bearing load 0 approaching counter-rotating production compressed air (28a) combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, and heating the oxygen + fuel + superheated steam on the inner wall (4Q) with high pressure and high temperature combustion gas (5M) with multiple theoretical combustion chambers (4Q) Various energy storage cycle coalescence engine and coalescence method in a simple water injection engine (88j) for theoretical combustion chamber (4Q) combustion + both center support bearing load 0 approaching counter-rotating production compressed air (28a) combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, high pressure high temperature combustion gas (5M) with multiple theoretical combustion chambers (4Q) (4Q) inner wall oxygen + fuel + superheated steam at optimum temperature Various energy storage cycle coalescence engines and coalescence methods that are heated to a theoretical combustion chamber (4Q) combustion + both center support bearing load 0 approaching counter-rotating production compressed air (28a) combustion into a simple water injection engine (88j).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Superheated steam that receives low-priced liquid oxygen (5K) + high-temperature water, and includes high-pressure high-temperature combustion gas (5M) having a plurality of theoretical combustion chambers (4Q) (4Q) oxygen + fuel on the inner wall + received high-temperature water Various energy storage cycle coalescence engines and coalescence with a simple water injection engine (88j) that heats the chamber to the theoretical combustion chamber (4Q) combustion + both center support bearing load 0 approaching counter-rotating production compressed air (28a) combustion Method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K), heat oxygen + fuel + superheated steam at the inner wall at the optimum temperature, theoretical combustion chamber (4Q) combustion + both sides center support bearing load 0 approach counter-rotating manufactured compressed air (28a ) Various energy storage cycle coalescing engine and coalescence method in a simple water injection engine (88j) for combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity, heating oxygen + fuel + superheated steam at the optimum temperature on the inner wall, theoretical combustion chamber (4Q) combustion + both-side center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) Various energy storage cycle coalescing engines and coalescence methods for a simple water injection engine (88j) for combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) + electricity + hot water, heat oxygen + fuel + superheated steam on the inner wall at optimal temperature, theoretical combustion chamber (4Q) combustion + both sides center support bearing load 0 approach double reversal Various energy storage cycle coalescing engine and coalescence method in a simple water injection engine (88j) for combustion of compressed air (28a) manufactured.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K), heat oxygen + fuel + superheated steam on the inner wall at the optimum temperature and burn the theoretical combustion chamber (4Q) + both sides center support bearing load 0 approaching counter-rotating manufactured compressed air ( 28a) Combining various energy storage cycle engines and combining methods in a simple water injection engine (88j) for combustion.   Magnetically utilized bearing load approaching 0 + super high speed circumferential speed horizontal + both sides center support bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion blade ratio critical material gravity turbine (8U) The theoretical combustion chamber with electricity + liquid air cooling + hot water to superheated steam temperature supply equipment (3D) receiving cheap liquid oxygen (5K) + electricity, and heating oxygen + fuel + superheated steam at the optimum temperature on the inner wall (4Q) Combustion + Both-side center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) Various energy storage cycle coalescing engine and coalescence method made into a simple water injection engine (88j) for combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, and heating oxygen + fuel + superheated steam on the inner wall at the optimum temperature to burn the theoretical combustion chamber (4Q) + double-sided center support bearing load close to 0 Various energy storage cycle coalescing engine and coalescence method in a simple water injection engine (88j) for inversion manufactured compressed air (28a) combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K), heat oxygen + fuel + superheated steam at the optimal temperature on the inner wall, and heat superheated steam (50) in the high-temperature water heating pipe (5H) by theoretical combustion chamber (4Q) combustion Various energy storage cycle coalescing engines and coalescence methods that are made into a simple water injection engine (88j) that burns with injection + both center support bearing load 0 approaching counter-rotating production compressed air (28a).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Received cheaper liquid oxygen (5K) + electricity, 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 coalescing engine and coalescence method, which is a simple water injection engine (88j) that burns heated injection + both center support bearing load 0 approaching counter-rotating production compressed air (28a).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) + electricity + hot water, heat oxygen + fuel + superheated steam at the inner wall at the optimum temperature, and heat the hot water heated pipe (5H) in the theoretical combustion chamber (4Q) combustion Various energy storage cycle coalescence engine and coalescence method (50), which is a simple water injection engine (88j) that burns heated injection + double side center support bearing load 0 approaching counter-rotating manufactured compressed air (28a).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) + hot water, heat oxygen + fuel + superheated steam on the inner wall at the optimum temperature, and receive hotheat steam received in the hot water heating pipe (5H) in the theoretical combustion chamber (4Q) combustion Various energy storage cycle coalescence engines and coalescence methods comprising a simple water injection engine (88j) that burns superheated steam (50) including heated injection + double-sided center support bearing load 0 approaching counter-rotating manufactured compressed air (28a).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K), air (28a) suction injection flow optimal location also with multiple theoretical combustion chambers (4Q) combustion injection + both sides center support bearing load 0 approaching counter-rotating production compression Various energy storage cycle coalescing engines and coalescing methods in a simple water injection engine (88j) 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) ) Receiving cheaper liquid oxygen (5K) + electricity, and air (28a) suction injection flow at the optimum location as well as multiple theoretical combustion chambers (4Q) combustion injection + double side center support bearing load 0 approach double reversal Manufacture compressed air (28a), a simple water injection engine (88j) that burns, 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) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, the air (28a) suction injection flow at the optimum location as well as multiple theoretical combustion chambers (4Q) combustion injection + both sides center support bearing load approach 0 Various energy storage cycle coalescing engine and coalescence method in the form of a simple water injection engine (88j) that burns counter-rotating manufactured compressed air (28a).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K), making it a simple water injection engine (88j), forward air inlet + both sides center support bearing load 0 approaching counter-rotating manufactured compressed air (28a) and burning various energy storage cycles Merger engine and merger method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Cheaper liquid oxygen (5K) + Electricity received + Both sides center support bearing load 0 approaching counter-rotating production Compressed air (28a) burned to make simple water injection engine (88j) and various energies forward of the air 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) ) Cheaper liquid oxygen (5K) + Electricity + High temperature water received + Both sides center support bearing load 0 approaching counter-rotating production Compressed air (28a) burned to make a simple water injection engine (88j) forward air inlet Various energy storage cycle coalescence engines and coalescence methods.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) + Both sides center support bearing load 0 approaching counter-rotating production Compressed air (28a) burns to make a simple water injection engine (88j) 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) ) Cheaper liquid oxygen (5K) + receiving electricity + both sides center support bearing load 0 approaching counter-rotating production Compressed air (28a) burns to make a simple water injection engine (88j), straight forward with air inlet Various energy storage cycle coalescing engine and coalescence method for injecting the maximum amount of bubbles to the bottom of the ship.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Cheaper liquid oxygen (5K) + Electricity + High temperature water received + Both sides center support bearing load 0 approaching counter-rotating production Compressed air (28a) burned to make a simple water injection engine (88j) forward air inlet Then, various energy storage cycle coalescing engines and coalescing methods in which bubbles are maximally injected to the bottom of the ship close to a straight line.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Less expensive liquid oxygen (5K) + High temperature water received + Both sides center support bearing load 0 approaching counter-rotating production Compressed air (28a) burned to make a simple water injection engine (88j) forward air inlet Various energy storage cycle coalescing engine and coalescence method for approaching a straight line and injecting the maximum amount of bubbles to the ship bottom   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) + Both sides center support bearing load 0 approaching counter-rotating production Compressed air (28a) combustion, high pressure high temperature combustion gas (5M) equipped with two kinds of theoretical combustion chambers (4Q) Various energy storage cycle coalescing engine and coalescence method, which is a simple injection engine (88k) of injection acceleration injection.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Less expensive liquid oxygen (5K) + receiving electricity + both sides center support bearing load 0 approaching counter-rotating production Compressed air (28a) burned high pressure high temperature combustion gas (2Q) with multiple theoretical combustion chambers (4Q) ( 5M) Various energy storage cycle coalescing engines and coalescence methods that are simple injection engines (88k) for injection acceleration injection.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Cheaper liquid oxygen (5K) + Electricity + High temperature water received + Both sides center support bearing load 0 approaching counter-rotating production Compressed air (28a) burned, high pressure high temperature equipped with two kinds of theoretical combustion chambers (4Q) Various energy storage cycle coalescing engine and coalescence method, which is a simple injection engine (88k) of combustion gas (5M) injection acceleration injection.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) + Both sides center support bearing load 0 approaching counter-rotating production Compressed air (28a) combustion, high pressure high temperature combustion gas (5M) equipped with two kinds of theoretical combustion chambers (4Q) (4Q) Various energy storage cycle coalescing engine and coalescence method, which is a simple injection engine (88k) that uses oxygen + fuel + superheated steam on the inner wall at the optimum temperature.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Less expensive liquid oxygen (5K) + receiving electricity + both sides center support bearing load 0 approaching counter-rotating production Compressed air (28a) burned high pressure high temperature combustion gas (2Q) with multiple theoretical combustion chambers (4Q) ( 5M) and (4Q) various energy storage cycle coalescence engines and coalescence methods, which are simple injection engines (88k) that use oxygen + fuel + superheated steam on the inner wall at an optimum temperature.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Cheaper liquid oxygen (5K) + Electricity + High temperature water received + Both sides center support bearing load 0 approaching counter-rotating production Compressed air (28a) burned, high pressure high temperature equipped with two kinds of theoretical combustion chambers (4Q) Various energy storage cycle coalescence engines and coalescence methods, which are simple injection engines (88k) using combustion gas (5M) with (4Q) 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) ) Receive cheaper liquid oxygen (5K) + Both sides center support bearing load 0 approaching counter-rotating production Compressed air (28a) combustion, high pressure high temperature combustion gas (5M) equipped with two kinds of theoretical combustion chambers (4Q) (4Q) Various energy storage cycle coalescing engines and coalescence methods in which a simple injection engine (88k) is made by heating the optimum temperature of oxygen + fuel + superheated steam on the inner wall 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 bearing load 0 approaching counter-rotating production Compressed air (28a) burned high pressure high temperature combustion gas (2Q) with multiple theoretical combustion chambers (4Q) ( 5M) (4Q) Various energy storage cycle coalescence engines and coalescence methods in which a simple injection engine (88k) 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) ) Cheaper liquid oxygen (5K) + Electricity + High temperature water received + Both sides center support bearing load 0 approaching counter-rotating production Compressed air (28a) burned, high pressure high temperature equipped with two kinds of theoretical combustion chambers (4Q) Various energy storage cycle coalescence engines which are made into a simple injection engine (88k) that uses oxygen (fuel) (5M), (4Q) inner wall oxygen + fuel + superheated steam to optimal temperature heating to make two types of theoretical combustion chamber (4Q) combustion, etc. 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) + High temperature water received + Both sides center support bearing load 0 approaching counter-rotating production Compressed air (28a) burned, high pressure high temperature combustion gas equipped with two kinds of theoretical combustion chambers (4Q) (5M) (4Q) Various energy storage cycles in which the superheated steam containing oxygen + fuel on the inner wall + fuel + received high-temperature water is heated to an optimal temperature to make two types of theoretical combustion chamber (4Q) combustion, etc. (88k) 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) ) Receive cheaper liquid oxygen (5K) + Both sides center support bearing load 0 approaching counter-rotating production Compressed air (28a) combustion, oxygen + fuel + superheated steam heated at optimum temperature on one kind of inner wall, two kinds Various energy storage cycle coalescence engine and coalescence method in a simple combustion engine (88k) 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) ) Cheaper liquid oxygen (5K) + receiving electricity + both sides center support bearing load 0 approaching counter-rotating production Compressed air (28a) burning, oxygen + fuel + superheated steam heated at the optimum temperature on one kind of inner wall Various energy storage cycle coalescing engines and coalescence methods in a simple injection engine (88k) of two types of theoretical combustion chamber (4Q) combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Cheaper liquid oxygen (5K) + Electricity + High temperature water received + Both sides center support bearing load 0 approaching counter-rotating production Compressed air (28a) burns, oxygen + fuel + superheated steam at one kind of inner wall at optimum temperature Various energy storage cycle coalescing engines and coalescence methods that are heated to a simple injection engine (88k) for combustion in two types of theoretical combustion chambers (4Q).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) + Both sides center support bearing load 0 approaching counter-rotating production Compressed air (28a) combustion, oxygen + fuel + superheated steam heated at optimum temperature on one kind of inner wall, two kinds Various energy storage cycle coalescence engine and coalescence method in a simple combustion engine (88k) 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) ) Cheaper liquid oxygen (5K) + receiving electricity + both sides center support bearing load 0 approaching counter-rotating production Compressed air (28a) burning, oxygen + fuel + superheated steam heated at the optimum temperature on one kind of inner wall 2 types of theoretical combustion chambers (4Q) various energy storage cycle coalescing engines and coalescence methods with simple injection engines (88k) for combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Cheaper liquid oxygen (5K) + Electricity + High temperature water received + Both sides center support bearing load 0 approaching counter-rotating production Compressed air (28a) burns, oxygen + fuel + superheated steam at one kind of inner wall at optimum temperature Various energy storage cycle coalescing engines and coalescence methods that are heated to a simple injection engine (88k) that burns two types of theoretical combustion chambers (4Q).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) + Both sides center support bearing load 0 approaching counter-rotating production Compressed air (28a) combustion, oxygen + fuel + superheated steam heated at optimum temperature on one kind of inner wall, two kinds Various energy storage cycle coalescence engines and coalescence methods that are simple injection engines (88k) 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) ) Cheaper liquid oxygen (5K) + receiving electricity + both sides center support bearing load 0 approaching counter-rotating production Compressed air (28a) burning, oxygen + fuel + superheated steam heated at the optimum temperature on one kind of inner wall Various energy storage cycle coalescence engines and coalescence methods that are simple injection engines (88k) that heat and inject superheated steam (50) of a high-temperature water heating pipe (5H) in two types of theoretical combustion chamber (4Q) combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Cheaper liquid oxygen (5K) + Electricity + High temperature water received + Both sides center support bearing load 0 approaching counter-rotating production Compressed air (28a) burns, oxygen + fuel + superheated steam at one kind of inner wall at optimum temperature Various energy storage cycle coalescence engines and coalescence methods that are heated and made into a simple injection engine (88k) that heats and injects superheated steam (50) of a high-temperature water heating pipe (5H) in two types of theoretical combustion chamber (4Q) combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Less expensive liquid oxygen (5K) + High temperature water received + Both sides center support bearing load 0 approaching counter-rotating production Compressed air (28a) burns and oxygen + fuel + superheated steam is heated at the optimum temperature on one kind of inner wall 2 types of theoretical combustion chamber (4Q) combustion, various energy storage cycle coalescence engine and coalescence method in a simple injection engine (88k) that heats and injects superheated steam (50) including superheated steam received in high temperature water heating pipe (5H) .   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) + Both sides center support bearing load 0 approaching counter-rotating production Compressed air (28a) burns, and air (28a) a plurality of theoretical combustion chambers at the optimum location of suction jet flow (4Q) Various energy storage cycle coalescence engines and coalescence methods that are simple injection engines (88k) 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) ) Cheaper liquid oxygen (5K) + Electricity received + Both sides center support bearing load 0 approaching counter-rotating production Compressed air (28a) burned, and air (28a) The suction jet flow at the most suitable place Combustion chamber (4Q) various energy storage cycle coalescing engine and coalescence method that is a simple injection engine (88k) that combusts and injects in the same manner.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Cheaper liquid oxygen (5K) + Electricity + High temperature water received + Both sides center support bearing load 0 approaching counter-rotating production Compressed air (28a) burned, and air (28a) suction jet flow at the optimal location 2 Various energy storage cycle coalescing engines and coalescence methods that are simple injection engines (88k) that combust and inject the same kind of theoretical combustion chamber (4Q) injectors.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + Both sides center support bearing load 0 approaching counter-rotating production Compressed air (28a) burned and rotated with simple injection engine (88k) to enable 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) ) Cheaper liquid oxygen (5K) + electricity received + both sides center support bearing load 0 approaching counter-rotating production Compressed air (28a) burned and rotated with simple injection engine (88k) to allow vertical ascent and descent 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) ) Less expensive liquid oxygen (5K) + Electricity + High temperature water received + Both sides center support bearing load 0 approaching counter-rotating production Compressed air (28a) burns and rotates with simple injection engine (88k) to cause vertical rise and fall Various energy storage cycle coalescence engines and coalescence methods made possible.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + Both sides center support bearing load 0 approaching counter-rotating production Compressed air (28a) burns and rotates with simple injection engine (88k) to enable various types of energy storage Cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Cheaper liquid oxygen (5K) + Electricity received + Both sides center support bearing load 0 approaching counter-rotating production Compressed air (28a) burned and rotated with simple injection engine (88k) to enable reverse injection Energy conservation cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Cheaper liquid oxygen (5K) + Electricity + High temperature water received + Both sides center support bearing load 0 approaching counter-rotating production Compressed air (28a) burns and rotates with simple injection engine (88k) to allow reverse injection Various energy storage cycle coalescence engines and coalescence methods.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + high temperature water + both center support bearing load 0 approaching counter-rotating production compressed air (28a) burning, rotating with simple injection engine (88k), enabling reverse injection Various energy storage cycle coalescence engines and coalescence methods.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Supplying electricity + hot water (52b) as liquid oxygen production, easy aiming to maximize suction speed, both sides center support bearing load of electric drive 0 approach simple multistage compressor (3t) + liquid oxygen production machine (88h) Various energy storage cycle coalescence engines and coalescence methods.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Supplying electricity as liquid oxygen production, easy aiming to maximize suction speed, both sides of electric drive center support bearing load 0 approach easy multistage compressor (3t) + liquid oxygen production machine (88h) various energy storage cycle coalescence 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) ) Electric + Superheated steam is supplied to produce liquid oxygen, easy aiming to maximize suction speed, electric drive both sides center support bearing load 0 approach easy multistage compressor (3t) + liquid oxygen production machine (88h) 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 + hot water (52b) as liquid oxygen production, easy aiming to maximize suction speed, both sides center support bearing load of electric drive 0 approaching easy multistage compressor (3t) + liquid oxygen production machine (88h) as liquid Various energy storage cycle coalescence engine and coalescence method for producing oxygen.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Supplying electricity as a liquid oxygen production, easy aiming to maximize the suction speed Electric drive both sides center support bearing load 0 approach simple multistage compressor (3t) + liquid oxygen production machine as a liquid oxygen production machine (88h) Various energy storage Cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) As an electric + superheated steam supply liquid oxygen production, easy aiming to maximize the suction speed of both sides of the electric drive center support bearing load 0 approach simple multistage compressor (3t) + liquid oxygen production machine (88h) to produce liquid oxygen Various energy storage cycle coalescence engines and coalescence methods.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Supplying electricity + hot water (52b) as liquid oxygen production, easy aiming to maximize suction speed, both sides center support bearing load of electric drive 0 approach simple multistage compressor (3t) + liquid oxygen production machine (88h) as air Various energy storage cycle coalescence engine and coalescence method for producing suction compression heat exchange superheated steam.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Supplying electricity as liquid oxygen production, easy aiming to maximize suction speed, both sides of electric drive center support bearing load 0 approaching simple multistage compressor (3t) + liquid oxygen production machine (88h) Various energy storage cycle coalescence engine and coalescence method for producing steam.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Electric + Superheated steam is supplied to produce liquid oxygen, easy aiming to maximize suction speed, both sides center support bearing of electric drive 0 approach easy multistage compressor (3t) + liquid oxygen production machine (88h) sucking and compressing air Various energy storage cycle coalescence engine and coalescence method for producing heat exchange superheated steam.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Electric + high-temperature water (52b) + superheated steam supply liquid oxygen production, easy aiming to maximize suction speed, both sides center support bearing load of electric drive 0 approach simple multistage compressor (3t) + liquid oxygen production machine (88h) ) Various energy storage cycle coalescence engine and coalescence method for producing compressed heat exchange superheated steam by sucking air.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Supplying electricity + hot water (52b) as liquid oxygen production, easy aiming to maximize suction speed, both sides center support bearing load of electric drive 0 approaching easy multistage compressor (3t) + liquid oxygen production machine (88h) as liquid Various energy storage cycle coalescence engines and coalescence methods for producing nitrogen.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Supplying electricity to produce liquid oxygen, easy aiming to maximize suction speed, both sides of electric drive center support bearing load 0 approach simple multistage compressor (3t) + liquid oxygen production machine (88h) various energy to produce liquid nitrogen Storage cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Supplying electricity + superheated steam to produce liquid oxygen, easy aiming to maximize suction speed, both sides center support bearing of electric drive 0 approach simple multistage compressor (3t) + liquid oxygen production machine (88h) to produce liquid nitrogen 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 + hot water (52b) as liquid oxygen production, easy aiming to maximize suction speed, both sides center support bearing load of electric drive 0 approaching easy multistage compressor (3t) + liquid oxygen production machine (88h) as liquid Various energy storage cycle coalescence engines and coalescence methods for supplying nitrogen to the production supply facility (3D).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Supplying electricity to produce liquid oxygen, easy aiming to maximize the suction speed Electric drive both sides center support bearing load 0 approach simple multistage compressor (3t) + liquid oxygen production machine (88h) to produce and supply liquid nitrogen ( 3D) various energy storage cycle coalescence engines and coalescence methods.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Supplying electricity + superheated steam to produce liquid oxygen, easy aiming to maximize suction speed, both sides center support bearing of electric drive 0 approach simple multistage compressor (3t) + liquid oxygen production machine (88h) to produce liquid nitrogen Various energy storage cycle coalescence engines and coalescence methods to be supplied to a supply facility (3D).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Supplying electricity + hot water (52b) as liquid oxygen production, easy aiming to maximize suction speed, both sides center support bearing load of electric drive 0 approaching easy multistage compressor (3t) + liquid oxygen production machine (88h) as liquid Various energy storage cycle coalescence engines and coalescence methods for supplying nitrogen + liquid oxygen + superheated steam to manufacturing and supply equipment (3D).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Supplying electricity as liquid oxygen production, easy aiming to maximize suction speed both sides center support bearing load of electric drive 0 approaching simple multistage compressor (3t) + liquid oxygen production machine (88h) as liquid nitrogen + liquid oxygen + superheat Various energy storage cycle coalescence engines and coalescence methods for supplying steam to the production and supply equipment (3D).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Electric + Superheated steam is supplied to produce liquid oxygen, easy target to maximize suction speed, both sides center support bearing load of electric drive 0 approach easy multistage compressor (3t) + liquid oxygen production machine (88h) as liquid nitrogen + liquid Various energy storage cycle coalescence engine and coalescence method for supplying oxygen + superheated steam to the production supply facility (3D).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Electric + high-temperature water (52b) + superheated steam supply liquid oxygen production, easy aiming to maximize suction speed, both sides center support bearing load of electric drive 0 approach simple multistage compressor (3t) + liquid oxygen production machine (88h) ) Various energy storage cycle coalescence engines and coalescence methods for supplying liquid nitrogen + liquid oxygen + superheated steam to the production supply facility (3D).   Horizontally-moving blade ratio critical material gravity turbine (8U) with ultra-high speed circumferential speed with magnetic utilization bearing load approaching 0 + double-sided center support bearing load approaching 0 multi-stage compressor (3t) + liquid Various energy storage cycle coalescence engines and coalescence methods configured to simplify the oxygen production machine (88h) and maximize the suction speed.   Horizontally-moving blade ratio critical material gravity turbine (8U) with ultra-high speed circumferential speed with magnetic utilization bearing load approaching 0 + double-sided center support bearing load approaching 0 multi-stage compressor (3t) + liquid Various energy storage cycle coalescence engines and coalescence methods that compress the air as a configuration that simplifies the oxygen production machine (88h) and maximizes the suction speed.   Horizontally-moving blade ratio critical material gravity turbine (8U) with ultra-high speed circumferential speed with magnetic utilization bearing load approaching 0 + double-sided center support bearing load approaching 0 multi-stage compressor (3t) + liquid Various energy storage cycle coalescence engines and coalescence methods for compressing air (28a) as a configuration that simplifies the oxygen production machine (88h) and maximizes the suction speed.   Horizontally-moving blade ratio critical material gravity turbine (8U) with ultra-high speed circumferential speed with magnetic utilization bearing load approaching 0 + double-sided center support bearing load approaching 0 multi-stage compressor (3t) + liquid Various energy storage cycle coalescence engines and coalescence methods for compressing one or more stages as a configuration that maximizes the suction speed by simplifying the oxygen production machine (88h).   Horizontally-moving blade ratio critical material gravity turbine (8U) with ultra-high speed circumferential speed with magnetic utilization bearing load approaching 0 + double-sided center support bearing load approaching 0 multi-stage compressor (3t) + liquid Various energy storage cycle coalescence engines and coalescence methods for heating one to several stages of compressed water as a configuration that simplifies the oxygen production machine (88h) and maximizes the suction speed.   Horizontally-moving blade ratio critical material gravity turbine (8U) with ultra-high speed circumferential speed with magnetic utilization bearing load approaching 0 + double-sided center support bearing load approaching 0 multi-stage compressor (3t) + liquid Various energy storage cycle coalescence engines and coalescence methods for heating one to several stages of compressed high-temperature water as a configuration that maximizes the suction speed by simplifying the oxygen production machine (88h).   Horizontally-moving blade ratio critical material gravity turbine (8U) with ultra-high speed circumferential speed with magnetic utilization bearing load approaching 0 + double-sided center support bearing load approaching 0 multi-stage compressor (3t) + liquid Various energy storage cycle coalescence engines and coalescence methods for heating 1 to multi-stage compressed superheated steam as a configuration that simplifies the oxygen production machine (88h) and maximizes the suction speed.   Horizontally-moving blade ratio critical material gravity turbine (8U) with ultra-high speed circumferential speed with magnetic utilization bearing load approaching 0 + double-sided center support bearing load approaching 0 multi-stage compressor (3t) + liquid Various energy storage cycle coalescence engines and coalescence methods for heating water with 1 to multi-stage compression as a configuration that simplifies the oxygen production machine (88h) and maximizes the suction speed.   Horizontally-moving blade ratio critical material gravity turbine (8U) with ultra-high speed circumferential speed with magnetic utilization bearing load approaching 0 + double-sided center support bearing load approaching 0 multi-stage compressor (3t) + liquid Various energy storage cycle coalescence engines and coalescence methods for heating high-temperature water by 1 to multi-stage compression as a configuration that simplifies the oxygen production machine (88h) and maximizes the suction speed.   Horizontally-moving blade ratio critical material gravity turbine (8U) with ultra-high speed circumferential speed with magnetic utilization bearing load approaching 0 + double-sided center support bearing load approaching 0 multi-stage compressor (3t) + liquid Various energy storage cycle coalescence engines and coalescence methods for heating superheated steam by 1 to multi-stage compression as a configuration that simplifies the oxygen production machine (88h) and maximizes the suction speed.   Horizontally-moving blade ratio critical material gravity turbine (8U) with ultra-high speed circumferential speed with magnetic utilization bearing load approaching 0 + double-sided center support bearing load approaching 0 multi-stage compressor (3t) + liquid Various energy storage cycle coalescence engines and coalescence methods for producing superheated steam by compression as a configuration that simplifies the oxygen production machine (88h) and maximizes the suction speed.   Horizontally-moving blade ratio critical material gravity turbine (8U) with ultra-high speed circumferential speed with magnetic utilization bearing load approaching 0 + double-sided center support bearing load approaching 0 multi-stage compressor (3t) + liquid Various energy storage cycle coalescence engines and coalescence methods that produce liquid oxygen + superheated steam by compression as a configuration that simplifies the oxygen production machine (88h) and maximizes the suction speed.   Horizontally-moving blade ratio critical material gravity turbine (8U) with ultra-high speed circumferential speed with magnetic utilization bearing load approaching 0 + double-sided center support bearing load approaching 0 multi-stage compressor (3t) + liquid Various energy storage cycle coalescence engines and coalescence methods for producing liquid oxygen + liquid nitrogen + superheated steam by compression as a configuration that simplifies the oxygen production machine (88h) and maximizes the suction speed.   Horizontally-moving blade ratio critical material gravity turbine (8U) with ultra-high speed circumferential speed with magnetic utilization bearing load approaching 0 + double-sided center support bearing load approaching 0 multi-stage compressor (3t) + liquid Various energy storage cycle coalescence engines and coalescence methods that produce liquid oxygen + liquid nitrogen + high temperature water by compression as a configuration that simplifies the oxygen production machine (88h) and maximizes the suction speed.   Horizontally-moving blade ratio critical material gravity turbine (8U) with ultra-high speed circumferential speed with magnetic utilization bearing load approaching 0 + double-sided center support bearing load approaching 0 multi-stage compressor (3t) + liquid Various energy storage cycle coalescence engines and coalescence methods for supplying the oxygen production machine (88h) to the liquid oxygen + superheated steam production / supply facility (3D) by compression as a configuration that maximizes the suction speed by simplifying the oxygen production machine (88h).   Horizontally-moving blade ratio critical material gravity turbine (8U) with ultra-high speed circumferential speed with magnetic utilization bearing load approaching 0 + double-sided center support bearing load approaching 0 multi-stage compressor (3t) + liquid Various energy storage cycle coalescence engine and coalescence method for supplying oxygen to liquid oxygen + liquid nitrogen + high pressure superheated steam production and supply equipment (3D) by compression as a configuration that simplifies the oxygen production machine (88h) and maximizes the suction speed.   Horizontally-moving blade ratio critical material gravity turbine (8U) with ultra-high speed circumferential speed with magnetic utilization bearing load approaching 0 + double-sided center support bearing load approaching 0 multi-stage compressor (3t) + liquid Various energy storage cycle coalescence engines and coalescence methods that supply the oxygen production machine (88h) to the liquid oxygen + liquid nitrogen + super high pressure superheated steam production / supply facility (3D) by compression as a configuration that simplifies the oxygen production machine (88h).   Horizontally-moving blade ratio critical material gravity turbine (8U) with ultra-high speed circumferential speed with magnetic utilization bearing load approaching 0 + double-sided center support bearing load approaching 0 multi-stage compressor (3t) + liquid Various energy storage cycle coalescence engines and coalescence methods that supply the oxygen production machine (88h) to the liquid oxygen + superhigh pressure superheated steam production and supply facility (3D) by compression as a configuration that simplifies the oxygen production machine (88h).   Horizontally-moving blade ratio critical material gravity turbine (8U) with ultra-high speed circumferential speed with magnetic utilization bearing load approaching 0 + double-sided center support bearing load approaching 0 multi-stage compressor (3t) + liquid Various energy storage cycle coalescence engines and coalescence methods that supply the oxygen production machine (88h) to the liquid oxygen + liquid nitrogen + super high pressure superheated steam production / supply facility (3D) by compression as a configuration that simplifies the oxygen production machine (88h).   Horizontally-moving blade ratio critical material gravity turbine (8U) with ultra-high speed circumferential speed with magnetic utilization bearing load approaching 0 + double-sided center support bearing load approaching 0 multi-stage compressor (3t) + liquid Various energy storage cycle coalescence engine and coalescence method for supplying oxygen + liquid oxygen + liquid nitrogen + super high pressure superheated steam production and supply equipment (3D) by compression as a configuration that simplifies the oxygen production machine (88h) and maximizes the suction 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 engine and coalescence method, in which low-cost liquid oxygen (5K) is received into a simple gas engine (88i) on both side center support bearing loads close to zero, and fuel injection combustion is performed in compressed air.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Various energy storage cycle coalescence engines and coalescence methods that make the two-sided center support bearing load zero approaching simple injection engine (88k) receive low-cost liquid oxygen (5K) and receive fuel injection combustion + compressed air fuel injection combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) More energy storage cycle coalescence engine with two types of theoretical combustion chambers: receiving low-cost liquid oxygen (5K) in a simple water injection engine (88j) on both sides center support bearing load (88j) and fuel injection combustion into compressed air 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) ) From both sides center support bearing load 0 approaching simple gas engine (88i) receiving cheap liquid oxygen (5K) fuel injection combustion + compressed air fuel injection combustion into two types of theoretical combustion chamber (4Q) 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) ) From both sides center support bearing load 0 approaching simple injection engine (88k) receiving cheap liquid oxygen (5K) fuel injection combustion + compressed air fuel injection combustion into two types of theoretical combustion chamber (4Q) and one type of opening and closing valve (1Q) 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) ) From both sides center support bearing load 0 approaching simple water injection engine (88j) receiving cheap liquid oxygen (5K) fuel injection combustion + compressed air fuel injection combustion into two types of theoretical combustion chamber (4Q), open and close at one type inlet Various energy storage cycle coalescence engine and coalescence method comprising a valve (1Q) oxygen injection nozzle (6L).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) From both sides center support bearing load 0 approaching simple gas engine (88i) receiving cheap liquid oxygen (5K) fuel injection combustion + compressed air fuel injection combustion into two types of theoretical combustion chamber (4Q) and one type of opening and closing valve (1Q) Various energy storage cycle coalescence engines and coalescence methods provided with an oxygen injection nozzle (6L) and a fuel injection nozzle (6X).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) From both sides center support bearing load 0 approaching simple injection engine (88k) receiving cheap liquid oxygen (5K) fuel injection combustion + compressed air fuel injection combustion into two types of theoretical combustion chamber (4Q) and one type of opening and closing valve (1Q) Oxygen injection nozzle (6L) Fuel injection nozzle (6X) Equipped with on-off valve (1Q) Various energy storage cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) From both sides center support bearing load 0 approaching simple water injection engine (88j) receiving cheap liquid oxygen (5K) fuel injection combustion + compressed air fuel injection combustion into two types of theoretical combustion chamber (4Q), open and close at one type inlet Valve (1Q) Oxygen injection nozzle (6L) Fuel injection nozzle (6X) Equipped with on-off valve (1Q) Closed oxygen fuel injection Combustion engine and combination method for various energy storage cycles.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) From both sides center support bearing load 0 approaching simple gas engine (88i) receiving cheap liquid oxygen (5K) fuel injection combustion + compressed air fuel injection combustion into two types of theoretical combustion chamber (4Q) and one type of opening and closing valve (1Q) Oxygen injection nozzle (6L) Fuel injection nozzle (6X) Equipped with on-off valve (1Q) Closed oxygen fuel injection Combustion rotation output increases various engine and engine 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) ) From both sides center support bearing load 0 approaching simple injection engine (88k) receiving cheap liquid oxygen (5K) fuel injection combustion + compressed air fuel injection combustion into two types of theoretical combustion chamber (4Q) and one type of opening and closing valve (1Q) Oxygen injection nozzle (6L) Fuel injection nozzle (6X) Open / close valve (1Q) Closed oxygen fuel injection Combustion rotation output increase 2 types (4Q) Superheated steam (50) Various energy storage cycle coalescence engine and coalescence method .   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) From both sides center support bearing load 0 approaching simple water injection engine (88j) receiving cheap liquid oxygen (5K) fuel injection combustion + compressed air fuel injection combustion into two types of theoretical combustion chamber (4Q), open and close at one type inlet Valve (1Q) Oxygen injection nozzle (6L) Fuel injection nozzle (6X) Open / close valve (1Q) Closed oxygen fuel injection Combustion rotation output increase 2 types (4Q) Superheated steam (50) injection and combustion gas (49) suction injection Various energy storage cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) From both sides center support bearing load 0 approaching simple gas engine (88i) receiving cheap liquid oxygen (5K) fuel injection combustion + compressed air fuel injection combustion into two types of theoretical combustion chamber (4Q) and one type of opening and closing valve (1Q) Oxygen injection nozzle (6L) Fuel injection nozzle (6X) Equipped with open / close valve (1Q) Closed oxygen fuel injection Combustion rotation output increase 2 types (4Q) Superheated steam (50) injection and suction injection injection of combustion gas (49) Various energy storage cycle coalescence engines and coalescence methods that increase propulsion output.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Both sides center support bearing load 0 approaching simple injection engine (88k) receiving cheap liquid oxygen (5K) fuel injection combustion + compressed air fuel injection combustion into two types of theoretical combustion chamber (4Q), opening and closing at one type inlet and outlet Various energy storage cycle coalescence engines and coalescence methods comprising a valve (1Q), an oxygen injection nozzle (6L), and a fuel injection nozzle (6X).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) From both sides center support bearing load 0 approaching simple water injection engine (88j) receiving cheap liquid oxygen (5K) fuel injection combustion + compressed air fuel injection combustion into two types of theoretical combustion chamber (4Q) and one type at the inlet and outlet On-off valve (1Q) Oxygen injection nozzle (6L) Fuel injection nozzle (6X) Equipped with on-off valve (1Q) various energy storage cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) From both sides center support bearing load 0 approach Easy gas engine (88i) receives cheap liquid oxygen (5K) fuel injection combustion + compressed air fuel injection combustion into two types of theoretical combustion chamber (4Q), open and close at one type inlet and outlet Valve (1Q) Oxygen injection nozzle (6L) Fuel injection nozzle (6X) Equipped with on-off valve (1Q) Closed oxygen fuel injection Combustion engine and combination method for various energy storage cycles.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Both sides center support bearing load 0 approaching simple injection engine (88k) receiving cheap liquid oxygen (5K) fuel injection combustion + compressed air fuel injection combustion into two types of theoretical combustion chamber (4Q), opening and closing at one type inlet and outlet Valve (1Q) Oxygen injection nozzle (6L) Fuel injection nozzle (6X) Open / close valve (1Q) Closed oxygen fuel injection combustion High pressure high temperature combustion gas (5M) various energy storage cycle coalescence engine and coalescence method .   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) From both sides center support bearing load 0 approach simple water injection engine (88j) low-cost liquid oxygen (5K) received fuel injection combustion + compressed air fuel injection combustion into two types of theoretical combustion chamber (4Q), open and close at one type inlet and outlet Valve (1Q) Oxygen injection nozzle (6L) Fuel injection nozzle (6X) Open / close valve (1Q) Closed oxygen fuel injection combustion High pressure high temperature combustion gas (5M) Outer periphery (6Y) Injected superheated steam (50) also outer periphery (6A) 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) ) Both sides center support bearing load 0 approach simple injection engine (88k) low cost liquid oxygen (5K) received 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 combustion High pressure high temperature combustion gas (5M) outer periphery (6Y) Rocket injection superheated steam (50) also outer periphery (6A) Various energy storage cycle coalescing engine and coalescence method for increasing rocket injection propulsion output.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) From both sides center support bearing load 0 approach simple water injection engine (88j) low-cost liquid oxygen (5K) received fuel injection combustion + compressed air fuel injection combustion into two types of theoretical combustion chamber (4Q), open and close at one type inlet and outlet Valve (1Q) Oxygen injection nozzle (6L) Fuel injection nozzle (6X) Open / close valve (1Q) Closed oxygen fuel injection combustion High pressure high temperature combustion gas (5M) outer periphery (6Y) Rocket injection superheated steam (50) also outer periphery (6A ) Various energy storage cycle coalescence engines and coalescence methods that increase rocket-injected water in front of 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) In-line co-rotating gear (4D) Electric drive solar heater (21) rotating on multiple turbines and generating electricity with multiple turbines + Double-side center support bearing load 0 approach simple multistage compressor ( 3t) + various energy storage cycle coalescence engine and coalescence method for liquid oxygen production machine (88h).   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) Rotating and generating electricity with multiple turbines Electric drive solar heater (21) + Both sides center support bearing load 0 approach easy multistage compressor (3t) + Liquid oxygen production Various energy storage cycle coalescence engine and coalescence method to make machine (88h).   Horizontally moving blade ratio critical material gravity turbine (8U) with a magnetic bearing load approaching 0 and super high speed circumferential speed. Ultra-high pressure vertically below the vacuum in the vacuum, accelerating gravitational acceleration and cylindrical turbine blade group (8A) horizontal Rotating shaft (16A) and cylindrical turbine blade group (8A) Electric drive solar heater (21) for multiple power generation + Both sides center support bearing load 0 approach easy multistage compressor (3t) + liquid oxygen production machine (88h) Various energy storage 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 Rotating shaft (16A) and cylindrical turbine blade group (8A) 20 sets of electric drive solar heater (21) + both sides center support bearing load 0 approach easy multistage compressor (3t) + liquid oxygen production machine (88h) Various energy storage cycle coalescence engines and coalescence methods.   Horizontally moving blade ratio critical material gravity turbine (8U) with a magnetic bearing load approaching 0 and super high speed circumferential speed. Ultra-high pressure vertically below the vacuum in the vacuum, accelerating gravitational acceleration and cylindrical turbine blade group (8A) horizontal Rotating shaft (16A) and cylindrical turbine blade group (8A) 40 sets of electric drive solar heater (21) + both sides center support bearing load 0 approach easy multistage compressor (3t) + liquid oxygen production machine (88h) Various energy storage cycle coalescence engines and coalescence methods.   Horizontally moving blade ratio critical material gravity turbine (8U) with a magnetic bearing load approaching 0 and super high speed circumferential speed. Ultra-high pressure vertically below the vacuum in the vacuum, accelerating gravitational acceleration and cylindrical turbine blade group (8A) horizontal Rotating shaft (16A) and cylindrical turbine blade group (8A) 80 sets of electric drive solar heater (21) + both sides center support bearing load 0 approach easy multistage compressor (3t) + liquid oxygen production machine (88h) Various energy storage cycle coalescence engines and coalescence methods.   Horizontally moving blade ratio critical material gravity turbine (8U) with a magnetic bearing load approaching 0 and super high speed circumferential speed. Ultra-high pressure vertically below the vacuum in the vacuum, accelerating gravitational acceleration and cylindrical turbine blade group (8A) horizontal Rotating shaft (16A) and cylindrical turbine blade group (8A) 100 sets of electric drive solar heater (21) + both sides center support bearing load 0 approach easy multistage compressor (3t) + liquid oxygen production machine (88h) Various energy storage cycle coalescence engines and coalescence methods.   Horizontally moving blade ratio critical material gravity turbine (8U) with a magnetic bearing load approaching 0 and super high speed circumferential speed. Ultra-high pressure vertically below the vacuum in the vacuum, accelerating gravitational acceleration and cylindrical turbine blade group (8A) horizontal Rotating shaft (16A) and cylindrical turbine blade group (8A) 150 sets of electric drive solar heater (21) + both sides center support bearing load 0 approach multistage compressor (3t) + liquid oxygen production machine (88h) Various energy storage cycle coalescence engines and coalescence methods.   Horizontally moving blade ratio critical material gravity turbine (8U) with a magnetic bearing load approaching 0 and super high speed circumferential speed. Ultra-high pressure vertically below the vacuum in the vacuum, accelerating gravitational acceleration and cylindrical turbine blade group (8A) horizontal Rotating shaft (16A) and cylindrical turbine blade group (8A) 200 sets of electric drive solar heater (21) + both sides center support bearing load 0 approach easy multistage compressor (3t) + liquid oxygen production machine (88h) Various energy storage cycle coalescence engines and coalescence methods.   Bearings with magnetic bearing load approaching 0 + super high speed circumferential speed with full blade ratio critical material gravity turbine (8U) power generation electric product + rocket combustion + jet combustion on both sides center support bearing load 0 approach simple water injection engine (88j ) Various energy storage cycle coalescence engines and coalescence methods that are driven equally.   Magnetically utilized bearing load approaching 0 + super high speed circumferential speed horizontal blade ratio critical material gravity turbine (8U) power generation electrical product + rocket combustion 2 places + jet combustion 2 places on both sides center support bearing load 0 approach simple water Various energy storage cycle coalescence engines and coalescence methods for driving an injection engine (88j) and the like.   Magnetically-enhanced bearing load approaching 0 + ultra-high speed peripheral blade ratio critical material gravity turbine (8U) power generation electrical product + 3 rocket combustion + jet combustion 3 places on both sides center support bearing load 0 approaching simple water Various energy storage cycle coalescence engines and coalescence methods for driving an injection engine (88j) and the like.   Magnetically utilized bearing load close to 0 + super high speed circumferential speed with full blade ratio critical material gravity turbine (8U) power generation electrical product + rocket combustion 4 locations + jet combustion 4 locations on both sides center support bearing load 0 approach simple water Various energy storage cycle coalescence engines and coalescence methods for driving an injection engine (88j) and the like.   Magnetically utilized bearing load close to 0 + super high speed circumferential speed with full blade ratio critical material gravity turbine (8U) power generation electrical product + rocket combustion 5 locations + jet combustion 5 locations on both sides center support bearing load 0 approach simple water Various energy storage cycle coalescence engines and coalescence methods for driving an injection engine (88j) and the like.   Magnetically-applied bearing load approaching 0 + ultra-high speed circumferential speed with full blade ratio critical material gravity turbine (8U) power generation electrical product + rocket combustion 6 places + jet combustion 6 places on both sides center support bearing load 0 approach simple water Various energy storage cycle coalescence engines and coalescence methods for driving an injection engine (88j) and the like.   Horizontally-moving blade ratio critical material gravity turbine (8U) power generation electric product + rocket combustion + jet combustion both sides center support bearing load 0 approach simple injection engine (88k) Various energy storage cycle coalescence engines and coalescence methods to be driven.   Magnetically-enhanced bearing load approaching 0 + ultra-high speed peripheral blade ratio critical material gravity turbine (8U) power generation electric product + two rocket combustion + jet combustion two places on both sides center support bearing load 0 approach simple injection Various energy storage cycle coalescence engine and coalescence method for driving the engine (88k).   Horizontally moving blade ratio critical material gravity turbine (8U) power generation electric product + 3 rocket combustion + 3 jet jets on both sides center support bearing load 0 approach and simple injection Various energy storage cycle coalescence engine and coalescence method for driving the engine (88k).   Magnetically-applied bearing load approaching zero + super high speed circumferential speed with full blade ratio critical material gravity turbine (8U) power generation electrical product + rocket combustion 4 places + jet combustion 4 places on both sides center support bearing load 0 approach simple injection Various energy storage cycle coalescence engine and coalescence method for driving the engine (88k).   Horizontally moving blade ratio critical material gravity turbine (8U) power generation electric product + 5 rocket combustion + 5 jet combustion on both sides center support bearing load 0 approach and simple injection Various energy storage cycle coalescence engine and coalescence method for driving the engine (88k).   Horizontally moving blade ratio critical material gravity turbine (8U) power generation electrical product + 6 rocket combustion + 6 jet combustion on both sides center support bearing load 0 approach and simple injection Various energy storage cycle coalescence engine and coalescence method for driving the engine (88k).   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 in which the maximum load of bubbles is injected into the bottom vertical parallel plate (9Q) using a simple water injection engine (88j) or the like driven simple water injection engine ship (7n).   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 engine and coalescence method for making the maximum injection of bubbles into the bottom vertical parallel plate (9Q) using a screw injection ship such as a simple water injection engine (88j) with a close bearing load.   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 have a bearing load 0 approach simple water injection engine (88j), etc., drive a simple water injection engine ship (7n) and have a wide bottom bottom parallel plate (9Q) to maximize the air flying height.   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 which make the bearing load 0 approach simple water injection engine (88j), etc., drive screw injection ship, and have a wide bottom bottom parallel plate (9Q) to maximize the air floating amount.   Horizontal type full blade ratio material gravity turbine (8U) Receives low-priced liquid oxygen (5K) from electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D), extremely low-priced electricity production, supports both sides centrally Various energy storage cycle coalescence engines and coalescence methods that have a bearing load 0 approach simple water injection engine (88j), etc., drive a simple water injection engine ship (7n) and have a wide vertical bottom plate (9Q) 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 water injection engine (88j), such as a simple water injection engine approaching a bearing load 0, and have a ship 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 storage cycle coalescing engine and coalescence method for simple injection engine (88k) rotating blade injection airplane (7q) with propulsion + both center support bearing load 0 approaching counter-rotating production compressed air (28a) combustion.   Horizontal all-blade ratio critical material gravity turbine (8U) power generation electric manufacturing, receiving liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) multiple ultra high pressure fuel combustion injection propulsion + both sides center support bearing load 0 approach Various energy storage cycle coalescing engine and coalescence method to make a simple injection engine (88k) rotary blade injection airplane (7q) with counter-rotating manufactured 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, theoretical combustion chamber (4Q) multiple ultra high pressure fuel combustion propulsion + both sides center support bearing Various energy conservation cycle coalescing engine and coalescence method to make a simple injection engine (88k) rotary blade injection airplane (7q) with zero load approaching counter-rotating production compressed air (28a) combustion.   Includes a theoretical combustion chamber (4Q) air suction flow path that receives liquid oxygen (5K) and produces a compression volume of 21/60000 of air compression, produced by a horizontal full blade ratio critical material gravity turbine (8U) generator Multiple ultra-high pressure fuel combustion injection propulsion + Both-side center support bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion simple injection engine (88k) Rotary blade injection plane (7q) Various energy storage cycle coalescence engine and coalescence Method.   Horizontal full-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity, equipped with theoretical combustion chamber (4Q) air suction channel, multiple ultra high pressure fuel combustion injection propulsion + both sides Various energy storage cycle coalescing engine and coalescence method to make a simple injection engine (88k) rotary blade injection airplane (7q) with center support bearing load 0 approaching counter-rotating manufactured 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 storage cycle coalescing engine and coalescence method for simple injection engine (88k) rotating blade injection airplane (7q) with propulsion + both center support bearing load 0 approaching counter-rotating production compressed air (28a) combustion.   Includes a theoretical combustion chamber (4Q) air suction flow path that receives liquid oxygen (5K) and produces a compression volume of 21/60000 of air compression, produced by a horizontal full blade ratio critical material gravity turbine (8U) generator Multiple ultra-high pressure fuel combustion injection propulsion + Both-side center support bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion simple injection engine (88k) Rotary blade injection airplane (7q) Driving various energy storage cycle coalescence engine and coalescence Method.   Horizontal full-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity, equipped with theoretical combustion chamber (4Q) air suction channel, multiple ultra high pressure fuel combustion injection propulsion + both sides Various energy storage cycle coalescence engines and coalescence methods driven by a simple injection engine (88k) rotating blade injection airplane (7q) with a center support bearing load 0 approaching counter-rotating manufactured 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 storage cycle coalescence engine and coalescence method driven by simple injection engine (88k) rotary blade injection airplane (7q) with propulsion + both center support bearing load 0 approaching counter-rotating production compressed air (28a) combustion.   Horizontal all-blade ratio critical material gravity turbine (8U) power generation electrical production, receiving liquid oxygen (5K) and making the compression volume 21/60000 of air compression multiple theoretical combustion chambers (4Q) + both sides center support bearing Various energy storage cycle coalescing engine and coalescence method driven by a simple injection engine (88k) rotating blade injection airplane (7q) with zero load approaching counter-rotating production 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 engine and coalescence method for driving a simple gas engine (88i) rotor blade airplane (7p) as compressed air (28a) combustion with center support bearing load 0 approaching counter-rotating production.   Horizontal all-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double side center support bearing load 0 approaching double reversal Various energy storage cycle coalescing engine and coalescence method for driving a simple gas engine (88i) rotor blade airplane (7p) as manufactured 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, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approach Various energy storage cycle coalescing engines and coalescence methods for driving a simple gas engine (88i) rotor blade airplane (7p) as counter-rotating manufactured compressed air (28a) combustion.   Theoretical combustion chamber (4Q) with high pressure fuel combustion + both sides receiving liquid oxygen (5K) and making compression volume 21/60000 Various energy storage cycle coalescence engine and coalescence method for driving a rotary blade airplane (7p) by driving a plurality of simple gas engines (88i) 1 as a center support bearing load 0 approaching counter-rotating production 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) ultra high pressure fuel combustion + double side center support bearing load 0 approaching double reversal Various energy storage cycle coalescing engines and coalescence methods for driving a compressed air (28a) combustion with a simple gas engine (88i) to drive a rotary wing airplane (7p).   Horizontal all-blade ratio critical material gravity turbine (8U) power generation electric manufacturing, receiving liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approach Various energy storage cycle coalescence engines and coalescence methods for driving a rotating blade airplane (7p) by driving a simple gas engine (88i) 1 to plural as counter-rotating manufactured compressed air (28a) combustion.   Theoretical combustion chamber (4Q) with high pressure fuel combustion + both sides receiving liquid oxygen (5K) and making compression volume 21/60000 Various energy storage cycle coalescence engine and coalescence method for driving a rotary blade airplane (7p) by driving a plurality of simple gas engines (88i) 1 as a center support bearing load 0 approaching counter-rotating production 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) ultra high pressure fuel combustion + double side center support bearing load 0 approaching double reversal Various energy storage cycle coalescing engines and coalescence methods for driving a compressed air (28a) combustion with a simple gas engine (88i) to drive a rotary wing airplane (7p).   Horizontal all-blade ratio critical material gravity turbine (8U) power generation electric manufacturing, receiving liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approach Various energy storage cycle coalescence engines and coalescence methods for driving a rotating blade airplane (7p) by driving a simple gas engine (88i) 1 to plural as counter-rotating manufactured compressed air (28a) combustion.   Theoretical combustion chamber (4Q) with high pressure fuel combustion + both sides receiving liquid oxygen (5K) and making compression volume 21/60000 Various energy storage cycle coalescence engines and coalescence methods that drive a simple gas engine (88i) to drive a rotary wing airplane (7p) as compressed air (28a) combustion near zero center support bearing load 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 gas engine (88i) driving rotor blade (7B) and driving a rotor blade airplane (7p) as combustion with compressed air (28a) approaching the center support bearing load close to zero.   Horizontal all-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double side center support bearing load 0 approaching double reversal Various energy storage cycle coalescence engines and coalescence methods for rotating a simple air engine (88i) driven rotor blade (7B) and driving a rotor blade airplane (7p) as a manufactured 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, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approach Various energy storage cycle coalescence engines and coalescence methods for rotating a simple gas engine (88i) driving rotor blade (7B) and driving a rotor blade airplane (7p) as counter-rotating manufactured compressed air (28a) combustion.   Theoretical combustion chamber (4Q) with high pressure fuel combustion + both sides receiving liquid oxygen (5K) and making compression volume 21/60000 Center support bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion of simple gas engine (88i) 1 to multiple drive rotor blades (7B) multiple energy storage cycle coalescence engine driven by multiple rotation rotor blade airplane (7p) And coalescing method.   Horizontal all-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double side center support bearing load 0 approaching double reversal Various energy storage cycle coalescence engines and coalescence methods for producing simple compressed air (28a) combustion as simple gas engine (88i) 1 to multiple drive rotor blades (7B) and driving the rotor blade airplane (7p).   Horizontal all-blade ratio critical material gravity turbine (8U) power generation electric manufacturing, receiving liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approach Various energy storage cycle coalescence engine and coalescence method for driving a rotary blade airplane (7p) by rotating a simple gas engine (88i) 1 to a plurality of driving rotor blades (7B) as counter-rotating manufactured compressed air (28a) combustion.   Theoretical combustion chamber (4Q) with high pressure fuel combustion + both sides receiving liquid oxygen (5K) and making compression volume 21/60000 Center support bearing load 0 approaching counter-rotating production Compressed air (28a) Combustion of simple gas engine (88i) 1 to multiple drive rotor blades (7B) multiple energy storage cycle coalescence engine driven by multiple rotation rotor blade airplane (7p) And coalescing method.   Horizontal all-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double side center support bearing load 0 approaching double reversal Various energy storage cycle coalescence engines and coalescence methods for producing simple compressed air (28a) combustion as simple gas engine (88i) 1 to multiple drive rotor blades (7B) and driving the rotor blade airplane (7p).   Horizontal all-blade ratio critical material gravity turbine (8U) power generation electric manufacturing, receiving liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approach Various energy storage cycle coalescence engine and coalescence method for driving a rotary blade airplane (7p) by rotating a simple gas engine (88i) 1 to a plurality of driving rotor blades (7B) as counter-rotating manufactured compressed air (28a) combustion.   Theoretical combustion chamber (4Q) with high pressure fuel combustion + both sides receiving liquid oxygen (5K) and making compression volume 21/60000 Various energy storage cycle coalescence engines and coalescence methods for rotating a simple gas engine (88i) driving rotor blade (7B) and driving a rotor blade airplane (7p) as combustion with compressed air (28a) approaching the center support bearing load close to zero.   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 engines and coalescence methods for driving a simple gas engine (88i) driving a simple injection engine (88k) as compressed air (28a) combustion with a center support bearing load approaching zero inversion.   Horizontal all-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double side center support bearing load 0 approaching double reversal Various energy storage cycle coalescence engine and coalescence method for driving simple gas engine (88i) driving simple injection engine (88k) as production 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, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approach Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88i) driven simple injection engine (88k) as counter-rotating manufactured compressed air (28a) combustion.   Theoretical combustion chamber (4Q) with high pressure fuel combustion + both sides receiving liquid oxygen (5K) and making compression volume 21/60000 Various energy storage cycle coalescence engine and coalescence method for driving a simple gas engine (88i) 1 to a multiple drive simple injection engine (88k) as combustion with compressed air (28a) approaching the center support bearing load 0 approaching counter rotating.   Horizontal all-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double side center support bearing load 0 approaching double reversal Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88i) to a multiple drive simple injection engine (88k) as manufactured 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, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approach Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88i) 1 to a multiple drive simple injection engine (88k) as counter-rotating manufactured compressed air (28a) combustion.   Theoretical combustion chamber (4Q) with high pressure fuel combustion + both sides receiving liquid oxygen (5K) and making compression volume 21/60000 Various energy storage cycle coalescence engine and coalescence method for driving a simple gas engine (88i) 1 to a multiple drive simple injection engine (88k) as combustion with compressed air (28a) approaching the center support bearing load 0 approaching counter rotating.   Horizontal all-blade ratio critical material gravity turbine (8U) power generation electricity production, receiving liquid oxygen (5K) + electricity, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + double side center support bearing load 0 approaching double reversal Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88i) to a multiple drive simple injection engine (88k) as manufactured 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, theoretical combustion chamber (4Q) ultra high pressure fuel combustion + both sides center support bearing load 0 approach Various energy storage cycle coalescence engines and coalescence methods for driving a simple gas engine (88i) 1 to a multiple drive simple injection engine (88k) as counter-rotating manufactured compressed air (28a) combustion.   Theoretical combustion chamber (4Q) with high pressure fuel combustion + both sides receiving liquid oxygen (5K) and making compression volume 21/60000 Various energy storage cycle coalescence engines and coalescence methods for driving a plurality of simple gas engines (88i) driven simple injection engines (88k) as compressed air (28a) combustion with a center support bearing load approaching zero inversion.

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