JP2013119793A - Various energy conservation cycle combined engine - Google Patents

Abstract

PROBLEM TO BE SOLVED: To solve problems in the conventional steam turbine power generation utilizing by half stationary blades of 0 work rate for blocking steam velocity to reduce the steam velocity to 1/10, multiply the water volume to 43,000 times at the maximum speed part, and the like so that it is close to 0 output power generation.SOLUTION: For improving the configuration comprising half stationary blades of 0 work rate for blocking the lightweight steam velocity, and the like and furthermore of 1/10 or less power generation amount in lightweight power generation, power generation amount per 1 unit of 1,355 times with respect to the conventional configuration is targeted by superimposing 100 sets of a mercury injection turbine for aiming at Mach 30 with all moving blades provided in a double reverse rotation structure with a lateral shaft 1h gear in 30 mmHg vacuum for example as a mercury gravitational acceleration power generation. For aiming at 0 bearing load, with electricity generated with a solar light heater driven by inexpensive electricity of 1/100 power generation cost such as 0 fuel cost, and the like, liquid air, and heated steam heating supply equipment 3D are prepared. For automobiles, ships, airplanes, and the like, liquid oxygen compression drive is employed for obtaining air compression 21/60,000 volume compression work ratio to have 1/10 fuel cost and 10 times speed so that a day trip is enabled to anywhere on the earth with airplanes by aiming at 1/500,000 space attaining cost. Thereby, excellent operation profit ratio is achieved for all products to be No. 1 in the world forever.

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 reactors to be completely abolished, the horizontal all-blade specific material gravity turbine 8U power generation electric drive 1 to multiple stages The pump 1G and the solar heater 21 are used, and the solar heating air is used as the compressed high temperature, and the heat production is divided and stored in the 1-multistage compression heat recovery unit 2C, and the 24-heat of 200 to 200 MPa superheated steam + liquid air 28a. Divided and stored in cold heat, electricity + liquid air cold heat + superheated steam temperature supply equipment 3D for infinite applications. For example, ships, vehicles, airplanes, etc. receive liquid oxygen and the compression volume work rate is 21/60000 of air compression. The volumetric power factor, the compression pressure of liquid oxygen and water 20 times, etc. are facilitated, the rotational power of the theoretical expansion engine 3Q is driven, the combined oxygen injection of the oxygen combined air injection unit 88B and the oxygen combined water injection unit 88L is promoted, In combined jet propulsion, natural phenomena are accelerated 2a Nitrogen, oxygen, and CO2 are supplied to seawater. Microorganisms and seaweeds increase, and food such as fish greatly increases in the food chain. O2 exhaust 1/10 and fuel costs 1/10 and 1/50 ten thousand expenses universe reaching aim, 10 double-speed aim is an airplane or a ship, on the technology of various energy conservation cycle union organizations and various energy conservation combined method.

  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. Super high-pressure high-temperature superheated steam 50 is heated by high-temperature combustion, and super high-pressure oxygen super-high-pressure fuel flame 3000 ° C or higher is used for various researches of oxygen-hydrogen-enhanced combustion aimed at pyrolysis and electrolysis of superheated steam, and super-high pressure combustion in the theoretical combustion chamber 4Q The gas 49 + superheated steam 50 is injected from the high-pressure / high-temperature combustion gas control valve 5a and the combustion gas injection nozzle 6Y to drive the theoretical expansion engine 3Q to drive various vehicles such as automobiles and tillers, propellers 7A, rotor blades 7B, Drives the screw 7C, drives various vehicles, propeller airplanes and screw ships, and aims at a fuel cost of 1/10 or 10 times speed by using liquid oxygen 5K for power generation electricity generation, and the best operating profit rate in the world The present invention relates to a technology for combining various energy storage cycle coalescence engines and coalescence methods.

  The existing jet gas turbine consumes enormous amount of fuel by air compression, and the rotation output and injection propulsion output are reduced, and space flight such as 16 rounds of the earth on the day of the air resistance 01 is impossible by air compression. As an aim of propulsion of the liquid compressed oxygen united air injection unit 88B combined with the horizontal type, the total moving blade ratio critical material gravity turbine 8U power generation electric drive multiple 1 to multiple stage theoretical gas compressor 3T equal heat pump 1G + solar heater 21 By heat production, it is divided and stored in high temperature water of 24 to 200 MPa to superheated steam temperature 50 + liquid air cold heat 28a, and as an electricity + liquid air cold heat + superheated steam heat supply facility 3D, the jet propulsion of the aircraft is liquid oxygen 5K + liquid fuel 1c + high temperature. Received by water 52a and compressed by compression of liquid oxygen, compressed volumetric power is compressed to 21/60000 volumetric power of air compression by ultra-high pressure, liquid oxygen control Open the valve 5T + water control valve 5Q + liquid fuel control valve 1K, set the fuel heating pipe 1L water heating pipe 5H oxygen heating pipe 5H to the optimum heating temperature of the oxygen combined air injection part 88B theoretical combustion chamber 4Q, and control the fuel. Open the valve 25b + oxygen control valve 24D + superheated steam control valve 25 and inject each one into the theoretical combustion chamber 4Q aiming at one or more theoretical ultra-high pressure combustion, oxygen injection nozzle 6L fuel injection nozzle 6X multiple central combustion at 3300 ° C. or more As a target for pyrolysis and electrolysis, superheated steam aims to increase oxygen-hydrogen combustion + air in front of rocket combustion is sucked and injected, and 1 to multi-stage suction air flow jet combustion is added, theoretical combustion chamber 4Q superheated steam injection nozzle 6A superheated steam 50 is targeted for 200MPa injection, combustion gas 49 is sucked and injected, and rocket combustion is aimed at the existing space cost of 1 / 500,000. To allow a day trip to one day in a row anywhere on Earth equal to 16 laps of the earth, aiming profit margin preeminent world in a variety of space shuttle airplane class, relates to a technology of various energy conservation cycle combined institutions and coalescence method.

  The existing ship consumes a large amount of fuel by air compression, reduces the rotational output and injection propulsion output, and consumes a large amount of fuel for low-speed movement. / 60000 volumetric power, liquid air production air compressor is also theoretically best theoretical gas compressor 3T addition, horizontal full blade ratio critical material gravity turbine 8U power generation electric drive 1 to multi-stage theoretical gas compressor 3T As the isothermal pump 1G compression, the solar heater 21 solar heating air is compressed to a high temperature, and heat production is divided and stored in the 1-multistage compression heat recovery unit 2C. Steam 50 hot + liquid air 28a cold and stored separately, electricity compressed as liquid + air cold + superheated steam hot water supply equipment 3D, pumping liquid oxygen 5K + liquid fuel 1c + hot water 52a in the process of receiving Aiming at 00 MPa, the liquid oxygen control valve 5T + the liquid fuel control valve 1K + the water control valve 5Q are opened, and the oxygen combined water injection part 88L is heated to the optimum temperature in the inner periphery of the theoretical combustion chamber 4Q, respectively. Each of the injections to the theoretical expansion engine 3Q is driven by water suction injection or rotationally driven to promote water suction / injection propulsion of the oxygen combined water injection unit 88L or to rotate the screw 7C of the theoretical expansion engine 3Q. / 10 As a fuel cost target, the screw propulsion theoretical expansion engine 3Q exhaust will be the bottom bottom exhaust injection propulsion, the natural phenomenon speeded up in the process of friction reduction injection propulsion, supplying oxygen, nitrogen, CO2 etc. into the sea, It is related to the technology of various energy conservation cycle coalescence engines and coalescence methods aiming at the world's highest profit rate by increasing the food of human beings that proliferate phytoplankton, seaweeds, corals, fish, etc. .

  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 velocity is dammed and the vanes with no work are alternately half-damped with the moving blade, the vapor velocity is approaching 1/100, and the gas volume is inversely proportional to the pressure. Therefore, because it requires a turbine blade that supports 240 times volume from 240 atmospheres to atmospheric pressure +30, 4 times Hg, and 25 times volume, it can handle 6000 times capacity, theoretically, the high-pressure steam speed is unreasonable and low speed is necessary. In addition to responding to the turbine blade area, the seawater temperature is raised by 7 degrees with all the generated heat, making the whole sea surface temperature-increasing natural phenomenon, increasing abnormal weather without upper limit, around 50 to 100 years People due to heavy rain in seawater There is in increasing the risk of closer to extinction. The green earth is a miracle product and there is a great risk of approaching other stars. According to the explanation of the power station, if the rise in seawater temperature is 7 degrees or less, there is no influence on the environment, but for example, 7 degrees in the sea area where the seawater temperature is 30 degrees If the rise continues, the typhoon wind speed will be 300m / sec, etc., and there will be danger of human beings extinction due to the covering of concentrated rainwater salt in seawater, etc., and the temperature of the whole sea surface will rise and nutrients such as nitrogen, oxygen, CO2 etc. The natural phenomenon that has supplied water is made impossible, the number of marine microorganisms, phytoplankton and seagrass is drastically reduced. The number of marine foods such as fish is drastically reduced. If China continues to grow 10%, the rise in seawater temperature will be 10%. The current rate is twice as high as the current rate in 20 years, and the speed of typhoons, seasonal winds and ocean tornadoes is 100m / sec. And forestry and residential areas Such as close to 0, for Japan residents it is difficult before and after 50 years, there is a background necessary technical development that corresponds to the existing technologies worst part before it's too late.

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 material mercury gravity turbine 8S power generation cylindrical turbine blade group 8A horizontal shaft plate 16 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 the expansion of low-cost electricity applications with zero fuel cost generation by mercury resources, solar heating of air with solar heater 21, 1-stage theoretical gas compression of mercury gravity turbine 8S fuel cost 0 power generation electric drive It is compressed multiple times with a heat pump 1G such as a machine 3T, and is heat-recovered multiple times and stored separately in 24 to 200 MPa high-temperature water 52a to superheated steam temperature 50 + liquid air cold heat 28a, from electricity + liquid air cold heat + superheated steam temperature heat supply equipment 3D Supply it to the liquid oxygen chamber 5K, storage battery, etc., make liquid air driven automobiles, airplanes and ships drive 1/10 fuel cost drive or 10 times speed drive, drive battery storage or electric drive for extremely cheap power generation In addition, there is a background that can prevent global warming with little CO2 exhaust.

  In high school and university, the existing engine is described as the best engine, and when we return to elementary school science without brainwashing and think about the best engine, the unit of work is kg weight m / sec. The engine is the best engine in terms of generating rotational output at a high speed, but there is no trace of thought. Therefore, for example, if the horizontal full-blade ratio critical material gravity turbine 8U power generation is used, there is a background of low fuel cost power generation. The best fuel cost is heating. Therefore, the fuel cost 0 power generation electric drive solar heater 21 is used, and the heat pump 1G such as the 1-multistage theoretical gas compressor 3T or the 1-multiple stage compression of the air 28a heated by sunlight with the fuel cost 0 power generation electric drive is used. In the heat recovery unit 2C, the heat is recovered multiple times and heat is recovered multiple times, divided into 5K cold liquid oxygen and 5L liquid nitrogen + hot high temperature water 52a to superheated steam 50, and in the process of infinite use of heat, for example permafrost Injecting superheated steam 50 into underground methane hydrate, splitting it into methane and water, recovering methane with liquid nitrogen cooled liquid methane and continuing the superheated steam injection forever, the methane recovery enclosure has a suitable temperature and lots of water droplets Land grazing, increasing the use of food by humans, and infinite use of heat, aiming to reach 1 / 500,000 in space-driven costs for liquid air-powered cars, ships and spacecrafts, and speeding natural phenomena in the process of ship driving 2a , Fine And the seaweed and coral, etc. to increase the food of fish such as the human race in the growth the food chain, etc., to prevent the heavy rain of sea water there is a background that can put off the human race extinct. Revolution of employment growth that will increase the employment by making the manufacturing operation monopolized 100% worldwide, with the operating profit rate becoming 10 times larger than the existing operational profit ratio, as the ship revolution and airplane revolution aiming at 10 times speed with low fuel cost There is a background that can be.

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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 19 applications, including PCT, from the filing date of Japanese Patent Application No. 2011-247103 to September 30, 2011.

  In the existing thermal power plants in the world, the total heat generation is 7 degrees Celsius, and the seawater temperature rise is 1000 times in 100 years, and the downdrafts and updrafts are increased as much as possible. As the number of storms, torrential rains, heat waves, cold waves, etc. increases without limit, typhoons, seasonal winds, tornadoes, etc., around 100 years in the sea near Japan, salt water on the land due to concentrated heavy rains, etc. Covering increases the danger of human land food loss, making it impossible for the natural phenomenon of supplying nutrients to the sea-cooled seabed in winter, dramatically reducing microorganisms, phytoplankton, seaweeds, corals, etc., fish through food chains, etc. The number of human underwater foods has been reduced as much as 1/100, and droughts, torrential rains, typhoons and seasonal winds have increased 10 times in 100 years. For example, typhoons and seasonal winds have an upper limit such as 300m / sec. weather Giant seafloor bedrock expansion earthquakes and tsunamis, and eastern Japan earthquakes and tsunamis have also become huge, preventing heavy rain in seawater to increase the danger of human extinction, preventing global warming such as rising seawater temperature, There is a challenge to postpone human extinction. A recent issue is the rapid increase in countries with deficits. The biggest cause is the epidemic that easily makes profits with low labor cost countries as the world's factories, and all the developing countries that can easily make profits compete for the best in imitation improvement like Japan in the past, so cheap and excellent products There is a risk of the destruction of manufacturing facilities in the developed countries and the deficit of jobs in the developed countries, and the destruction of employment.There is an urgent need to increase profit margins in developed countries because the current economic crisis is in the early stages. However, as a top-secret manufacturing operation of the invention that keeps 100% monopoly on the world scale forever, there is a challenge to make the world's most eternal financial surplus with outstanding profitability forever.

Horizontal full blade ratio critical material gravity turbine 8U fuel cost 0 power generation low cost electric drive all, heat production by solar heater 21 + 1-multistage theoretical gas compressor 3T etc. heat pump 1G + 1-multistage compression heat recovery unit 2C , Electricity + liquid air cold heat + high temperature water to superheated steam temperature heat supply equipment 3D, the received liquid oxygen 5K is compressed to 21/60000 volumetric compression work rate of air compression, the theory that ultra high pressure combustion and ultra high temperature combustion are easy As combustion chamber 4Q, high-pressure high-temperature superheated steam 50 is heated by near-center combustion of oxyfuel ultra-high pressure combustion, and thermal decomposition electrolysis of superheated steam is aimed at combustion of 3000 ° C. or more for oxygen-hydrogen-enhanced combustion. A theoretical expansion engine 3Q driven by a theoretical combustion chamber 4Q, an oxygen combined water injection unit 88L, and an oxygen combined air injection unit 88B are used to drive vehicles such as automobiles, ships, and airplanes and to drive and Propulsion drive, ship jet propulsion drive speeds up natural phenomena 2a, supplies oxygen, nitrogen, CO2 etc. into the sea, increases microorganisms, phytoplankton, seaweeds, corals, fish, etc., increases human food The plane is going around the earth 16 times a day in the prime of space flight close to CO2 exhaust 0, etc. Every day on the earth, it is assumed that CO2 exhaust is a little flight anywhere in the atmosphere, 100% global scale monopoly and top secret manufacturing operation As the world's most profitable power generation, ships, airplanes, automobiles, etc., the world's number one with outstanding profitability and the world's largest number of new jobs, preventing droughts, torrential rains, typhoons, seasonal winds, heavy rains in seawater, and earthquakes and tsunamis Prevent global warming and postpone human extinction.

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, and seawater temperature rises 0, CO2 emissions 0 and fuel costs 0 Electric power drive is required. Therefore, the fuel cost is 0. Electricity generated by power generation + liquid air cold heat + high temperature water to superheated steam temperature heat supply equipment 3D receives liquid oxygen 5K, etc., and the compression work rate of combustion oxygen is 21/60000 volumetric compression work of air compression The theoretical combustion chamber 4Q uses the theoretical expansion engine 3Q, the oxygen coalescence water injection unit 88L, and the oxygen coalescence air injection as an aim to increase the superhigh pressure superheated steam 50 in the superficial combustion chamber 4Q center and increase the pyrolysis electrolysis. Part 88B has the effect of being able to drive the most efficiently, and in addition to the effect of targeting 1/10 or 10 times the fuel cost of automobiles, ships and airplanes, the space arrival cost is aimed at 1 / 500,000 of existing space rockets The wheel, screw 7C, propeller 7A and rotor blade 7B are driven by the theoretical expansion engine 3Q, and the ship, airplane, car, etc. are driven by the rotational force, and the ship injection propulsion drive is used. Natural phenomenon speeding up 2a, and the effect of increasing the digestive capacity of underwater microorganisms such as CO2 to tens of thousands of times of the forest, etc. is great, and phytoplankton, seaweeds, corals, etc. are propagated, and fish and other human beings in the food chain etc. Greatly increase undersea food, prevent desertification, droughts, torrential rains, typhoons, seasonal winds, earthquake tsunamis, etc., postpone the most important human extinction of humanity, and aim to achieve the world's best profit rate is there.

Plane drive receives liquid oxygen hot water from electricity + liquid air cold heat + high temperature water to superheated steam temperature heat supply equipment, which is driven by electric power driven by gravity turbine 8U power generation with zero fuel cost, horizontal fuel blade ratio, liquid oxygen 5K + liquid fuel 1c + high temperature water 52a is compressed by ultra high pressure with the liquid fuel pump 4a + liquid oxygen pump 4b + water pump 4c, the liquid fuel control valve 1K + liquid oxygen control valve 5T + water control valve 5Q is opened, and fuel in the inner periphery of the theoretical combustion chamber 4Q Heating pipe 1L + oxygen heating pipe 5F + high temperature water heating pipe 5H is optimally heated to open the fuel control valve 25b oxygen control valve 24D and to perform mixed injection ignition combustion near the center of the oxygen gas + fuel gas plural locations, theoretical combustion chamber 4Q The fuel heating pipe 1L on the inner circumference + oxygen heating pipe 5F + high-temperature water heating pipe 5H is optimally heated and superheated to super-high pressure and high-temperature superheated steam 50, etc., and the theoretical combustion chamber 4Q superheated steam is heated at the highest temperature and super-high pressure combustion. Aiming at pyrolytic electrolysis aiming at increased oxygen hydrogen combustion, driving the oxygen coalesced air injection unit 88B, aiming for space arrival cost 1 / 500,000 of existing space rocket, using the same fuel cost 10 times injection propulsion output It has the effect of aiming for prime, for example, the jet propulsion output is aimed at 100 times the pressure of existing jets, 10 times the calorie injection, and 1000 times the propulsion output for the short time. Since the steam injection speed and the combustion gas injection speed are the highest in vacuum, the existing space rocket ground mass injection is considered the worst, and from the vicinity of the highest flight altitude of the existing aircraft, high pressure high temperature combustion gas 5M + 5N high pressure high temperature steam 5N There is an effect that the injection amount is increased and the earth is made 16 times a day, etc., and the space use prime that allows a day trip anywhere on the earth can be aimed.

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 of electricity + liquid cold / heat supply equipment 3D (Example 3) Explanatory drawing of 9B9C9D9E6F6G6H of theoretical gas compressor 3T (Example 4) Explanatory drawing of 5b6X6Y9B9C9D9E5 of theoretical expansion engine 3Q (Example 5) Explanatory drawing of oxygen combined water injection part 88L (Example 6) Explanatory drawing of the oxygen coalescence air injection part 88B (Example 7) Explanatory drawing of the theoretical expansion locomotive 4L (Example 8) Explanatory drawing of oxygen coalescence screw ship 39Q (Example 9) Explanatory drawing of the oxygen coalescence screw injection ship 39S (Example 10) Explanatory drawing of oxygen coalescence injection ship 39R (Example 11) Explanatory drawing of the oxygen coalescence injection plane 39T (Example 12) Explanatory drawing of oxygen combined propeller plane 39U (Example 13)

  The use of gravity acceleration in vacuum for a long period of time is prevented by brainwashing such as existing steam turbine power generation, and one unit of 100 sets prevents the aim of generating power 43,000 times that of one existing steam turbine power generation, for example, the existing best steam turbine power generation Steam pressure is reduced by reducing the atmospheric pressure, the same speed, and the same volumetric power, kg weight m / second, to 1/1700 of the water power, and by installing the stationary blades alternately with the moving blades and blocking the rotation output to zero. The seawater temperature rises by 7 degrees with all of the driving heat of the sea, the fishes drastically decrease, the bottom bedrock expands into earthquakes and tsunamis, and the typhoons, seasonal winds and sea tornadoes around Japan are increased to around 100 m / sec. There is a danger that food extinctions and humankind extinction will be approaching rapidly by providing salt coating on the land in around 50 to 100 years, such as heavy rain of suction seawater is expected over the sea. That is, the invention becomes too vast due to many fatal drawbacks of the existing technology, so the invention is described in the explanation of the reference numerals, and the part that has been repeatedly explained in the previous application is omitted, and other than the horizontal full blade ratio material gravity turbine 8U Will be explained in substitution for three examples, and we will try to materialize the invention without common sense.

Figure 1 Gravity acceleration in vacuum + mercury injection speed Mach 30 drive, etc., aiming to the limit, horizontal type blade blade critical material gravity turbine 8U power generation is proportional to kg weight m / second, so both sides of cylindrical turbine blade group 8A And repulsive permanent magnets 9B attracting permanent magnets 9C at a plurality of locations such as the center, and the cylindrical turbine blade group 8A side as a ring type inner periphery 1 pole outer periphery 1 pole magnetization, and the turbine outer box 77a side as a ring type inner periphery 2 poles The upper attraction permanent magnet 9C is the lower repulsion permanent magnet 9B, and the weight of the rotating part is made close to 0 by the repulsive force and the attraction force at multiple locations, the bearing load is made close to 0, and the aim is to update the super high speed turbine peripheral speed record. Medium mercury gravity acceleration Mach 30 Turbine driving approach aiming, horizontal axis 16A with horizontal shaft plate 16 aiming at infinite increase of fixed rotation speed and rotation outer diameter, one type is manufactured 2 sets 1 set 100 sets in series Movement As a manufacture of flywheel turbines, or as one set, 200 series full-blade flywheel turbines and bite-in series full-blade flywheel turbines, each with 100-200 sets vertically by fully automatic casting, fully automatic processing, etc. One unit is manufactured, and 100 units, etc. are provided in the existing highest building height of 828m vertically, and one unit is provided. For example, the mercury 3E platinum ball 2E is raised vertically by 828m, etc. The platinum ball 2E is mixed and injected with a large material accelerator 6W at a pressure of mercury 3E to aim Mach 28 injection, driven by acceleration of gravity acceleration and vacuum, and the cylindrical turbine blade group 8A is counter-synchronously rotated by the counter-synchronous gear 4C. The rotating gear 4D is rotated at the same speed and in the same direction, such as 100 pairs, making it easy to mass-produce cheaply, eliminating the need for boilers and nuclear reactors, and accelerating the mercury acceleration etc. The generator 1 is selectively provided as an opposing synchronous gear 4C main shaft or a series co-rotating gear 4D main shaft, and more than 100 sets of driving power generation costs outside the turbine outer casing 77a are aimed at 1/10, and the structure is extremely Simple and extremely inexpensive electric product infinite and electric drive infinite, making the world's best energy conservation cycle combined engine power generation and combined method power generation with outstanding profitability.

The horizontal full-blade specific material gravity turbine 8U power generation is composed of 100 units such as 100 existing vertical buildings in the turbine outer box 77a and one unit, and a platinum ball 2E with mercury 3E pressure, for example, by a specific material accelerator 6W. Mixed injection + acceleration of gravity acceleration in vacuum = Mach 28 aiming, injected into cylindrical turbine blade group 8A, horizontal full blade ratio material gravity turbine 8U drive power generation, maintaining Mach 28 speed aim, gravity acceleration in vacuum As the maximum acceleration effect, the next turbine is driven by the next turbine to make effective use of the head to make the gravity turbine 8U power generation, and by frictional heat cooling, it is easy to exceed the existing power generation maximum vacuum such as 30mmHg by air extractor 51 , 100 pairs are used for the drop 828m, and compared with the final stage of the existing steam turbine power generation, the vacuum degree is 30mmHg water 43,000 times volume Mach 1 speed steaming As a simple comparison with 100 turbines of one turbine 8U power generation amount, 1/1000 volume of mercury is 43 × 100 × 13, 55 = 58265 times mercury power generation amount by Mach 1 speed injection, and platinum ball is 91891 The energy saving cycle coalescence engine fuel cost becomes 0 extremely low-cost power generation, which results in the power generation amount of astronomical magnification that requires experiments such as calculation of double platinum ball power generation amount.

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

The heat production of the solar heater 21 in FIG. 3 is a horizontal all-blade ratio critical material gravity turbine 8U fuel cost 0 power generation power generation extremely cheap electric drive, cheap electricity + liquid air cold heat + superheated steam temperature supply equipment 3D The solar heater 21 has a buoyancy on the surface of the water or a circular railroad on the flat ground, and the solar heater 21 is used as a floating device or a land device for maintaining and rotating sunlight at right angles from east to west. Is provided with a rotation support part 4f, and equipped with a gear unit 4d and a roller 4e, and as a cylindrical rotation part 77G, it controls the vertical rotation of sunlight in the vertical direction, and controls the rotation of the vertical direction in the east-west direction by using buoyancy and circular railway. , By controlling the rotation of sunlight in two directions at right angles, and setting it as a device that maximizes the air temperature in the heat absorption tube 4H, collects sunlight with the largest amount of earth in a straight line by the rectangular long lens 2d and heats it near the focal length. Absorption tube 4H The internal air passage 28A air 28a temperature is maximized, the external air passage 28A air 28a temperature is also increased, and the existing lens cross section is linearly extended as a rectangular long lens 2d. A heat insulating material 2c such as a cylinder is surrounded by a cylindrical rotating portion 77G or the like to make a long cylinder such as a cylinder, a long long lens 2d is a joint 80A + fastener 80B, and a sealed upper part is a 4H external air passage 28A. Intake and compression as 1 to multiple stage heat pump 1G for suction, theoretical gas compressor 3T and the like as heat pump 1G are set to 800 to 1200 ° C multiple times, and heat recovery is repeatedly performed at 1 to multiple stage compression heat recovery unit 2C. Then, the liquid air 28a cold heat is stored in the liquid oxygen chamber 5K + liquid nitrogen chamber 5L, and the 24-heat of about 200-400 MPa superheated steam is divided and stored in the high-pressure high-temperature steam chamber 5N. Electrical + liquid air cold + using various applications in the superheated steam heat supply facilities 3D, the electric drive flourish and battery driven prime, to various thermal utilization prime and various cold use PRIME electrical product.

The theoretical gas compressor 3T of FIG. 4 is equipped with a repulsive permanent magnet 9B attracting permanent magnet 9C compressed air part 9D vacuum part 9E water injection part 6F aiming at super-large size, ultra-high speed rotation, and compression ratio greatly increased, and uses magnetic force + air pressure. With a bearing load approaching zero or using heat of vaporization, the compression ratio of one unit is greatly increased, and Boyle's law gas volume is inversely proportional to the pressure. The best aim is to compress the suction from the large circumferential blade to the central short blade. As a result, the maximum intake air amount is aimed at, and the intake air velocity is aimed at the maximum at the upper compression blade group 8g and the lower compression blade group 8h of all the rotor blades, and the assembly compression blade group 8j facilitates assembly and suction. With the aim of the maximum mouth area and the best compression efficiency, the horizontal-type full blade ratio material gravity turbine 8U fuel cost 0 power generation extremely low-priced electric drive, by the double reversal magnetic (gear) device 85 (85Y) of the horizontal shaft 1h gear , Upper compression blade group 8g The side compression blade group 8h is rotated in the opposite direction to rotate in the opposite direction, the relative peripheral speed is 3 to 10 times that of the existing axial flow compressor, the theoretical gas compressor 3T is the best theoretical gas compressor 3T, and the final compression blade 6 stationary blade 6G The heat production is to press fit into the compressed air heat exchanger 2Y, and the heating air of the solar heater 2 is mainly compressed with a heat pump 1G such as the theoretical gas compressor 3T, and 1 to a plurality of stages of compression heat for each compression high temperature. Heat is recovered by the recovery unit 2C, divided and stored as liquid air cold heat + superheated steam temperature heat, and used as a supply facility 3D for electricity + liquid air cold heat + hot water to superheated steam temperature heat. For use in infinite heating applications such as greenhouse cultivation, inexpensive liquid oxygen is used for driving automobiles, ships and airplanes with a compression work rate of 21/60000 of air compression, and inexpensive liquid nitrogen is used for infinite use for cooling such as ice production, Various uses You use.

The theoretical expansion engine 3Q aiming at oxygen-hydrogen increase combustion in the ultra-high pressure limit combustion of FIG. , With the use of magnetic force + air pressure and bearing load approaching zero, horizontal full blade ratio material gravity turbine 8U fuel cost 0 power generation extremely cheap electricity production from electricity + liquid air cold heat + hot water to superheated steam heat supply equipment 3D, By receiving liquid oxygen 5K + electricity + high temperature water and compressing liquid oxygen 5K, the compression volume work rate becomes 21/60000 volume compression work rate of air compression, and liquid oxygen 5K + liquid fuel 1c + high temperature water 52a is 24 to Compressed to an ultrahigh pressure such as 200 MPa, the liquid oxygen control valve 5T + liquid fuel control valve 1K + water control valve 5Q is opened, the theoretical combustion chamber 4Q inner wall fuel heating pipe 1L high-temperature water heating pipe 5H oxygen heating pipe 5 Then, the upstream superheated steam control valve 25 + oxygen control valve 24D + fuel control valve 25b (not shown) is opened and burned at 3000 ° C. or more in the vicinity of the super high pressure fuel oxygen center, and a part of the superheated steam 50 is burned. Aspirating pyrolysis electrolysis oxygen oxygen hydrogen increase combustion aiming near the center, 200MPa aiming superheated steam 50 heated to the optimum temperature on the inner wall is injected with superheated steam injection nozzle 6A, combustion gas injection nozzle 6Y combustion gas 49 is sucked and injected, Compressed intake air passage 5b The compressed air portion 9D of the air injection nozzle 5 is sucked and injected, and the theoretical expansion engine 3Q is driven to increase the fuel combustion amount significantly by increasing the fuel injection combustion combustion amount from the fuel injection nozzle 6X of the fuel pipe 25c. Then, the combustion gas 49 is changed to a high-pressure high-temperature combustion gas 49 and injected from the center in a circumferential direction of 380 degrees, and the upper expansion blade group 8d and the lower expansion blade group 8e are optimally injected. A double inversion driving, the volume of Boyle's law gas as the best theoretical expansion engine 3Q theory which is inversely proportional to the pressure, the theoretical expansion engine 3Q which injects the turbine outer casing 77a assembled turbine blade group 8f.

The rocket combustion + jet combustion drive of the oxygen coalescence water injection unit 88L aiming at oxygen-hydrogen increase combustion in the ultra-high pressure limit combustion of FIG. By receiving liquid oxygen 5K + electricity + high temperature water from the electricity + liquid air cold heat + high temperature water to superheated steam temperature supply facility 3D and compressing the liquid oxygen 5K, the compression volume work rate is 21/60000 volume of air compression. The compression work rate is set, liquid oxygen 5K + liquid fuel 1c + high temperature water 52a is compressed to an ultrahigh pressure such as 24-200 MPa, the liquid oxygen control valve 5T + liquid fuel control valve 1K + water control valve 5Q is opened, and the theoretical combustion chamber 4Q inner wall fuel Heating tube 1L + high temperature water heating tube 5H + oxygen heating tube 5F is heated to an optimum temperature, superheated steam control valve 25 + oxygen control valve 24D + fuel control valve 25b is opened, and ultra-high pressure fuel acid The high-pressure high-temperature superheated steam 50 is heated by multiple combustion at 3000 ° C. or more in the vicinity of the center, and a part of the superheated steam 50 is aimed at the combustion by suction pyrolysis electrolysis oxygen oxygen hydrogen increase near the center, and the superheated steam injection nozzle 6A aimed at the inner wall protection 200 MPa. Injecting combustion gas 49 by suction, ultra high pressure high temperature rocket combustion injection, fuel injection nozzle 6X multiple fuel injection jet combustion in air suction flow, ultra high pressure high temperature rocket combustion + jet combustion 1 to multiple times, the highest ultra high pressure Various energy storage cycle coalescence engines that make superheated steam 50 easy to achieve the maximum injection speed by core superheat injection, suck air in front of air 28a and suck water in front of water 52a into oxygen combined water injection unit 88L And a coalescence method.

The rocket combustion + jet combustion drive of the oxygen combined air injection unit 88B aiming at oxygen-hydrogen increase combustion in the ultra-high pressure extreme combustion in FIG. 7 is a horizontal type full blade ratio critical material gravity turbine 8U fuel cost 0 power generation extremely cheap electric production, By receiving liquid oxygen 5K + electricity + high temperature water from the electricity + liquid air cold heat + high temperature water to superheated steam temperature supply facility 3D and compressing the liquid oxygen 5K, the compression volume work rate is 21/60000 volume of air compression. The compression work rate is set, liquid oxygen 5K + liquid fuel 1c + high temperature water 52a is compressed to ultrahigh pressure such as 24-200 MPa, the liquid oxygen control valve 5T + liquid fuel control valve 1K + water control valve 5Q is opened, and the theoretical combustion chamber 4Q inner wall fuel Heating to the optimum temperature with the heating pipe 1L + high temperature water heating pipe 5H + oxygen heating pipe 5F, the superheated steam control valve 25 + oxygen control valve 24D + fuel control valve 25b is opened, and ultra high pressure fuel High-temperature high-temperature superheated steam 50 is heated by multiple combustion at 3000 ° C. or more in the vicinity of the elementary center, and a part of the superheated steam 50 is aimed at the combustion by suction pyrolysis electrolytic oxygen hydrogen hydrogen increase near the center, and the superheated steam injection nozzle aimed at the inner wall protection 200 MPa Combustion gas 49 suction injection with 6A injection, ultra high pressure high temperature rocket combustion injection, fuel injection nozzle 6X multiple fuel injection jet combustion in air suction flow, ultra high pressure high temperature rocket combustion + jet combustion 1 to multiple times, the most Various energy storage cycle coalescence engines and coalescence methods are adopted in which superheated steam 50 that is easy to be high pressure is set to the maximum injection speed by core superheat injection, and the air 28a in front is sucked and injected into the oxygen coalescence air injection unit 88B.

The theoretical combustion chamber 4Q theoretical expansion engine 3Q drive of the theoretical expansion engine vehicle 4L aiming at hydrogen + oxygen increase combustion in the ultra high pressure limit combustion of FIG. 8 is a horizontal type full blade ratio critical material gravity turbine 8U fuel cost 0 power generation extremely cheap electricity Liquid oxygen 5K + electricity + high temperature water is received from the manufacturing equipment 3D of electricity + liquid air cold heat + high temperature water to superheated steam temperature heat supply, the high temperature water 52a is compressed to 200MPa etc. by the water pump 4c, and the liquid fuel 1c is liquid The fuel pump 4a compresses, and the liquid oxygen 5K is compressed by the liquid oxygen pump 4b, so that the compression volume work rate is 21/60000 volume compression work rate of air compression, and the liquid oxygen control valve 5T is theoretically assumed to be the open liquid oxygen 5K. Supply overheat to the inner wall of the combustion chamber 4Q, overheat the water control valve 5Q open high temperature water 52a to the inner wall of the theoretical combustion chamber 4Q, and supply the liquid fuel control valve 1K open liquid fuel 1c to the inner wall of the theoretical combustion chamber 4Q Supply superheated, superheated to super high pressure optimum temperature + 200MPa high temperature superheated steam 50 manufactured, superheated steam control valve 25 + oxygen control valve 24D + fuel control valve 25b opened, combustion near oxyfuel super high pressure center 3000 ° C or more The inner peripheral high-temperature water heating pipe 5H and the like are heated, and a part of the superheated steam 50 is aimed at the combustion in the vicinity of the center by the suction pyrolysis electrolysis oxygen oxygen hydrogen increase combustion, and the liquid oxygen 5K + liquid fuel on the inner wall of the theoretical combustion chamber 4Q 1c + high temperature water 52a is heated to produce superheated steam 50, fuel, oxygen, inner wall protection combustion or super high pressure / high temperature combustion at the optimum temperature, and open the high pressure / high temperature combustion gas control valve 5a (not shown) to drive the theoretical expansion engine 3Q. Then, the generator 1 is driven to store in the storage battery 1A, the storage battery driving wheel 4J is driven, and the CO2 exhaust 1/10 fuel cost 1/10 operating profit ratio is aimed at 10 times that of the existing automobile. To car 4L, to various energy saving cycle combined institutions and coalescence method.

Figure 9 The theoretical expansion engine 3Q drive of the theoretical combustion chamber 4Q, aiming to increase oxygen hydrogen in the ultra-high pressure extreme combustion of the oxygen coalescence screw ship 39Q, the horizontal full blade ratio material gravity turbine 8U fuel cost 0 power generation extremely cheap electric production The liquid oxygen 5K + electricity + high temperature water is received from the electricity + liquid air cold heat + high temperature water to superheated steam temperature heat supply facility 3D, and the liquid oxygen 5K is liquid compressed to reduce the compression volume work rate to 21 of air compression. / 60000 volumetric compression power, liquid oxygen 5K + liquid fuel 1c + high temperature water 52a is compressed to ultra high pressure such as 24-200 MPa by liquid fuel pump 4a + liquid oxygen pump 4b + water pump 4c, and liquid oxygen control valve 5T + liquid fuel Open control valve 1K + water control valve 5Q, heat to optimal temperature at theoretical combustion chamber 4Q inner wall, superheated steam control valve 25 + oxygen control valve 24D + fuel control valve 25b Open and burn at a temperature of 3000 ° C. or more near the super-high pressure fuel oxygen center, suck a part of superheated steam 50 into the near-center combustion, aim at pyrolytic electrolysis oxygen-hydrogen increase combustion, Liquid oxygen 5K + liquid fuel 1c + high temperature water 52a is heated to produce superheated steam 50, fuel, oxygen, inner wall protection combustion or super high pressure / high temperature combustion at optimum temperature, and high pressure / high temperature combustion gas control valve 5a is opened. Multiple drive options, screw drive and oxygen coalescence screw ship 39Q to drive, CO2 exhaust 1/10 fuel cost 1/10 operating profit rate 10 times that of existing ship, oxygen coalescence screw ship 39Q, various energy Use a storage cycle coalescence engine and coalescence method.

Fig. 10 Oxygen hydrogen injection by the theoretical combustion chamber 4Q aiming at increased oxygen and hydrogen combustion in the ultra high pressure limit combustion of the oxygen combined screw injection ship 39S, the theoretical expansion engine 3Q drive is a horizontal full blade ratio critical 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 receives liquid oxygen 5K + electricity + high temperature water, the screw drive by the theoretical expansion engine 3Q is the horizontal axis in Figure 5 Drive 1h or drive similar to that described in FIG. 9, the theoretical combustion chamber 4Q in FIG. 5 is moved to the oxygen combined water injection portion 88L as shown in FIG. 6, and the inlet of the air 28a is made as close to a straight line as possible. Provided as propulsion propulsion, equipped with intake air passage 5b around the leading theoretical combustion chamber 4Q combustion gas injection nozzle 6Y, jet bubbles are injected to the bottom of the jet combustion additional ship for rocket combustion, Six streamlined theoretical combustion chambers 4Q1 to 4Q1 are optimally adapted to the application, liquid oxygen 5K compression is set to 21/60000 volumetric compression work rate of air volumetric compression work rate, and combustion gas is obtained by superheated steam injection nozzle 6A injection targeting 200 MPa. Suction rocket injection, fuel injection nozzle 6X multiple jet combustion, sucking and injecting air in front, sucking and injecting water to make large and small ships, high speed ships and ultra high speed ships to be propelled, for rocket combustion Jet combustion added to increase combustion amount, oxygen combined water injection part 88L super high pressure mass combustion 100 times output target, 10% speed target injection propulsion of existing ship, same speed CO2 exhaust 1/10 fuel cost 1/10 Oxygen coalescence water injection unit 88L aiming at 10 times the operating profit rate of existing ships, and various energy conservation cycle coalescence engines and coalescence methods.

Fig. 11 Oxygen hydrogen increased combustion by the theoretical combustion chamber 4Q, aiming at increased oxygen hydrogen combustion in the ultra high pressure limit combustion of the oxygen combined injection ship 39R, the horizontal combined rotor blade critical material gravity turbine 8U fuel cost 0 power generation extremely cheap As shown in FIG. 6, liquid oxygen 5K + electricity + high temperature water is received from electricity + liquid air cold heat + high temperature water to superheated steam temperature heat supply equipment 3D, and the theoretical combustion chamber 4Q is supplied to the oxygen combined water injection unit 88L as shown in FIG. In FIG. 6, a streamlined theoretical combustion chamber 4Q1 is formed by using the air 28a around the leading theoretical combustion chamber 4Q as the intake air passage 5b and injecting and burning fuel into the intake air or the like from a plurality of fuel injection nozzles 6X to form rocket combustion + jet combustion. -A superheated steam injection nozzle aiming at 200MPa with a plurality of selections according to the application, liquid oxygen 5K compression and air volume compression work rate of 21/60000 volume compression work rate With A injection, internal combustion gas suction injection + jet combustion + forward air suction injection + forward water suction injection to make large and small ships, high-speed ships and ultra-high-speed ships to be propelled, jet for rocket combustion Combustion added to increase the combustion amount, the oxygen coalescence injection ship 39R injection propulsion air floating vertical parallel plate 9Q is wide, the air floating amount maximum + friction reduction amount maximum, oxygen combined water injection unit 88L ultra high pressure mass combustion The target is 100 times output, the target is 10 times the speed of the existing ship, the same speed CO2 exhaust 1/10 fuel cost 1/10 the operating profit ratio is 10 times that of the existing ship, oxygen combined water injection unit 88L Energy conservation cycle coalescence engine and coalescence method.

Fig. 12 Oxygen hydrogen injection in the theoretical combustion chamber 4Q, aiming at increased oxygen and hydrogen combustion in the ultra-high pressure extreme combustion of the oxygen combined injection airplane 39T, is driven by the horizontal full blade ratio critical material gravity turbine 8U fuel cost 0 power generation extremely cheap 7 from the electric + liquid air cold heat + high temperature water to superheated steam temperature heat supply equipment 3D of the electric manufacturing, the theoretical combustion chamber 4Q is received in the oxygen combined air injection unit 88B as shown in FIG. 7 streamlined theoretical combustion chambers 4Q1 to 4Q1 are formed by using the air 28a around the leading theoretical combustion chamber 4Q as the intake air passage 5b and performing fuel injection combustion on the intake air or the like from a plurality of fuel injection nozzles 6X to form rocket combustion + jet combustion. Select multiple units according to the application, liquid oxygen 5K compression, air volume compression work rate of 21/60000 volume compression work rate, superheated steam injection nose aiming at 200 MPa 6A injection, internal combustion gas suction injection + jet combustion + sucking and injecting forward air, rocket combustion + jet combustion, and propelling by jet combustion, and when going up into the universe, it will be a variety of airplanes that return to space by rocket combustion, Oxygen combined air injection unit 88B Super high pressure mass combustion 100 times output aim, enabling a day trip anywhere on the earth such as 16 rounds of space use in the space use prime day near fuel cost 0, CO2 exhaust at the same speed in the atmosphere 1/10 Fuel Cost 1/10 Operating Profit Margin Various energy storage cycle coalescence engines and coalescence methods are used, aiming for an oxygen coalescence air injection unit 88B, aiming 10 times that of existing airplanes.

Fig. 13 Oxygen-hydrogen propulsion aircraft 39U ultra-high pressure limit combustion aiming to increase oxygen and hydrogen combustion, Fig. 5 Theoretical combustion chamber 4Q theoretical expansion engine 3Q propeller 7A drive, horizontal all blade ratio material gravity turbine 8U fuel cost 0 power generation extreme Receives liquid oxygen 5K + electricity + high temperature water from electricity + liquid air cold heat + high temperature water to superheated steam temperature heat supply equipment 3D manufactured by low-cost electricity, and aims at 200 MPa by liquid compression, liquid oxygen control valve 5T + liquid fuel control valve 1K + water control valve 5Q is opened, the theoretical combustion chamber 4Q inner wall fuel heating pipe 1L + high temperature water heating pipe 5H + oxygen heating pipe 5F is heated to the optimum temperature, and the superheated steam 50, fuel and oxygen at the optimum temperature are converted into superheated steam. Open the control valve 25 + oxygen control valve 24D + fuel control valve 25b, burn at 3000 ° C. or more near the super high pressure fuel oxygen center, and part of the superheated steam 50 near the combustion center With the aim of suction pyrolysis electrolysis oxygen oxygen hydrogen increase combustion, protective combustion of the inner wall and ultra-high pressure high temperature combustion, 200MPa target superheated steam 50 is injected with superheated steam injection nozzle 6A, and combustion gas injection nozzle 6Y combustion gas 49 is suctioned and injected. The theoretical expansion engine which sucks and injects the compressed air portion 9D air of the compressed intake air passage 5b and the fuel injection nozzle 6X and greatly increases the fuel injection combustion combustion amount from the fuel injection nozzle 6X, thereby increasing the fuel combustion amount. 3Q driving, combustion gas 49 as high-pressure high-temperature combustion gas 49, theoretical expansion engine 3Q driving by circumferential direction injection of 380 degrees in the circumferential direction from the center, propeller 7A driving or rotor blade 7B driving by the horizontal axis 1h, in the atmosphere Combined with the combined oxygen and Fig. 12 with the same speed CO2 exhaust 1/10 aiming at fuel cost 1/10 and the operating profit rate aiming 10 times as much as the existing airplane. To propeller jet airplane 39N, to a variety of energy storage cycle combined institutions and coalescence method.

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 water at an exhaust temperature of 29 ° C. and a vacuum pressure of 30 mmHg, and assuming that the steam speed of the final moving blade group of the existing steam turbine is sonic, 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 becomes 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 use it for agriculture, industry, industry, mining, etc.

Horizontal type moving blade ratio critical material gravity turbine 8U power generation Extremely inexpensive power generation as an electric product prime, electric + liquid air cold heat + superheated steam temperature supply equipment 3D receives liquid oxygen 5K, driven by liquid oxygen and As a ship or airplane, liquid oxygen 5K is liquid-compressed to obtain 21/60000 volume compression work rate of the air volume compression work rate, and the theoretical expansion engine 3Q, the oxygen combined water injection unit 88L, and the oxygen combined air injection unit 88B are provided. Driving, there is a possibility that CO2 exhaust and fuel costs will be close to 1/10 in a car, a ship may be close to 10 times the speed with the same fuel cost, and an airplane will have a space arrival cost of 1 / 500,000, etc. There is a possibility of making a major revolution in the use of cold energy, such as making day trips anywhere on the planet as a prime use of space.

0: 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 engines and various energy coalescence means used to save and use the gravitational energy by ascending equipment) Machine, 1A: storage battery, 1B: pressure engine (oxygen pressure gear engine, oxygen pressure reciprocating engine, water pressure gear engine, water pressure reciprocating engine, etc., various engines for high-pressure injection of liquid) 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 infinite increase in pressure after increasing the amount of collected cold heat) 1K: liquid fuel control valve, 1L: Fuel heating pipe, 1Y: multi-stage combustion chamber (liquid oxygen and liquid nitrogen are separately compressed 24-200 MPa, combustion gas and nitrogen gas are separately manufactured, and combustion gas injection fuel injection fuel injection combustion inside and outside is performed multiple times in the injection or injection 1b: Fuel (liquid fuel + liquefiable gas fuel) 1b: Fuel pipe (provided so that the fuel injection temperature becomes the optimum temperature) 1c: Liquid fuel, 1d: Mercury, 1g: Gravity acceleration part 1h: horizontal axis, 2: solar heater (collects sunlight in a straight line with a long lens and heats the hot air forming the intake air) 2a: speeds up the natural phenomenon 2a: Speeding up natural phenomena (by generating cold water 28a and mixing cold water 28a in the power generation to supply the seawater to the seabed) 2a: Speeding up natural phenomena (supplying nutrients such as nitrogen, oxygen, and CO2 into the sea in the ocean, reducing the ability of microorganisms to digest tens of thousands of forests) Double target phytoplankton, seaweed, etc. Increase food for humans such as fish and kombu by breeding food chain, etc. 2b: Low water resistance (Air + combustion gas + superheated steam is jetted to the bottom of the ship to make water resistance low) 2c: insulation material, 2d: long lens (convex lens cross section linearly extended into a rectangular shape, multiple focal lengths aiming for maximum focal length lens width) 2e: water surface, 2A: heat-resistant material, 2B: heat absorbing material, 2C: 1 to multi-stage compression heat recovery device (Heat energy is air temperature, heat pump is compressed multiple times, heat is recovered multiple times in various heat exchangers such as 2C2X2Y2Z of 2C, and the remainder is divided and stored as warm 50 + liquid cold 28a) 2E: Specific critical substances (including alloys, platinum Sphere, gold sphere, tungsten alloy powder sintered sphere, silver sphere, copper sphere, tin sphere, lead sphere, zinc sphere, aluminum sphere, indium, cadmium, gallium, thallium, bismuth, etc. In the method, impact energy is reduced as the diameter decreases. For example, molten steel is injected into the atmosphere, and high-speed collision pulverization is used to produce ultra-small diameter steel balls by cooling with air cooling water. 2E: Specific critical substances (silicon resin coating and silica 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, coated lead alloy balls, coated zinc alloy balls・ Coated aluminum alloy balls) 2F: Specific critical material riser (gravity energy is increased and preserved) 2H: Cold seawater mixer (cooling seawater is mixed with cold heat to cool superheated vaporization heat in the process of speeding up natural phenomenon and condensate ) 2X: Air heat exchanger (the air is compressed with a heat pump at high temperature, heat recovery compressed air mass infinite increase or pressure infinite increase is aimed) 2Y: Compressed air heat exchanger (high temperature air or combustion gas is used for air cooling + superheated steam heat production 2Z: Specific material heat exchanger (used for temperature control of liquid metal below 500 degrees) 3a: Water repellent plating, 3A: Water repellent coating, 3B: Water pressure reciprocating engine (Water in multi-stage oxygen pressure reciprocating engine) 3D: Electricity + liquid air cold heat + superheated steam heat supply equipment (cooling + heat production by gravity power generation and supplying liquid oxygen and liquid nitrogen to supply liquid oxygen and liquid nitrogen) Cars, ships and airplanes Methane is injected into the methane hydrate supplied with overheated steam or superheated steam, etc. Recovery of methane, etc. Electricity + cold heat + warm use intensive 3E: Specific critical substances (specific critical liquid substances such as mercury and water at room temperature) 3E: Specific critical substances ( Low-melting-point alloy 500 ° C or less liquid and stable high-temperature liquid alloy) 3F: Oxygen pressure reciprocating engine (liquid oxygen, liquid nitrogen and fuel are used as injection combustion 24-200MPa combustion gas, fuel injection multistage combustion in the process of expansion, multistage oxygen 3G: Theoretical combustion gear engine (liquid oxygen + liquid fuel + water is compressed and heated to inject and burn) 3H: Reciprocating piston, 3J: Theoretical combustion reciprocating engine (liquid acid) 3K: External gear 3L: Multistage combustion chamber 3M: Steam pressure reciprocating engine (Multistage oxygen pressure reciprocating engine multistage heating water and steam to multistage steam pressure reciprocating engine) 3N: Steam pressure gear engine (multistage oxygen pressure gear engine multistage heating water and steam to drive the multistage steam pressure gear engine) 3P: Theoretical expansion engine (the volume of gas is inversely proportional to pressure) 3Q: Theoretical expansion engine (best engine + aiming at the highest acceleration drive in vacuum by Boyle's law) 3R: Theoretical gas turbine (theoretical best gas turbine whose gas volume is inversely proportional to pressure) 3S: Theoretical steam turbine (theoretical best steam turbine whose gas volume is inversely proportional to pressure) 3T: Theoretical gas compressor (theoretical best gas pressure whose gas volume is inversely proportional to pressure) 3U: Theoretical turbine, 3V: Pump engine (uses existing pumps in the engine) 3X: Compressor engine (uses existing compressors in the engine) 3Y: Counter-rotating engine (gas volume is inversely proportional to pressure) 3Z: Oxygen pressure gear engine (liquid oxygen, liquid nitrogen, and fuel injection combustion is used to make a combustion gas of 24 to 200 MPa, and water and water vapor on the inner and outer circumferences are heated by multistage combustion and linked to the multistage water pressure gear engine) 3a: water repellent plating, 3b: water repellent coating, 4C: counter-synchronous gear, 4D: series co-rotating gear, 4F: combustion gas reciprocating engine, 4H: heat absorption tube (long lens 2d makes sunlight into heat absorption tube straight 4J: storage battery drive wheel, 4K: theoretical expansion engine vehicle, 4L: theoretical expansion engine vehicle, 4Q: theoretical combustion chamber ( 4W: Theoretical compression chamber, 4Y: Theoretical combustion chamber (combustion chamber for high-temperature pyrolysis, electrolysis combustion, and water, aiming at compound 0) 4Z: Combustion gas gear engine, 4X: Turbine blade 4a: Liquid fuel pump, 4b: Liquid oxygen pump, 4c: Water pump, 4d: Gear device, 4e: Roller, 4f: Rotation support, 5: Air injection nozzle, 5a: High pressure High-temperature combustion gas control valve, 5b: Compressed intake air passage, 5d: Combustion flow inner wall, 5e: Ultra-high pressure oxygen, 5A: Supply valve, 5B: Cooling fin, 5C: Exhaust chamber 5D: Exhaust valve 5E: Supply chamber 5F : Oxygen heating pipe, 5G: Steam heating pipe, 5H: High temperature water heating pipe, 5K: Liquid oxygen, 5K: Liquid oxygen chamber, 5L: Liquid nitrogen, 5L: Liquid nitrogen chamber, 5M: High pressure high temperature combustion gas, 5M: High pressure High temperature combustion 5N: high pressure high temperature steam chamber, 5N: high pressure high temperature steam chamber, 5P: water vapor control valve, 5Q: water control valve, 5R: superheated steam control valve, 5S: compressed air heating pipe, 5T: liquid oxygen control valve, 6 : Final compression blade, 6A: superheated steam injection nozzle, 6B: compressed air injection nozzle, 6E: specific material injection nozzle, 6F: water injection nozzle, 6G: stationary blade, 6H: drain pipe, 6L: oxygen injection nozzle, 6W : Specific critical material accelerator (liquid specific critical material 3E pressure and specific gravity difference using specific gravity 3E or 2E mixed injection) 6X: Fuel injection nozzle, 6X: Afterburner (fuel injection cold heat 28a combustion flow 6Y into suction air flow) 6Y: Combustion gas injection nozzle (cold heat 28a combustion flow) 6Z: Steam injection nozzle, 7A: Propeller, 7B: Rotary blade, 7C: Scribing -, 8c: Turbine blades (a straight long turbine blade is provided on the outer surface of the cylinder to aim for fully automatic machining and weight reduction of the inner and outer circumferences) 8d: upper expansion blade group, 8e: lower expansion blade group, 8f: assembly turbine Blade group, 8g: Upper compression blade group, 8h: Lower compression blade group, 8j: Assembly compression blade group, 8A: Cylindrical turbine blade group (enables fully automatic machining and precision assembly as a horizontal cylindrical turbine blade group) 8S: Horizontal all-blade turbine (opposite all-blade pusher turbine series full-blade pusher turbine turbine biting all-blade pusher turbine) 8S: Horizontal all-blade turbine (with linear long turbine blades on the outer surface of the cylinder, all on the inner and outer circumferences) 8S: Horizontal type full-blade water gravity turbine (existing steam turbine is a stationary blade and the damming output approaches 0 because all blades are indispensable and the work rate is 1 / 3.6 that of platinum balls) Vital material vacuum degree because it is extremely small 8M: Vertical type moving blade water gravity turbine (6 types of cylindrical turbine moving blade group fitting assembly + magnetic utilization bearing load approach 0) 8N: Vertical type full moving blade specific gravity Large material gravity turbine (6 types of cylindrical turbine blade group fitting assembly + magnetic utilization bearing load approach 0) 8R: Horizontal full blade water gravity turbine (cylindrical turbine blade group series opposed synchronous rotation + magnetic utilization bearing load 0) 8S: Horizontal all-blade ratio critical material gravity turbine (cylindrical turbine blade group series opposed synchronous rotation + magnetic utilization bearing load 0 approach) 8P: Vertical type all-blade water gravity turbine (6 types of cylindrical turbines) Rotor blade grouping assembly + Magnetically utilized bearing load 0 approach + Super high speed peripheral speed) 8Q: Vertical type whole blade ratio material gravity turbine (6 types of cylindrical turbine blade group fitting assembly + magnetic bearing load) 0 approach + super high speed circumference 8T: Horizontal all-blade water gravity turbine (cylindrical turbine blade group serially opposed synchronous rotation + magnetic utilization bearing load 0 approach + super high speed peripheral speed) 8U: Horizontal all-blade ratio critical material gravity turbine (cylindrical) Turbine blade series synchronous rotation + magnetic bearing load approaching 0 + super high speed peripheral speed) 9: Wear resistant annular assembly (fitting assembly that reduces the weight of specific critical material including 8c with cemented carbide and reduces weight Method) 9A: Cylindrical ring assembly (6 types of wear-resistant cylindrical ring assembly moving blade group makes structure simple, few parts, fully automatic machining, easy assembly, light weight easy, etc.) 9A: Cylindrical ring assembly ( The outer cylindrical blade group 60D is configured by fitting the fixed inlet outer blade 60E + outer annular blade 60G + outlet fixed outer blade 60J, and the inner cylindrical blade group 60C by fitting the fixed inlet inner blade 60F + inner annular blade 60H + outlet fixed inner blade 60K. a configuration 9B: Repulsive permanent magnet, 9C: Suction permanent magnet, 9D: Compressed air part, 9E: Vacuum part, 9Q: Vertical parallel plate (vertical parallel plate for guiding the blast air to the storage stern) 10: Hull, 10A: Ship cabin, 10b: Cockpit, 10c: Control room, 10d: Guest room, 10e: Cargo compartment, 16: Horizontal shaft plate (disc for facilitating precision assembly) 16A: Horizontal shaft, 11D: Cooling chamber dedicated to gas, 21 : Solar heater (mainly used with the intake air passage also 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 (compressed and stored in the form of 50 heat of compressed air calorie compressed air 28a + compressed air 28a cold containing liquid oxygen and liquid nitrogen by compressing air 28a with a heat pump) 28b: compressed air Calorie , 28A: intake air passage, 28B: air passage inlet, 38: rotation guide, 38a: flight trunk, 38b: flight wing, 38c: flight tail, 38d: vertical wing, 38e: leading edge of the wing, 38g: surface wing 38h: Ascending boat, 38B: Air suction jet ship (with 79S79T79Y79Z) 38C: Water suction jet ship (with 79U79X) 39A: Solar thermal gravity plane, 39B: Solar thermal gravity rotating plane, 39C: Solar thermal gravity helicopter, 39D: Screw ship, 39G: Solar thermal gravity flight vessel, 39H: Oxygen coalescence screw vessel, 39J: Oxygen coalescence injection vessel, 39K: Oxygen coalescence screw injection vessel, 39L: Oxygen coalescence injection aircraft, 39M: Oxygen coalescence propeller aircraft,
39N: oxygen coalescence propeller jet plane, 39P: oxygen coalescence rotorcraft, 39Q: oxygen coalescence screw ship, 39R: oxygen coalescence jet ship, 39S: oxygen coalescence screw jet ship, 39T: oxygen coalescence jet airplane, 39U: oxygen coalescence propeller Airplane, 40A: Rudder, 49: Combustion gas, 50: Superheated steam, 50: Superheated steam chamber, 50: Heat (compressed air 28a with a heat pump and divided into 50 heat of compressed air calorie heat + compressed air 28a cold) 50A: Water vapor, 50a: Superheated steam injection pipe, 51: Air extractor, 51: Merge extractor (extractor for joining) 51A: Air extraction chamber, 52a: Hot water 52a: Deep ocean water, 52b: High temperature water, 52d: Heat (change from 50) 52e: Cold (change from 28a) 55B: Transmission, 60A: Inner shaft device (Turbine blade equipped device) 60B: Outer shaft device (turbine blade equipped device) 60C: Cylindrical inner moving blade group (Wear resistant cylindrical annular assembly fixed moving blade group including fully automatic processing easy assembly) 60D: Cylindrical outer side Rotor blade group (Wear resistant cylindrical annular assembly fixed rotor blade group including fully automatic machining easy assembly) 60E: Entrance fixed outer blade (inlet blade fixing annular outer ring blade assembly) 60F: Entrance fixed inner blade (Inlet blade for annular assembly fixing inner rotor blade group) 60G: Outer annular blade (intermediate blade for annular assembly of outer rotor blade group) 60H: Inner annular blade (intermediate blade for annular assembly of inner rotor blade group) 60J: Outlet Fixed outer wing (outlet blade for annular assembly fixing outer rotor blade group) 60K: Outlet fixed inner wing (exit blade for annular assembly fixing inner rotor blade group) 76: gear device (including magnetic friction power transmission device) 77B: Semi-cylindrical outer box, 77F: Outside injection section , 77G: Cylindrical rotating part, 77a: Turbine outer casing, 80: Bearing (including magnetic bearing + air bearing) 80a: Thrust bearing (including magnetic bearing + air bearing) 80A: Joint, 80B: Fastener, 80Y: Liquid air Suction water jet (high pressure high temperature combustion gas 5M received high pressure high temperature steam chamber 5N, fuel injected and burned into 5M multiple times, injected 5N heated multiple times from inner and outer peripheries, air sucked and injected into water 80Z: Liquid air suction water jet (high pressure high temperature combustion gas 5M receiving high pressure high temperature steam chamber 5N, fuel injection combustion in 5M multiple times, 5N is heated multiple times from the inner circumference and inner circumference outer circumference several times Injecting, fuel injection combustion injection to a plurality of locations of air suction flow, air suction injection and water suction injection) 84: Counter-rotating magnetic friction device (fixed portion inner blade group and outer blade group) Almost the same speed 84Y: Counter-rotating gear device (same as in existing technology) 85: Counter-rotating magnetic device (magnet-use gear height from slight to non-contact and rotating in the opposite direction by a horizontal shaft 1h gear) 85Y: Counter-rotating gear device (reciprocally rotated with the existing horizontal shaft 1h gear) 88A: Oxygen combined air injection unit (rocket injection + jet combustion + combined steam injection and the like) 88B: Oxygen combined air injection unit (super High pressure rocket combustion + jet combustion + superheated steam injection suction) 88K: Oxygen combined water injection part (rocket combustion + jet combustion + steam injection and combined injection) 88L: Oxygen combined water injection part (super high pressure rocket combustion + jet combustion + superheat) 95a: Combustion gas reservoir, 95b: Compressed air reservoir, 95c: Superheated steam reservoir, 103: Cold heat recovery device,

Claims (377)

  A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, and a series rotation gear (4D) between the horizontal axes (16A), and a pair of vertical rotations in the same direction at the same speed rotation. + Various energy storage cycle coalescence engine and coalescence method for generating 1 to 20 sets of horizontal gravity blade (8U) critical material gravity turbine (8U) with super high speed circumferential speed.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, and a series rotation gear (4D) between the horizontal axes (16A), and a pair of vertical rotations in the same direction at the same speed rotation. + Various energy storage cycle coalescing engine and coalescence method for generating 21 to 40 sets of gravity-type gravity turbine (8U) horizontal full blade ratio material with ultra-high speed circumferential speed.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, and a series rotation gear (4D) between the horizontal axes (16A), and a pair of vertical rotations in the same direction at the same speed rotation. + Various energy storage cycle coalescence engine and coalescence method for generating 41-60 sets of horizontal turbine blade critical material gravity turbine (8U) with ultra-high speed circumferential speed.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, and a series rotation gear (4D) between the horizontal axes (16A), and a pair of vertical rotations in the same direction at the same speed rotation. + Various energy storage cycle coalescence engine and coalescence method for generating 61 to 80 sets of horizontal all-blade ratio critical material gravity turbine (8U) with super high speed circumferential speed.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, and a series rotation gear (4D) between the horizontal axes (16A), and a pair of vertical rotations in the same direction at the same speed rotation. + Various energy storage cycle coalescing engine and coalescence method for generating a power generator with a total gravity of 81 to 100 horizontal gravity blades (8U) with a super high speed circumferential speed.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, and a series rotation gear (4D) between the horizontal axes (16A), and a pair of vertical rotations in the same direction at the same speed rotation. + Horizontal type full blade ratio material gravity turbine (8U) 101-120 sets of power generation with super high speed circumferential speed.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, and a series rotation gear (4D) between the horizontal axes (16A), and a pair of vertical rotations in the same direction at the same speed rotation. + Various energy storage cycle coalescence engines and coalescence methods for generating a power generator of a horizontal all-blade ratio critical material gravity turbine (8U) 121-140 with ultra-high speed circumferential speed.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, and a series rotation gear (4D) between the horizontal axes (16A), and a pair of vertical rotations in the same direction at the same speed rotation. + Various energy storage cycle coalescence engine and coalescence method for generating a power generation of a horizontal all-blade ratio critical material gravity turbine (8U) 141-160 with ultra-high speed circumferential speed.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, and a series rotation gear (4D) between the horizontal axes (16A), and a pair of vertical rotations in the same direction at the same speed rotation. + Various energy storage cycle coalescence engines and coalescence methods for generating a set of horizontal full-blade ratio critical material gravity turbine (8U) 161-180 sets at an ultra-high speed circumferential speed.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, and a series rotation gear (4D) between the horizontal axes (16A), and a pair of vertical rotations in the same direction at the same speed rotation. + Various energy storage cycle coalescence engines and coalescence methods for generating a power generator of a horizontal all-blade ratio critical material gravity turbine (8U) 181 to 200 sets at an ultra-high speed circumferential speed.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Various energy storage cycle coalescence engines and coalescence methods for generating 1-20 sets of horizontal full-blade ratio critical material gravity turbines (8U) with magnetic bearing loads approaching 0 and super-high speed circumferential speed driven by Mach 1-30 .   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Various energy storage cycle coalescence engines and coalescence methods for generating a power generation by using a horizontal full-blade ratio critical material gravity turbine (8U) 21-40 sets with a magnetic bearing load of 0 approaching to Mach 1-30 and an ultra-high speed circumferential speed. .   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Various energy storage cycle coalescence engine and coalescence method for generating 41-60 sets of horizontal full-blade ratio critical material gravity turbine (8U) with a magnetic bearing load of 0 approaching Mach 1-30 and an ultra-high speed circumferential speed .   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Various energy storage cycle coalescence engine and coalescence method for generating a horizontal full-blade ratio critical material gravity turbine (8U) 61-80 sets with magnetic bearing load 0 approaching + super high speed circumferential speed driven by Mach 1-30 .   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Various energy storage cycle coalescence engine and coalescence method for generating a horizontal all-blade ratio critical material gravity turbine (8U) 81 to 100 sets with magnetic bearing load 0 approaching + super high speed circumferential speed driven by Mach 1-30 .   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Various energy storage cycle coalescence engine and coalescence method for generating a horizontal all-blade ratio critical material gravity turbine (8U) 101-120 sets with a magnetic bearing load of 0 driven by Mach 1-30 and approaching super high speed + circumferential speed .   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Various energy storage cycle coalescence engine and coalescence method for generating a horizontal all-blade ratio critical material gravity turbine (8U) 121-140 sets with a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed driven by Mach 1-30 injection .   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Various energy storage cycle coalescence engine and coalescence method for generating power by using magnetically driven bearings of Mach 1 to 30 and using a horizontal all-blade ratio critical material gravity turbine (8U) 141 to 160 set at 0 approaching super high speed and circumferential speed. .   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Various energy storage cycle coalescence engine and coalescence method for generating a horizontal full-blade ratio critical material gravity turbine (8U) 161-180 sets with a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed driven by Mach 1-30 .   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Various energy storage cycle coalescence engine and coalescence method for generating a horizontal all-blade ratio critical material gravity turbine (8U) 181-200 sets with a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed driven by Mach 1-30 .   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Aiming at Mach 30, the injection ratio critical material (2E) is driven by mixed injection acceleration. Magnetically utilized bearing load approaching 0 + Super high speed circumferential speed with a full blade ratio critical material gravity turbine (8U) 1-20 sets of power generation Various energy storage cycle coalescence engines and coalescence methods.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Aiming at Mach 30, the injection ratio critical material (2E) is driven by mixed injection acceleration. Magnetically utilized bearing load approaching 0 + Ultra-high speed circumferential speed of the critical blade gravity material (8U) 21-40 sets of power generation Various energy storage cycle coalescence engines and coalescence methods.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Aiming at Mach 30, the injection ratio critical substance (2E) is driven by mixed injection acceleration. Magnetically utilized bearing load approaching 0 + Super high speed circumferential speed with a full blade ratio critical substance gravity turbine (8U) 41-60 sets of power generation Various energy storage cycle coalescence engines and coalescence methods.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Aiming at Mach 30, the injection ratio critical material (2E) is driven by mixed injection acceleration. Magnetically utilized bearing load approaching 0 + Ultra high speed circumferential speed horizontal material ratio specific gravity material gravity turbine (8U) 61-80 sets of power generation Various energy storage cycle coalescence engines and coalescence methods.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Aiming at Mach 30, the injection ratio critical material (2E) is driven by mixed injection acceleration. Magnetically utilized bearing load approaching zero + super high speed circumferential speed with a full blade ratio critical material gravity turbine (8U) 81-100 sets of power generation Various energy storage cycle coalescence engines and coalescence methods.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Aiming at Mach 30, the injection ratio critical substance (2E) is driven by mixed injection acceleration. Magnetically utilized bearing load approaching 0 + Super high speed circumferential speed with a full blade ratio critical substance gravity turbine (8U) 101-120 sets of power generation Various energy storage cycle coalescence engines and coalescence methods.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Aiming at Mach 30, the injection ratio critical material (2E) is driven by mixed injection acceleration. Magnetically utilized bearing load approaching 0 + Ultra-high speed circumferential speed with a full blade ratio critical material gravity turbine (8U) 121-140 power generation Various energy storage cycle coalescence engines and coalescence methods.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Aiming at Mach 30, the injection ratio critical material (2E) is driven by mixed injection acceleration. Magnetically utilized bearing load approaching 0 + Ultra-high speed circumferential speed with a full blade ratio critical material gravity turbine (8U) 141 to 160 sets of power generation. Various energy storage cycle coalescence engines and coalescence methods.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Aiming at Mach 30, the injection ratio critical material (2E) is driven by mixed injection acceleration. Magnetically utilized bearing load approaching 0 + Ultra high speed circumferential speed with a full blade ratio critical material gravity turbine (8U) 161-180 sets of power generation Various energy storage cycle coalescence engines and coalescence methods.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Aiming at Mach 30, the injection ratio critical substance (2E) is driven by mixed injection acceleration. Magnetically utilized bearing load approaching 0 + Ultra-high speed circumferential speed with a full blade ratio critical substance gravity turbine (8U) 181 to 200 sets of power generation Various energy storage cycle coalescence engines and coalescence methods.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal shafts (16A), and a set of each set rotating in the same vertical direction and at the same speed, allowing the entire inner diameter to be cut. Various energy storage cycle coalescence engine and coalescence method for generating 1 to 20 sets of horizontal full-blade ratio critical material gravity turbine (8U) with a magnetic utilization bearing load of 0 approaching diameter + super high speed circumferential speed.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal shafts (16A), and a set of each set rotating in the same vertical direction and at the same speed, allowing the entire inner diameter to be cut. Various energy storage cycle coalescence engine and coalescence method for generating 21-40 sets of gravity-type gravity turbine (8U) horizontal-type moving blade ratio critical material having a magnetic bearing load of 0 approaching diameter + super high speed circumferential speed.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal shafts (16A), and a set of each set rotating in the same vertical direction and at the same speed, allowing the entire inner diameter to be cut. Various energy storage cycle coalescence engine and coalescence method for generating 41-60 sets of horizontal full-blade ratio critical material gravity turbine (8U) with a magnetic utilization bearing load of 0 approaching diameter + super high speed circumferential speed.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal shafts (16A), and a set of each set rotating in the same vertical direction and at the same speed, allowing the entire inner diameter to be cut. Various energy storage cycle coalescence engine and coalescence method for generating a set of 61 to 80 sets of horizontal full-blade ratio critical material gravity turbine (8U) with a magnetic utilization bearing load of 0 approaching diameter + super high speed circumferential speed.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal shafts (16A), and a set of each set rotating in the same vertical direction and at the same speed, allowing the entire inner diameter to be cut. Various energy storage cycle coalescence engine and coalescence method for generating 100 to 100 sets of horizontal full-blade ratio critical material gravity turbine (8U) with a magnetic bearing load of 0 approaching diameter + super high speed circumferential speed.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal shafts (16A), and a set of each set rotating in the same vertical direction and at the same speed, allowing the entire inner diameter to be cut. Various energy storage cycle coalescence engine and coalescence method for generating a power generation of a horizontal full blade ratio critical material gravity turbine (8U) 101-120 sets with a magnetic utilization bearing load of 0 approaching diameter + super high speed circumferential speed.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal shafts (16A), and a set of each set rotating in the same vertical direction and at the same speed, allowing the entire inner diameter to be cut. Various energy storage cycle coalescence engine and coalescence method for generating a power generation of a horizontal full blade ratio critical material gravity turbine (8U) 121-140 with a diameter-based magnetic bearing load approaching 0 and an ultra-high speed circumferential speed.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal shafts (16A), and a set of each set rotating in the same vertical direction and at the same speed, allowing the entire inner diameter to be cut. Various energy storage cycle coalescence engine and coalescence method for generating a set of horizontal full blade ratio critical material gravity turbines (8U) 141-160 with a diameter-based magnetic bearing load approaching 0 and an ultra-high speed circumferential speed.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal shafts (16A), and a set of each set rotating in the same vertical direction and at the same speed, allowing the entire inner diameter to be cut. Various energy storage cycle coalescence engine and coalescence method for generating a set of horizontal full-blade ratio critical material gravity turbine (8U) 161-180 sets with a diameter-based magnetic bearing load approaching 0 and an ultra-high speed circumferential speed.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal shafts (16A), and a set of each set rotating in the same vertical direction and at the same speed, allowing the entire inner diameter to be cut. Various energy storage cycle coalescence engines and coalescence methods for generating a power generation by using a horizontal full blade ratio critical material gravity turbine (8U) 181 to 200 sets with a magnetic bearing load of 0 approaching diameter + super high speed circumferential speed.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) The inner diameter driven by Mach 1 to 30 can be cut all over the surface. The maximum diameter of the magnetically utilized bearing load is close to 0 + super high speed circumferential speed. Energy conservation cycle coalescence engine and coalescence method.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) The inner diameter driven by Mach 1 to 30 can be cut all over the surface. The maximum diameter of the magnetically utilized bearing load is close to 0 + super high speed circumferential speed. Energy conservation cycle coalescence engine and coalescence method.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) The inner diameter driven by Mach 1 to 30 can be cut all over the surface The maximum diameter of the magnetically utilized bearing load is close to 0 + super high speed circumferential velocity ratio of the all-blade blade critical material gravity turbine (8U) 41-60 various power generation Energy conservation cycle coalescence engine and coalescence method.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) The inner diameter driven by Mach 1 to 30 can be cut all over the surface. The maximum diameter of the magnetically utilized bearing load is close to 0 + super high speed circumferential speed. Energy conservation cycle coalescence engine and coalescence method.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) The inner diameter driven by Mach 1 to 30 can be cut all over the surface. The maximum diameter of the magnetically utilized bearing load is close to 0 + super high speed circumferential speed. Energy conservation cycle coalescence engine and coalescence method.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) The inner diameter driven by Mach 1 to 30 can be cut all over the surface The maximum diameter of the magnetically utilized bearing load close to 0 + super high speed circumferential speed with a serious blade gravity material (8U) 101-120 Energy conservation cycle coalescence engine and coalescence method.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) The inner diameter driven by Mach 1 to 30 can be cut all over the surface The maximum diameter of the magnetically utilized bearing load is close to 0 + super high speed circumferential speed with all the blade ratio critical material gravity turbine (8U) 121-140 various power generation Energy conservation cycle coalescence engine and coalescence method.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) The inner diameter driven by Mach 1 to 30 can be cut all over the surface. The maximum diameter of the magnetically utilized bearing load is close to 0 + super high speed circumferential speed. Energy conservation cycle coalescence engine and coalescence method.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) The inner diameter driven by Mach 1 to 30 can be cut all over the surface The maximum diameter of the magnetically utilized bearing load close to 0 + super high speed circumferential speed with a serious blade gravity material (8U) 161-180 Energy conservation cycle coalescence engine and coalescence method.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) The inner diameter driven by Mach 1 to 30 can be cut all over the surface. The maximum diameter of the magnetically utilized bearing load is close to 0 + the super-high speed circumferential speed. Energy conservation cycle coalescence engine and coalescence method.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Aiming at Mach 30, the injection ratio critical material (2E) is driven by mixed injection acceleration. The whole inner diameter can be cut. Experiment using the maximum diameter magnetic bearing load close to 0 + Super high speed circumferential speed with a full blade ratio critical material gravity turbine (8U) ) Various energy storage cycle coalescence engines and coalescence methods for generating 1 to 20 sets of power.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Aiming at Mach30, injection ratio critical material (2E) is mixed and accelerated. Full internal diameter cutting is possible. Experiment using the maximum diameter magnetic bearing load approaching zero + ultra-high speed circumferential speed ratio material gravity turbine (8U) ) Various energy storage cycle coalescence engines and coalescence methods for generating 21 to 40 sets of power.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Aiming at Mach30, injection ratio critical material (2E) is mixed and accelerated. Full internal diameter cutting is possible. Experiment using the maximum diameter magnetic bearing load approaching zero + ultra-high speed circumferential speed ratio material gravity turbine (8U) ) Various energy storage cycle coalescence engines and coalescence methods for generating 41 to 60 sets of power.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Aiming at Mach30, injection ratio critical material (2E) is mixed and accelerated. Full internal diameter cutting is possible. Experiment using the maximum diameter magnetic bearing load approaching zero + ultra-high speed circumferential speed ratio material gravity turbine (8U) ) 61-80 sets of various energy storage cycle coalescence engines and coalescence methods.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Aiming at Mach 30, the injection ratio critical material (2E) is driven by mixed injection acceleration. The whole inner diameter can be cut. Experiment using the maximum diameter magnetic bearing load close to 0 + Super high speed circumferential speed with a full blade ratio critical material gravity turbine (8U) ) Various energy storage cycle coalescence engines and coalescence methods for generating 81 to 100 sets of power.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Aiming at Mach30, injection ratio critical material (2E) is mixed and accelerated. Full internal diameter cutting is possible. Experiment using the maximum diameter magnetic bearing load approaching zero + ultra-high speed circumferential speed ratio material gravity turbine (8U) ) Various energy storage cycle coalescence engines and coalescence methods for generating 101 to 120 sets of power.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Aiming at Mach 30, the injection ratio critical material (2E) is driven by mixed injection acceleration. The whole inner diameter can be cut. Experiment using the maximum diameter magnetic bearing load close to 0 + Super high speed circumferential speed with a full blade ratio critical material gravity turbine (8U) ) Various energy storage cycle coalescence engines and coalescence methods for generating 121 to 140 sets of power.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Aiming at Mach30, injection ratio critical material (2E) is mixed and accelerated. Full internal diameter cutting is possible. Experiment using the maximum diameter magnetic bearing load approaching zero + ultra-high speed circumferential speed ratio material gravity turbine (8U) ) 141 to 160 sets of various energy storage cycle coalescence engines and coalescence methods.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Aiming at Mach30, injection ratio critical material (2E) is mixed and accelerated. Full internal diameter cutting is possible. Experiment using the maximum diameter magnetic bearing load approaching zero + ultra-high speed circumferential speed ratio material gravity turbine (8U) ) Various energy storage cycle coalescence engines and coalescence methods for generating 161 to 180 power sets.   A horizontal shaft (16A) is fixed to both sides of the cylindrical turbine blade group (8A) with a horizontal shaft plate (16), and a pair of opposed synchronous gears (4C) is mounted on the horizontal shaft (16A). ) A pair of counter-synchronous rotations, a series of co-rotating gears (4D) between the horizontal axes (16A), and a pair of vertical and same-direction rotating speeds, and a specific material (3E) Aiming at Mach30, injection ratio critical material (2E) is mixed and accelerated. Full internal diameter cutting is possible. Experiment using the maximum diameter magnetic bearing load approaching zero + ultra-high speed circumferential speed ratio material gravity turbine (8U) ) Various energy storage cycle coalescence engines and coalescence methods for generating 181 to 200 sets of power.   A pair of two horizontal shafts (16A) fixed with horizontal shaft plates (16) on both sides of the cylindrical turbine blade group (8A), which is a wear-resistant super-water-repellent plating (3a). Various energy storage cycle coalescence engines and coalescence methods for generating 1 to 20 sets of a horizontal all-blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed.   A pair of two horizontal shafts (16A) fixed with horizontal shaft plates (16) on both sides of the cylindrical turbine blade group (8A), which is a wear-resistant super-water-repellent plating (3a), to form an opposed series full blade impeller turbine. Various energy storage cycle coalescence engines and coalescence methods for generating a power generation of a gravity-type gravity turbine (8U) 21-40 sets of horizontal type blades with a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed.   A pair of two horizontal shafts (16A) fixed with horizontal shaft plates (16) on both sides of the cylindrical turbine blade group (8A), which is a wear-resistant super-water-repellent plating (3a). Various energy storage cycle coalescence engines and coalescence methods for generating 41-60 power generations of a horizontal full-blade ratio critical material gravity turbine (8U) with a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed.   A pair of two horizontal shafts (16A) fixed with horizontal shaft plates (16) on both sides of the cylindrical turbine blade group (8A), which is a wear-resistant super-water-repellent plating (3a). Various energy storage cycle coalescence engines and coalescence methods for generating a set of horizontal material-powered blade ratio critical material gravity turbine (8U) 61-80 with magnetic bearing load approaching 0 + super high speed circumferential speed.   A pair of two horizontal shafts (16A) fixed with horizontal shaft plates (16) on both sides of the cylindrical turbine blade group (8A), which is a wear-resistant super-water-repellent plating (3a), to form an opposed series full blade impeller turbine. Various energy storage cycle coalescence engines and coalescence methods for generating a power generation of a horizontal-type full-blade ratio critical material gravity turbine (8U) 81 to 100 with a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed.   A pair of two horizontal shafts (16A) fixed with horizontal shaft plates (16) on both sides of the cylindrical turbine blade group (8A), which is a wear-resistant super-water-repellent plating (3a). Various energy storage cycle coalescence engine and coalescence method for generating 100 to 120 sets of horizontal full blade ratio gravity material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed.   A pair of two horizontal shafts (16A) fixed with horizontal shaft plates (16) on both sides of the cylindrical turbine blade group (8A), which is a wear-resistant super-water-repellent plating (3a). Various energy storage cycle coalescence engine and coalescence method for generating a horizontal all-blade ratio critical material gravity turbine (8U) 121-140 power generation with magnetic bearing load approaching 0 + super high speed circumferential speed.   A pair of two horizontal shafts (16A) fixed with horizontal shaft plates (16) on both sides of the cylindrical turbine blade group (8A), which is a wear-resistant super-water-repellent plating (3a), to form an opposed series full blade impeller turbine. Various energy storage cycle coalescence engine and coalescence method for generating a horizontal all-blade ratio critical material gravity turbine (8U) 141-160 power generation with magnetic utilization bearing load approaching 0 + super high speed circumferential speed.   A pair of two horizontal shafts (16A) fixed with horizontal shaft plates (16) on both sides of the cylindrical turbine blade group (8A), which is a wear-resistant super-water-repellent plating (3a), to form an opposed series full blade impeller turbine. Various energy storage cycle coalescence engine and coalescence method for generating a set of horizontal full blade ratio critical material gravity turbine (8U) 161-180 sets with magnetic bearing load approaching 0 + super high speed circumferential speed.   A pair of two horizontal shafts (16A) fixed with horizontal shaft plates (16) on both sides of the cylindrical turbine blade group (8A), which is a wear-resistant super-water-repellent plating (3a), to form an opposed series full blade impeller turbine. Various energy storage cycle coalescence engine and coalescence method for generating a total gravity blade (8U) 181 to 200 sets of a horizontal all-blade ratio critical material with a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed.   A magnet with a wear-resistant super-water-repellent plating (3a), with two horizontal shafts (16A) fixed to both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a series full-blade propeller turbine. Various energy storage cycle coalescence engines and coalescence methods for generating 1 to 20 sets of horizontal-type full blade ratio critical material gravity turbine (8U) with a bearing load approaching 0 and an ultra-high speed circumferential speed.   A magnet with a wear-resistant super-water-repellent plating (3a), a set of two horizontal shafts (16A) fixed on both sides of a cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a series full blade impeller turbine. Various energy storage cycle coalescence engine and coalescence method for generating a set of 40 to 40 horizontal gravity blade critical material gravity turbines (8U) with a bearing load approaching 0 and an ultra-high speed circumferential speed.   A magnet with a wear-resistant super-water-repellent plating (3a), a set of two horizontal shafts (16A) fixed on both sides of a cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a series full blade impeller turbine. Various energy storage cycle coalescence engines and coalescence methods for generating 41-60 sets of horizontal-type full blade ratio critical material gravity turbine (8U) with a bearing load approaching 0 and an ultra-high speed circumferential speed.   A magnet with a wear-resistant super-water-repellent plating (3a), with two horizontal shafts (16A) fixed to both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a series full-blade propeller turbine. Various energy storage cycle coalescence engine and coalescence method for generating a set of 80 to 80 generators of a horizontal all-blade ratio critical material gravity turbine (8U) with a bearing load approaching 0 and an ultra-high speed circumferential speed.   A magnet with a wear-resistant super-water-repellent plating (3a), a set of two horizontal shafts (16A) fixed on both sides of a cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a series full blade impeller turbine. Various energy storage cycle coalescence engine and coalescence method for generating 100 to 100 sets of horizontal-type full-blade ratio critical material gravity turbine (8U) with approaching bearing load 0 approach + super high speed circumferential speed.   A magnet with a wear-resistant super-water-repellent plating (3a), a set of two horizontal shafts (16A) fixed on both sides of a cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a series full blade impeller turbine. Various energy storage cycle coalescence engine and coalescence method for generating 100 to 120 sets of horizontal full-blade ratio critical material gravity turbine (8U) with a bearing load approaching 0 and an ultra-high speed circumferential speed.   A magnet with a wear-resistant super-water-repellent plating (3a), a set of two horizontal shafts (16A) fixed on both sides of a cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a series full blade impeller turbine. Various energy storage cycle coalescence engines and coalescence methods for generating a set of horizontal full-blade ratio critical material gravity turbines (8U) 121-140 sets with a bearing load approaching 0 and an ultra-high speed circumferential speed.   A magnet with a wear-resistant super-water-repellent plating (3a), a set of two horizontal shafts (16A) fixed on both sides of a cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a series full blade impeller turbine. Various energy storage cycle coalescing engine and coalescence method for generating a set of horizontal full-blade ratio critical material gravity turbine (8U) 141-160 sets with a bearing load approaching 0 and an ultra-high speed circumferential speed.   A magnet with a wear-resistant super-water-repellent plating (3a), a set of two horizontal shafts (16A) fixed on both sides of a cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a series full blade impeller turbine. Various energy storage cycle coalescence engine and coalescence method for generating a total gravity blade (8U) 161-180 sets of horizontal full-blade ratio critical material gravity load approaching zero + super high speed circumferential speed.   A magnet with a wear-resistant super-water-repellent plating (3a), a set of two horizontal shafts (16A) fixed on both sides of a cylindrical turbine blade group (8A) by a horizontal shaft plate (16), and a series full blade impeller turbine. Various energy storage cycle coalescing engine and coalescence method for generating a total gravity blade (8U) 181 to 200 sets of horizontal-type full blade ratio critical material gravity load approaching 0 + super high speed circumferential speed.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), which is a wear-resistant super water-repellent plating (3a). Various energy storage cycle coalescence engines and coalescence methods for generating 1 to 20 sets of horizontal full-blade ratio critical material gravity turbine (8U) with a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), which is a wear-resistant super water-repellent plating (3a). Various energy storage cycle coalescence engines and coalescence methods for generating 21 to 40 sets of horizontal all-blade ratio critical material gravity turbine (8U) with a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), which is a wear-resistant super water-repellent plating (3a). Various energy storage cycle coalescence engines and coalescence methods for generating 41 to 60 sets of horizontal all-blade ratio critical material gravity turbine (8U) with a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), which is a wear-resistant super water-repellent plating (3a). Various energy storage cycle coalescence engine and coalescence method for generating a set of horizontal full-blade ratio critical material gravity turbine (8U) 61-80 with a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), which is a wear-resistant super water-repellent plating (3a). Various energy storage cycle coalescence engine and coalescence method for generating a horizontal all-blade ratio critical material gravity turbine (8U) 81 to 100 sets with a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), which is a wear-resistant super water-repellent plating (3a). Various energy storage cycle coalescence engines and coalescence methods for generating 100 to 120 sets of horizontal full-blade ratio critical material gravity turbine (8U) with a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), which is a wear-resistant super water-repellent plating (3a). Various energy storage cycle coalescence engines and coalescence methods for generating a set of horizontal all-blade ratio critical material gravity turbines (8U) 121-140 with a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), which is a wear-resistant super water-repellent plating (3a). Various energy storage cycle coalescence engines and coalescence methods for generating a horizontal all-blade ratio critical material gravity turbine (8U) 141-160 sets with a magnetic bearing load approaching 0 and an ultra-high speed circumferential speed.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), which is a wear-resistant super water-repellent plating (3a). Various energy storage cycle coalescence engine and coalescence method for generating a set of horizontal full blade ratio critical material gravity turbine (8U) 161-180 sets with a magnetically utilized bearing load approaching 0 and an ultra-high speed circumferential speed.   A set of two horizontal shafts (16A) fixed on both sides of the cylindrical turbine blade group (8A) by a horizontal shaft plate (16), which is a wear-resistant super water-repellent plating (3a). Various energy storage cycle coalescence engine and coalescence method for generating a total gravity blade (8U) 181 to 200 sets of horizontal full-blade ratio critical material gravity approaching 0 with an ultra-high speed circumferential speed.   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 electricity multiple times with 1 to multiple stage heat pump (1G), and recovers heat with 1 to multiple stage compression heat recovery unit (2C) for each compression, electricity + liquid air cold + high temperature Various energy storage cycle coalescence engines and coalescence methods for water to superheated steam temperature supply equipment (3D).   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. Horizontal approaching blade ratio critical material gravity turbine (8U) with 0 approach + super high speed circumferential speed (8U) Compressed by suction multiple times with 1 to multi-stage heat pump (1G) of extremely inexpensive power generation electric drive, 1 for each compression ~ Various energy storage cycle coalescence engine and coalescence method to recover heat with multi-stage compression heat recovery device (2C) to make electricity + liquid air cold heat + hot water ~ superheated steam temperature heat supply equipment (3D).   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, 1 to multi-stage heat pump (1G) compresses suction multiple times, and each compression recovers heat with 1 to multi-stage compression heat recovery unit (2C) Liquid energy cold heat + high temperature water to superheated steam temperature supply facility (3D) Various energy storage cycle coalescing engines and coalescence methods.   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 maximum air (28a) temperature, using magnetic bearing load close to 0 and super high speed circumferential speed (8U) 1G) Various energy that is compressed by suction multiple times, and recovers heat with 1 to multiple-stage compression heat recovery device (2C) for each compression to make electricity + liquid air cold heat + hot water to superheated steam temperature supply equipment (3D) Conservation cycle coalescence engine and coalition Method.   The solar heater (21) is provided with buoyancy on the water surface, and includes a rotation support part (4f) that controls rotation of the sunlight at a right angle from east to west, and includes a gear device (4d) and a roller (4e). ) As a cylindrical rotating part (77G), as a device for controlling rotation of the sunlight at a right angle in the vertical direction and as a device for controlling rotation at a right angle in the east-west direction by using buoyancy, the sunlight is linearly irradiated around the center of the heat absorption tube (4H). 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 and electric drive, 1 to multi-stage heat pump (1G) compresses suction multiple times, 1 to multi-stage compression heat recovery unit (2C) recovers heat for each compression, + Liquid air cooling + hot water to overheating Various energy conservation cycle combined institutions and coalescence how to temperature heat supply facilities (3D).   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 by suction multiple times with 1 to multi-stage heat pump (1G) of extremely inexpensive power generation electric drive, heat is recovered with 1 to multi-stage compression heat recovery unit (2C) for each compression, and electricity + liquid air cooling + Various energy storage cycle coalescing engine and coalescence method for high temperature water to superheated steam temperature supply equipment (3D).   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 full-blade ratio critical material gravity turbine (8U) with zero load approach + super-high speed circumferential speed (8U) Extremely inexpensive electricity-driven electric drive, 1 to multi-stage heat pump (1G) compressed multiple times with suction Various energy storage cycle coalescence engines and coalescence methods that recover heat from a 1 to multi-stage compression heat recovery device (2C) to make electricity + liquid air cold heat + hot water to superheated steam temperature heat supply equipment (3D).   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 and electric drive, 1 to multi-stage heat pump (1G) compresses suction multiple times, 1 to multi-stage compression heat recovery unit (2C) recovers heat for each compression, + Liquid air cold heat + High temperature water to superheated steam temperature heat supply equipment (3D) Various energy storage cycle coalescence engine and coalescence method.   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 type whole blade ratio critical material gravity turbine (8U) with maximum irradiation internal air (28a) temperature, magnetic utilization bearing load approaching 0 + super high speed circumferential speed Extremely inexpensive power generation electric drive, 1 to multi-stage heat Compressed several times with a pump (1G) and recovered heat with 1 to multi-stage compression heat recovery device (2C) for each compression to make electricity + liquid air cold heat + hot water to superheated steam temperature heat supply equipment (3D) Various energy storage cycle unit 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). Horizontal all-blade specific gravity with maximum magnetic bearing load approaching 0 + super high speed circumferential speed, with the highest temperature of the irradiated internal air (28a), and the external air (28a) also heating each air passage (28A) high temperature selective suction Large material gravity turbine (8U) Extremely inexpensive power generation Electric drive, 1 to multi-stage heat pump (1G) compresses several times with suction, and heat is recovered with 1 to multi-stage compression heat recovery unit (2C) for each compression , Electricity + liquid air cold + high temperature Various energy saving cycles combined engine and coalescence process for the ~ superheated steam heat supply facilities (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) ) Various energy conservation cycle coalescence engines and coalescence methods that collect superheated steam hot methane injection into methane hydrate on the sea floor.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) And recovering superheated steam hot-injected methane with liquid nitrogen (5L) cooled liquid methane to methane hydrate on the seabed.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 conservation cycle coalescence engines and coalescence methods that collect superheated steam hot-injected methane in methane hydrate under permafrost land.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 recover superheated steam hot-injected methane with liquid nitrogen (5 L) cooled liquid methane to methane hydrate under permafrost land.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 conservation cycle coalescence engines and coalescence methods for methane recovery and pasture grazing projects, etc. by installing a superheated steam heat injection enclosure in methane hydrate under permafrost.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 are collected and collected by superheated steam injection enclosure in the oil sand zone.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 are collected and collected by superheated steam injection enclosures in the oil shale area.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 conservation cycle coalescence engines and coalescence methods that are collected from and collected by an overheated steam injection enclosure in an old oil extraction zone.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 conservation cycle coalescence engines and coalescence methods that receive low-temperature superheated steam in the food manufacturing industry, etc., and make mass production of inexpensive food products.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 receive cheaper superheated steam and use it for agriculture, industrial, industrial and mining industries to make the best use of thermal energy.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) aiming at ultra-high pressure combustion to receive cheaper liquid oxygen (5K) and make the compression volume 21/60000 of air compression. Various energy storage cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and aims at ultra-high pressure combustion (4Q) Various energy storage cycle coalescence engines and coalescence that drive the theoretical expansion engine (3Q) as ultra-high pressure fuel combustion and drive the automobile 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) aiming for ultra-high pressure combustion, various energy storage cycles combined with theoretical expansion engine (3Q) as ultra-high pressure fuel combustion and driving automobile 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) ) Theoretical combustion chamber (4Q) driven by ultra-high pressure combustion aiming at ultra-high pressure combustion which receives cheaper liquid oxygen (5K) and the compression volume is 21/60000 of air compression. ) Various energy storage cycle coalescence engines and coalescence methods that store in the drive battery (1A) and drive the battery drive wheels (4J) rotation theoretical expansion engine automobile (4L).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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, storing in the theoretical expansion engine (3Q) driven generator (1) driven storage battery (1A) as the theoretical combustion chamber (4Q) ultra high pressure fuel combustion aiming at ultra high pressure combustion Storage battery driving wheel (4J) rotation theory expansion engine automobile (4L) 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) ) Theoretical combustion chamber (4Q) receiving ultra-high pressure combustion by receiving cheaper liquid oxygen (5K) + electricity + high temperature water (4Q) Theoretical expansion engine (3Q) Drive generator (1) Drive battery (1A) Various energy storage cycle coalescing engine and coalescence method for storing in a battery and driving a storage battery drive wheel (4J) rotation theoretical expansion engine automobile (4L).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) driven by ultra-high pressure combustion aiming at ultra-high pressure combustion which receives cheaper liquid oxygen (5K) and the compression volume is 21/60000 of air compression. ) Various energy storage cycle coalescence engines and coalescence methods that store in the drive storage battery (1A) and drive the storage battery drive wheel (4J) and the theoretical expansion engine automobile (4L) capable of rotating the normal wheel.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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, storing in the theoretical expansion engine (3Q) driven generator (1) driven storage battery (1A) as the theoretical combustion chamber (4Q) ultra high pressure fuel combustion aiming at ultra high pressure combustion Various energy storage cycle coalescing engines and coalescence methods for driving a theoretical expansion engine automobile (4L) capable of rotating a battery drive wheel (4J) and rotating a normal wheel.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) receiving ultra-high pressure combustion by receiving cheaper liquid oxygen (5K) + electricity + high temperature water (4Q) Theoretical expansion engine (3Q) Drive generator (1) Drive battery (1A) Various energy storage cycle coalescing engines and coalescence methods for driving a theoretical expansion engine vehicle (4L) capable of rotating in a battery and driving a storage battery drive wheel (4J) and normal wheels.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) and setting the compression volume to 21/60000 of air compression Theoretical combustion chamber (4Q) aimed at ultrahigh pressure combustion Theoretical expansion by driving the theoretical expansion engine (3Q) as ultrahigh pressure fuel combustion Various energy storage cycle coalescence engine and coalescence method for driving a locomotive (4L).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) and setting the compression volume to 21/60000 of air compression Theoretical combustion chamber (4Q) aiming at ultrahigh pressure combustion The theoretical expansion engine (3Q) is driven as a superhigh pressure fuel combustion and screw ( 7C) Various energy storage cycle coalescence engines and coalescence methods for driving a rotating ship.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and aims at ultra-high pressure combustion (4Q) Drives the theoretical expansion engine (3Q) as ultra-high pressure fuel combustion and drives various screws to drive the screw (7C) rotating ship 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) aiming for ultra high pressure combustion, driving theoretical expansion engine (3Q) as ultra high pressure fuel combustion, driving screw (7C) rotating ship 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) and setting the compression volume to 21/60000 of air compression Theoretical combustion chamber (4Q) aiming at ultrahigh pressure combustion 1 to drive multiple theoretical expansion engines (3Q) as ultrahigh pressure fuel combustion Various energy storage cycle coalescing engine and coalescence method for driving a screw (7C) multiple rotation ship.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and aims at ultra-high pressure combustion (4Q) Theoretical expansion engine (3Q) 1 to multiple drives and screw (7C) multiple rotation ship drive as ultrahigh pressure fuel combustion Various energy storage cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) aiming at ultra high pressure combustion 1 to drive multiple theoretical expansion engines (3Q) as super high pressure fuel combustion, multiple screws (7C) Various energy storage cycle coalescence engines and coalescence methods for driving a rotating ship.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) and setting the compression volume to 21/60000 of air compression Theoretical combustion chamber (4Q) aiming at ultrahigh pressure combustion 1 to drive multiple theoretical expansion engines (3Q) as ultrahigh pressure fuel combustion Various energy storage cycle coalescence engine and coalescence method for driving a screw (7C) multi-rotation oxygen coalescence screw ship (39Q).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) + electricity and aims at ultrahigh pressure combustion (4Q) Theoretical expansion engine (3Q) 1 to multiple drive and screw (7C) multiple rotation oxygen coalescence as ultrahigh pressure fuel combustion Various energy storage cycle coalescence engine and coalescence method for driving a screw vessel (39Q).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) aiming at ultra high pressure combustion 1 to drive multiple theoretical expansion engines (3Q) as super high pressure fuel combustion, multiple screws (7C) Various energy storage cycle coalescence engine and coalescence method for driving rotary oxygen coalescence screw ship (39Q).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) and making the compression volume 21/60000 of air compression. Theoretical combustion chamber aiming at ultra high pressure combustion (4Q) The theoretical expansion engine (3Q) is driven as super high pressure fuel combustion and oxygen coalescence Various energy storage cycle coalescence engine and coalescence method for driving a screw vessel (39Q).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) and setting the compression volume to 21/60000 of air compression Theoretical combustion chamber (4Q) aiming at ultrahigh pressure combustion The theoretical expansion engine (3Q) is driven as a superhigh pressure fuel combustion and screw ( 7C) Rotating oxygen coalescence water injection section (88L) Various energy storage cycle coalescence engines and coalescence methods for driving an injection propulsion ship.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and aims at ultra-high pressure combustion (4Q) Drives the theoretical expansion engine (3Q) as ultra-high pressure fuel combustion and screw (7C) rotary oxygen combined water injection part ( 88L) Various energy storage cycle coalescence engines and coalescence methods for driving a propulsion propulsion ship.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) aiming for ultra high pressure combustion, driving theoretical expansion engine (3Q) as ultra high pressure fuel combustion, screw (7C) rotating oxygen combined water Various energy storage cycle coalescence engine and coalescence method for driving an injection unit (88L) jet propulsion ship.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) and setting the compression volume to 21/60000 of air compression Theoretical combustion chamber (4Q) aiming at ultrahigh pressure combustion 1 to drive multiple theoretical expansion engines (3Q) as ultrahigh pressure fuel combustion Various energy storage cycle coalescence engine and coalescence method for driving a screw (7C) multiple rotation oxygen coalescence water injection part (88L) injection propulsion ship.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and aims at ultrahigh pressure combustion (4Q) Theoretical expansion engine (3Q) 1 to multiple drive and screw (7C) multiple rotation oxygen coalescence as ultrahigh pressure fuel combustion Various energy storage cycle coalescing engine and coalescence method for driving water injection part (88L) jet propulsion ship.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) aiming at ultra high pressure combustion 1 to drive multiple theoretical expansion engines (3Q) as super high pressure fuel combustion, multiple screws (7C) Rotating oxygen coalescence water injection part (88L) injection propulsion ship driving various energy storage cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) and setting the compression volume to 21/60000 of air compression Theoretical combustion chamber (4Q) aiming at ultrahigh pressure combustion 1 to drive multiple theoretical expansion engines (3Q) as ultrahigh pressure fuel combustion Various energy storage cycle coalescence engine and coalescence method for driving a screw (7C) multiple rotation oxygen coalescence water injection section (88L) injection propulsion oxygen coalescence screw injection vessel (39S).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) + electricity and aims at ultrahigh pressure combustion (4Q) Theoretical expansion engine (3Q) 1 to multiple drive and screw (7C) multiple rotation oxygen coalescence as ultrahigh pressure fuel combustion Various energy storage cycle coalescence engine and coalescence method for driving water injection part (88L) injection propulsion oxygen coalescence screw injection vessel (39S).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) aiming at ultra high pressure combustion 1 to drive multiple theoretical expansion engines (3Q) as super high pressure fuel combustion, multiple screws (7C) Various energy storage cycle coalescence engine and coalescence method for driving rotary oxygen coalescence water injection part (88L) injection propulsion oxygen coalescence screw injection vessel (39S).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) and making the compression volume 21/60000 of air compression. Theoretical combustion chamber aiming at ultra high pressure combustion (4Q) The theoretical expansion engine (3Q) is driven as super high pressure fuel combustion and oxygen coalescence Various energy storage cycle coalescence engine and coalescence method for driving water injection part (88L) injection propulsion oxygen coalescence screw injection vessel (39S).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 aiming at streamlined ultra-high pressure combustion that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression (4Q) Oxygen combined water injection part (4Q) 88L) Various energy storage cycle coalescence engines and coalescence methods for driving a propulsion propulsion ship.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and aims at streamlined ultra-high pressure combustion (4Q) Oxygen combined water injection part (88L) injection propulsion and various energy to drive the ship Storage cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity + hot water and aims at streamlined ultrahigh pressure combustion (4Q) oxygen combined water injection part (88L) injection propulsion ship 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) ) Received less expensive liquid oxygen (5K) and made the theoretical combustion chamber (4Q) air suction flow path aiming at streamlined ultra-high pressure combustion to make the compression volume 21/60000 of air compression. Various energy storage cycle coalescence engine and coalescence method for driving oxygen coalescence water injection part (88L) injection propulsion ship.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Oxygen combined water injection unit (88L) injection that receives low-priced liquid oxygen (5K) + electricity and has a superficial combustion chamber (4Q) air suction channel that aims at streamlined ultra-high pressure combustion and has multiple ultra-high pressure fuel combustion injection propulsion Various energy storage cycle coalescence engines and coalescence methods for driving propulsion vessels.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) receiving low-cost liquid oxygen (5K) + electricity + high-temperature water and aiming at streamlined ultra-high pressure combustion (4Q) Oxygen combined water injection section with multiple ultra-high pressure fuel combustion injection propulsion including an air suction channel ( 88L) Various energy storage cycle coalescence engines and coalescence methods for driving a propulsion propulsion ship.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Received less expensive liquid oxygen (5K) and made the theoretical combustion chamber (4Q) air suction flow path aiming at streamlined ultra-high pressure combustion to make the compression volume 21/60000 of air compression. Various energy storage cycle coalescence engines and coalescence methods for driving an oxygen coalescence water injection section (88L) injection propulsion oxygen coalescence injection ship (39R).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Oxygen combined water injection unit (88L) injection that receives low-priced liquid oxygen (5K) + electricity and has a superficial combustion chamber (4Q) air suction channel that aims at streamlined ultra-high pressure combustion and has multiple ultra-high pressure fuel combustion injection propulsion Various energy storage cycle coalescence engine and coalescence method for driving propulsion oxygen coalescence injection ship (39R).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) receiving low-cost liquid oxygen (5K) + electricity + high-temperature water and aiming at streamlined ultra-high pressure combustion (4Q) Oxygen combined water injection section with multiple ultra-high pressure fuel combustion injection propulsion including an air suction channel ( 88L) Various types of energy storage cycle coalescence engine and coalescence method for driving an injection propulsion oxygen coalescence injection ship (39R).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) and making the compression volume 21/60000 of air compression. Streamlined ultra high pressure combustion aiming at the theoretical combustion chamber (4Q) Multiple oxygen coalescence water injection part (88L) injection propulsion oxygen coalescence Various energy storage cycle coalescence engine and coalescence method for driving a jet ship (39R).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 aims at streamlined ultrahigh pressure combustion that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression. 88B) Various energy storage cycle coalescing engines and coalescence methods for making jet propulsion airplanes.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and aims at streamlined ultra-high pressure combustion (4Q) Various energy to make an oxygen combined air injection part (88B) injection propulsion airplane with multiple ultra-high pressure fuel combustion injection propulsion Storage cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity + hot water and aims at streamlined ultra-high pressure combustion (4Q) oxygen combined air injection part (88B) injection propulsion airplane 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) ) Received less expensive liquid oxygen (5K) and made the theoretical combustion chamber (4Q) air suction flow path aiming at streamlined ultra-high pressure combustion to make the compression volume 21/60000 of air compression. Various energy storage cycle coalescence engines and coalescence methods for making an oxygen coalescence air injection unit (88B) injection propulsion airplane.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Oxygen combined air injection unit (88B) injection that receives cheaper liquid oxygen (5K) + electricity and has a theoretical combustion chamber (4Q) air suction channel aiming at streamlined ultra high pressure combustion and multiple ultra high pressure fuel combustion injection propulsion Various energy conservation cycle coalescence engines and coalescence methods for propulsion airplanes.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) which receives cheaper liquid oxygen (5K) + electricity + high temperature water and aims at streamlined ultrahigh pressure combustion (4Q) oxygen combined air injection section (multiple ultrahigh pressure fuel combustion injection propulsion equipped with air suction channel) 88B) Various energy storage cycle coalescing engines and coalescence methods for making jet propulsion airplanes.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Received less expensive liquid oxygen (5K) and made the theoretical combustion chamber (4Q) air suction flow path aiming at streamlined ultra-high pressure combustion to make the compression volume 21/60000 of air compression. Various energy storage cycle coalescence engines and coalescence methods for driving an oxygen coalescence air injection section (88B) injection propulsion oxygen coalescence injection airplane (39T).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Oxygen combined air injection unit (88B) injection that receives cheaper liquid oxygen (5K) + electricity and has a theoretical combustion chamber (4Q) air suction channel aiming at streamlined ultra high pressure combustion and multiple ultra high pressure fuel combustion injection propulsion Various energy storage cycle coalescence engine and coalescence method for driving a propulsion oxygen coalescence jet airplane (39T).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) + electricity + high temperature water and aims at streamlined ultrahigh pressure combustion (4Q) oxygen combined air injection section (multiple ultrahigh pressure fuel combustion injection propulsion equipped with air suction channel) 88B) Various energy storage cycle coalescence engines and coalescence methods for driving an injection propulsion oxygen coalescence airplane (39T).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) and setting the compression volume to 21/60000 of air compression Streamlined ultra-high pressure combustion aiming the theoretical combustion chamber (4Q) multiple oxygen coalescence air injection part (88B) injection propulsion oxygen coalescence Various energy storage cycle coalescence engines and coalescence methods for driving an injection plane (39T).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) aiming at ultra-high pressure combustion that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression. The propeller ( 7A) Various energy storage cycle coalescence engines and coalescence methods for driving a rotating airplane.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and aims at ultra-high pressure combustion (4Q) Drives the theoretical expansion engine (3Q) as ultra-high pressure fuel combustion and drives the propeller (7A) rotating airplane to save various energy Cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) aiming at ultra high pressure combustion, theoretical expansion engine (3Q) driving as super high pressure fuel combustion, propeller (7A) rotating airplane driving Various energy storage cycle coalescence engines and coalescence methods.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) and setting the compression volume to 21/60000 of air compression Theoretical combustion chamber (4Q) aiming at ultrahigh pressure combustion 1 to drive multiple theoretical expansion engines (3Q) as ultrahigh pressure fuel combustion Propeller (7A) Various energy storage cycle coalescence engine and coalescence method for driving a multi-turn airplane.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and aims at ultra-high pressure combustion (4Q) Theoretical expansion engine (3Q) 1 to multiple drive as propeller (7A) multiple-rotation airplane drive Various energy storage cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity + hot water and aims at ultrahigh pressure combustion (4Q) One or more theoretical expansion engines (3Q) drive multiple propellers (7A) as ultrahigh pressure fuel combustion Various energy storage cycle coalescence engine and coalescence method for driving a rotating airplane.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) and setting the compression volume to 21/60000 of air compression Theoretical combustion chamber (4Q) aiming at ultrahigh pressure combustion 1 to drive multiple theoretical expansion engines (3Q) as ultrahigh pressure fuel combustion Various energy storage cycle coalescence engines and coalescence methods for driving a propeller (7A) multi-rotation oxygen coalescence propeller airplane (39U).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) + electricity and aims at ultra-high pressure combustion (4Q) Theoretical expansion engine (3Q) 1 to multiple drive and propeller (7A) multi-rotation oxygen coalescence Various energy storage cycle coalescence engine and coalescence method driven by propeller airplane (39U).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) + electricity + hot water and aims at ultrahigh pressure combustion (4Q) One or more theoretical expansion engines (3Q) drive multiple propellers (7A) as ultrahigh pressure fuel combustion Various energy storage cycle coalescence engines and coalescence methods driven by a rotary oxygen coalescence propeller airplane (39U).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) aiming at ultra-high pressure combustion that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression. The propeller ( 7A) Various energy storage cycle coalescence engines and coalescence methods driven by a rotating oxygen coalescence propeller airplane (39U).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) aiming at ultra high pressure combustion which receives cheaper liquid oxygen (5K) and the compression volume is 21/60000 of air compression. Theoretical expansion engine (3Q) driven rotor blade (7B) ) Various energy conservation cycle coalescence engines and coalescence methods that rotate and drive the aircraft.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and aims at ultra-high pressure combustion (4Q) Theoretical expansion engine (3Q) driven rotor blades (7B) as the ultra-high pressure fuel combustion 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) aimed at ultrahigh pressure combustion (4Q) Theoretical engine (3Q) driven rotor blades (7B) rotating as ultra high pressure fuel combustion Various energy storage cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) aiming at ultra-high pressure combustion that receives cheaper liquid oxygen (5K) and the compression volume is 21/60000 of air compression. Wings (7B) Various energy storage cycle coalescing engines and coalescence methods for driving a plurality of wings to drive an airplane.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and aims at ultra-high pressure combustion (4Q) Theoretical expansion engine (3Q) 1-Multi-drive rotor (7B) Various energy storage cycle coalescence engines and coalescence methods to be 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) receiving ultra-high pressure combustion by receiving cheaper liquid oxygen (5K) + electricity + high temperature water (4Q) Theoretical expansion engine (3Q) 1 to multiple drive rotor blades (7B) multiple rotations Various energy storage cycle coalescence engine and coalescence method for driving by 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) aiming at ultra-high pressure combustion that receives cheaper liquid oxygen (5K) and the compression volume is 21/60000 of air compression. Various energy storage cycle coalescence engines and coalescence methods for driving the wing (7B) and rotating the oxygen coalescence rotorcraft (39P).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) + electricity and aims at ultrahigh pressure combustion (4Q) Theoretical expansion engine (3Q) 1 to multiple drive rotor blades (7B) multiple rotations as oxygen combustion Various energy storage cycle coalescence engine and coalescence method for driving a coalesced rotorcraft (39P).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) receiving ultra-high pressure combustion by receiving cheaper liquid oxygen (5K) + electricity + high temperature water (4Q) Theoretical expansion engine (3Q) 1 to multiple drive rotor blades (7B) multiple rotations Then, various energy storage cycle coalescence engines and coalescence methods for driving an oxygen coalescence rotorcraft (39P).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) aiming at ultra high pressure combustion which receives cheaper liquid oxygen (5K) and the compression volume is 21/60000 of air compression. Theoretical expansion engine (3Q) driven rotor blade (7B) ) Various energy storage cycle coalescence engines and coalescence methods that rotate and drive oxygen coalesced rotorcraft (39P).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) driven by ultra-high pressure combustion aiming at ultra-high pressure combustion that receives cheaper liquid oxygen (5K) and the compression volume is 21/60000 of air compression. (7A) Driven propeller (7A) Various energy storage cycle coalescence engines and coalescence methods that rotate and drive an oxygen coalescence air injection unit (88B) 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) + electricity and aims at ultra-high pressure combustion (4Q) Theoretical expansion engine (3Q) drive propeller (7A) rotates as an ultra-high pressure fuel combustion and oxygen combined air injection unit (88B) ) Various energy storage cycle coalescence engines and coalescence methods for driving jet propulsion airplanes.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity + hot water and aims at ultra-high pressure combustion (4Q) Theoretical engine (3Q) drive propeller (7A) rotates as super high-pressure fuel combustion and oxygen combined air injection (88B) Various energy storage cycle coalescence engine and coalescence method for driving an injection propulsion airplane.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) aiming at ultra-high pressure combustion that receives cheaper liquid oxygen (5K) and the compression volume is 21/60000 of air compression. Theoretical expansion engine (3Q) 1 to multiple drive propellers (7A) Various energy storage cycle coalescence engines and coalescence methods that rotate a plurality of times to drive an oxygen coalescence air injection unit (88B) 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) + electricity and aims at ultra-high pressure combustion (4Q) Theoretical expansion engine (3Q) 1-Multi-drive propeller (7A) multiple rotations and oxygen combined air Various energy storage cycle coalescence engine and coalescence method for driving an injection unit (88B) jet propulsion airplane.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + high temperature water, theoretical combustion chamber (4Q) aiming for ultra high pressure combustion (4Q) theoretical expansion engine (3Q) 1-multiple drive propeller (7A) multiple rotations Oxygen coalescence air injection unit (88B) Various energy storage cycle coalescence engines and coalescence methods for driving jet propulsion airplanes.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) aiming at ultra-high pressure combustion that receives cheaper liquid oxygen (5K) and the compression volume is 21/60000 of air compression. Theoretical expansion engine (3Q) 1 to multiple drive propellers (7A) Various energy storage cycle coalescence engines and coalescence methods that rotate a plurality of times and drive an oxygen coalescence air injection unit (88B) injection propulsion oxygen coalescence propeller injection airplane (39N).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) + electricity and aims at ultra-high pressure combustion (4Q) Theoretical expansion engine (3Q) 1-Multi-drive propeller (7A) multiple rotations and oxygen combined air Various energy storage cycle coalescence engines and coalescence methods for driving an injection unit (88B) injection propulsion oxygen coalescence propeller jet airplane (39N).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) aiming for ultra high pressure combustion (4Q) theoretical expansion engine (3Q) 1-multiple drive propeller (7A) multiple rotations Various energy storage cycle coalescence engines and coalescence methods for driving an oxygen coalescence air injection section (88B) injection propulsion oxygen coalescence propeller injection airplane (39N).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) driven by ultra-high pressure combustion aiming at ultra-high pressure combustion that receives cheaper liquid oxygen (5K) and the compression volume is 21/60000 of air compression. (7A) Driven propeller (7A) Various energy storage cycle coalescence engines and coalescence methods that rotate and drive the oxygen coalescence air injection section (88B) injection propulsion oxygen coalescence propeller injection airplane (39N).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) and setting the compression volume to 21/60000 of air compression Theoretical combustion chamber aiming at high pressure combustion (4Q) High pressure high temperature combustion gas control valve (5a) Open combustion as ultra high pressure fuel combustion Various energy storage cycle coalescing engines and coalescence methods for injecting high-pressure and high-temperature combustion gas (5M) from a gas injection nozzle (6Y) and driving a theoretical expansion engine (3Q).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) + electricity and aims at ultra high pressure combustion (4Q) High pressure high temperature combustion gas control valve (5a) High pressure high temperature than open combustion gas injection nozzle (6Y) Various energy storage cycle coalescence engines and coalescence methods for injecting combustion gas (5M) to drive a theoretical expansion engine (3Q).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) + electricity + high temperature water and aims at ultra high pressure combustion (4Q) High pressure high temperature combustion gas control valve (5a) Open combustion gas injection nozzle (6Y) as ultra high pressure fuel combustion Various energy storage cycle coalescence engines and coalescence methods for injecting higher pressure and high temperature combustion gas (5M) to drive a theoretical expansion engine (3Q).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) and setting the compression volume to 21/60000 of air compression Theoretical combustion chamber aiming at high pressure combustion (4Q) High pressure high temperature combustion gas control valve (5a) Open combustion as ultra high pressure fuel combustion Various high-pressure combustion gas (5M) is injected from the gas injection nozzle (6Y) to drive the theoretical expansion engine (3Q) in which the upper expansion blade (8d) and the lower expansion blade (8e) are reversed in the horizontal axis (1h). 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) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and aims at ultra high pressure combustion (4Q) High pressure high temperature combustion gas control valve (5a) High pressure high temperature than open combustion gas injection nozzle (6Y) Various energy storage cycle coalescence engine and coalescence method for driving a theoretical expansion engine (3Q) in which combustion gas (5M) is injected and the upper expansion blade (8d) and the lower expansion blade (8e) are transversely reversed (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) + electricity + high temperature water and aims at ultra high pressure combustion (4Q) High pressure high temperature combustion gas control valve (5a) Open combustion gas injection nozzle (6Y) as ultra high pressure fuel combustion Various energy storage cycle combined engines that drive a theoretical expansion engine (3Q) that injects higher-pressure high-temperature combustion gas (5M) to rotate the upper expansion blade (8d) and lower expansion blade (8e) in the horizontal axis (1h), 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) ) Receiving cheaper liquid oxygen (5K) and setting the compression volume to 21/60000 of air compression Theoretical combustion chamber aiming at high pressure combustion (4Q) High pressure high temperature combustion gas control valve (5a) Open combustion as ultra high pressure fuel combustion High-pressure high-temperature combustion gas (5M) is injected from the gas injection nozzle (6Y), and the upper expansion blade (8d) and the lower expansion blade (8e) are turned on the horizontal axis (1h). Various energy storage cycle coalescence engines and coalescence methods driven by an engine (3Q).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) + electricity and aims at ultra high pressure combustion (4Q) High pressure high temperature combustion gas control valve (5a) High pressure high temperature than open combustion gas injection nozzle (6Y) Various types of energy storage by injecting combustion gas (5M) and driving the upper expansion blade (8d) and the lower expansion blade (8e) on the horizontal axis (1h) and the counter-rotating assembly turbine blade (8f) assembling the theoretical expansion engine (3Q) Cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity + high temperature water and aims at ultra high pressure combustion (4Q) High pressure high temperature combustion gas control valve (5a) Open combustion gas injection nozzle (6Y) as ultra high pressure fuel combustion Higher-pressure high-temperature combustion gas (5M) is injected to drive the upper expansion blade (8d) and lower expansion blade (8e) to the theoretical expansion engine (3Q) of the horizontal axis (1h) and the counter rotating assembly turbine blade (8f). 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) for high pressure combustion aiming at ultra high pressure combustion which receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression High pressure high temperature combustion gas control valve (5a) Open air The suction combustion amount is increased, the high-pressure high-temperature combustion gas (5M) is injected from the combustion gas injection nozzle (6Y), and the upper expansion blade (8d) and the lower expansion blade (8e) are set on the horizontal axis (1h). (8f) Assembling theoretical expansion engine (3Q) Various energy storage cycle merging engines and merging methods for driving.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) aiming at ultra-high pressure combustion that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression High pressure high temperature combustion gas control valve (5a) open circle Various energy storage cycle coalescing engines and coalescence methods for a theoretical expansion engine (3Q) that expands and expands in the circumferential direction by 380 degrees.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) + electricity and aims at ultra-high pressure combustion (4Q) High-pressure high-temperature combustion gas control valve as ultra-high-pressure fuel combustion (5a) Theoretical expansion that expands 380 degrees in the circumferential direction Various energy storage cycle coalescing engines and coalescence methods for the engine (3Q).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) + electricity + hot water and aims at ultra-high pressure combustion (4Q) high-pressure and high-temperature combustion gas control valve (5a) as an ultra-high-pressure fuel combustion 380 degrees expansion in the circumferential direction Various energy storage cycle coalescence engine and coalescence method to make a theoretical expansion engine (3Q).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) aiming at ultra-high pressure combustion that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression High pressure high temperature combustion gas control valve (5a) open circle Various energy storage cycle coalescence engines and coalescence methods for a theoretical expansion engine (3Q) that achieves a maximum drive speed by expansion at 380 degrees in the circumferential direction.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) + electricity and aims at ultra high pressure combustion (4Q) High pressure high temperature combustion gas control valve as ultra high pressure fuel combustion (5a) Maximum drive with expanded expansion of 380 degrees in the circumferential direction Various energy storage cycle coalescing engine and coalescence method for the theoretical expansion engine (3Q) to speed.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity + hot water and aims at ultra-high pressure combustion (4Q) high-pressure and high-temperature combustion gas control valve (5a) as an ultra-high-pressure fuel combustion 380 degrees expansion in the circumferential direction Various energy storage cycle coalescing engine and coalescence method for a theoretical expansion engine (3Q) with a maximum driving 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) ) Theoretical combustion chamber (4Q) aiming at ultra-high pressure combustion that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression High pressure high temperature combustion gas control valve (5a) open circle Various energy storage cycle coalescing engines and coalescence methods for a theoretical expansion engine (3Q) that achieves a maximum drive speed by expansion at 380 degrees in the circumferential direction and double inversion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and aims at ultra-high pressure combustion (4Q) High-pressure and high-temperature combustion gas control valve as ultra-high-pressure fuel combustion (5a) 380 degrees expansion and double expansion in the circumferential direction Various energy storage cycle coalescing engine and coalescence method for a theoretical expansion engine (3Q) that achieves maximum driving speed by reversal.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) + electricity + hot water and aims at ultra-high pressure combustion (4Q) high-pressure and high-temperature combustion gas control valve (5a) as an ultra-high-pressure fuel combustion 380 degrees expansion in the circumferential direction And various energy storage cycle coalescing engines and coalescence methods for a theoretical expansion engine (3Q) that achieves maximum driving speed by counter rotation.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) aiming at ultra-high pressure combustion that receives cheaper liquid oxygen (5K) and makes the compression volume 21/60000 of air compression High pressure high temperature combustion gas control valve (5a) open circle Various energy storage cycle coalescing engines and coalescence methods for a theoretical expansion engine (3Q) that is double-reversed with 380 degree expansion in the circumferential direction.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Ultra high pressure combustion which 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 a compression volume of 21/60000 volume of air compression, etc. Various energy storage cycle coalescing engine and coalescence method for 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) ) Receives cheaper liquid oxygen (5K) + electricity, compresses liquid together with liquid fuel (1c) and water (52a), and compresses the compressed volume with an ultra-high pressure compressed fuel injection combustion such as 21/60000 volume of air compression Various energy storage cycle coalescence engine and coalescence method for a theoretical combustion chamber (4Q) aimed at high pressure combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K) + electricity + hot water, liquid compression with liquid fuel (1c) and water (52a), ultra-high pressure compressed fuel injection with air compression of 21/60000 volume, etc. Various energy storage cycle coalescing engine and coalescence method for a theoretical combustion chamber (4Q) aiming at ultra high pressure 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) ) Combined with various energy conservation cycles that receive cheaper liquid oxygen (5K) and compress it with liquid fuel (1c) or water (52a) to heat it to the optimum temperature on the inner wall of the theoretical combustion chamber (4Q) aiming at ultra high pressure combustion 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) + electricity, compressing liquid together with liquid fuel (1c) and water (52a) and heating to optimum temperature on the inner wall of the theoretical combustion chamber (4Q) aiming for ultra high pressure combustion Cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) + electricity + high temperature water, compress it with liquid fuel (1c) and water (52a), and heat it to the optimum temperature on the inner wall of the theoretical combustion chamber (4Q) aimed at ultra high pressure combustion 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), compressing liquid with liquid fuel (1c) and water (52a) and aiming for ultrahigh pressure combustion Heating oxygen control valve (24D) to the optimum temperature at the inner wall of the theoretical combustion chamber (4Q) + Fuel control valve (25b) + Various energy storage cycle coalescence engine and coalescence method for opening superheated steam control valve (25).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Heated oxygen control valve (5Q) + oxygen is heated to the optimum temperature on the inner wall of the theoretical combustion chamber (4Q) that receives liquid oxygen (5K) + electricity and compresses liquid together with liquid fuel (1c) and water (52a) and aims at ultra high pressure combustion ( 24D) + fuel control valve (25b) + superheated steam control valve (25) to open various energy storage cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) + electricity + hot water, 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) aiming for ultra high pressure combustion Various energy storage cycle coalescence engines and coalescence methods for opening the control valve (24D) + fuel control valve (25b) + superheated steam control valve (25).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Oxygen control valve heated to the optimum temperature on the inner wall of the theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + hot water and compresses liquid together with liquid fuel (1c) and water (52a) and aims at ultra high pressure combustion (24D) + Fuel control valve (25b) + Superheated steam control valve (25) and various energy storage cycle coalescing engines and coalescence methods for injecting together with the 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) and burn the heated oxygen control valve (24D) + fuel control valve (25b) + superheated steam control valve (25) to the optimum temperature by more than 3000 ° C near the open oxygen fuel burner center Various energy storage cycle coalescence engine and coalescence method to make the theoretical combustion chamber (4Q) aiming at ultra-high pressure combustion that heats the superheated steam (50) at the periphery.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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, and open the heated oxygen control valve (24D) + fuel control valve (25b) + superheated steam control valve (25) to the optimum temperature. Various energy storage cycle coalescing engines and coalescence methods that make the theoretical combustion chamber (4Q) aiming at ultra-high pressure combustion that heats the outer superheated steam (50) by combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receive cheaper liquid oxygen (5K) + electricity + hot water, and open the oxygen control valve (24D) + fuel control valve (25b) + superheated steam control valve (25) to the optimum temperature near the center of the open oxygen fuel burner Various energy storage cycle coalescence engine and coalescence method for a theoretical combustion chamber (4Q) aiming at ultra high pressure combustion that heats the outer superheated steam (50) by combustion at 3000 ° C or more.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 burn the heated oxygen control valve (24D) + fuel control valve (25b) + superheated steam control valve (25) to the optimum temperature by more than 3000 ° C near the open oxygen fuel burner center Various energy storage cycle coalescing engine and coalescence method in which the superheated steam (50) is heated to a theoretical combustion chamber (4Q) aiming at super high pressure combustion aiming at part of the heat of the surrounding superheated steam (50).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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, and open the heated oxygen control valve (24D) + fuel control valve (25b) + superheated steam control valve (25) to the optimum temperature. Various energy storage cycle coalescence engine and coalescence method for heating the superheated steam (50) at the outer periphery in the combustion to a theoretical combustion chamber (4Q) aiming at ultra-high pressure combustion aiming at a part of the suction pyrolysis electrolysis near the center.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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, and open the oxygen control valve (24D) + fuel control valve (25b) + superheated steam control valve (25) to the optimum temperature near the center of the open oxygen fuel burner Various energy storage cycle coalescence engines and coalescence methods that heat the outer superheated steam (50) by combustion at a temperature of 3000 ° C. or more and make a theoretical combustion chamber (4Q) aiming at super high pressure combustion aiming at part of the vicinity by suction pyrolysis electrolysis.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 burn the heated oxygen control valve (24D) + fuel control valve (25b) + superheated steam control valve (25) to the optimum temperature by more than 3000 ° C near the open oxygen fuel burner center Various energy storage cycle coalescence engines and coalescence methods for heating the superheated steam (50) at the periphery to a theoretical combustion chamber (4Q) aiming at ultra high pressure combustion aiming at suction thermal decomposition electrolysis oxygen hydrogen increase combustion near the center.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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, and open the heated oxygen control valve (24D) + fuel control valve (25b) + superheated steam control valve (25) to the optimum temperature. Various energy storage cycle coalescence engine and coalescence method for heating the outer superheated steam (50) by the combustion to the theoretical combustion chamber (4Q) aiming at ultra high pressure combustion aiming at the suction pyrolysis electrolysis oxygen hydrogen increase combustion near the center.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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, and open the oxygen control valve (24D) + fuel control valve (25b) + superheated steam control valve (25) to the optimum temperature near the center of the open oxygen fuel burner Heating peripheral superheated steam (50) by combustion at 3000 ° C or more Multiple parts of energy storage cycle coalescence engine and coalescence to make theoretical combustion chamber (4Q) aiming at super high pressure combustion aiming at suction pyrolysis electrolysis oxygen hydrogen increase combustion near the center 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, and opening the heated oxygen control valve (24D) + fuel control valve (25b) + superheated steam control valve (25) to the optimum temperature. Various energy conservation cycle coalescence engines that make superheated combustion (4Q) aiming at super high-pressure combustion aiming at the suction pyrolysis electrolysis decomposition oxygen hydrogen increase combustion around the center of the heating of the peripheral superheated steam (50) including the superheated steam received by combustion above ℃ 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) ) Various types of oxygen combined water injection unit (88L) that receives cheaper liquid oxygen (5K) and has a theoretical combustion chamber (4Q) that aims at ultra-high pressure combustion as a streamlined combustion gas (49) injection acceleration 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) ) Receiving cheaper liquid oxygen (5K) + electricity, the theoretical combustion chamber (4Q) aiming at ultra-high pressure combustion is streamlined, and the combustion gas (49) injection accelerating injection oxygen combined water injection part (88L) is provided in series 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) ) Combustion gas (49) oxygen combined water injection unit (acceleration injection injection) with a plurality of series of theoretical combustion chambers (4Q) that receive cheaper liquid oxygen (5K) + electricity + hot water and aim at ultra-high pressure combustion aiming at super high pressure combustion (4) 88L), various energy storage cycle coalescence engines and coalescence methods.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K), the combustion chamber (4) equipped with multiple theoretical combustion chambers (4Q) aiming at ultra-high pressure combustion in a streamlined form (4Q) and oxygen on the inner wall (5d) and combustion flow inner wall (5d) + Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence water injection unit (88L) that uses fuel + superheated steam heated 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) ) Receive the cheaper liquid oxygen (5K) + electricity, and the combustion chamber (4Q) and the combustion flow inner wall (5d) of the combustion chamber (4Q) with a plurality of in-line combustion gas (49) with a streamlined combustion chamber (4Q) aiming at ultra-high pressure combustion Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence water injection section (88L) that uses oxygen + fuel + superheated steam heated 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) ) By receiving cheaper liquid oxygen (5K) + electricity + high-temperature water, the theoretical combustion chamber (4Q) aiming at ultra-high pressure combustion is a streamlined combustion gas (49) equipped with multiple series (4Q) inner wall and combustion flow inner wall ( 5d) Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence water injection unit (88L) that uses oxygen + fuel + superheated steam heated at an optimal temperature.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K), the combustion chamber (4) equipped with multiple theoretical combustion chambers (4Q) aiming at ultra-high pressure combustion in a streamlined form (4Q) and oxygen on the inner wall (5d) and combustion flow inner wall (5d) + Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence water injection section (88L) that converts fuel + superheated steam to an optimal combustion temperature (4Q) combustion, etc. aiming at ultra high pressure 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 the cheaper liquid oxygen (5K) + electricity, and the combustion chamber (4Q) and the combustion flow inner wall (5d) of the combustion chamber (4Q) with a plurality of in-line combustion gas (49) with a streamlined combustion chamber (4Q) aiming at ultra-high pressure combustion Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence water injection section (88L) for theoretical combustion chamber (4Q) combustion, etc., aiming at super high pressure combustion by heating oxygen + fuel + superheated steam 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) ) By receiving cheaper liquid oxygen (5K) + electricity + high-temperature water, the theoretical combustion chamber (4Q) aiming at ultra-high pressure combustion is a streamlined combustion gas (49) equipped with multiple series (4Q) inner wall and combustion flow inner wall ( 5d) Various energy storage cycle coalescence engines and coalescence methods in the oxygen coalescence water injection section (88L) for the theoretical combustion chamber (4Q) combustion, etc., in which the oxygen + fuel + superheated steam of 5d) is heated at an optimum temperature to aim at ultrahigh pressure 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) ) By receiving cheaper liquid oxygen (5K) + high temperature water, the combustion chamber (4Q) and the combustion flow inner wall (5d) Various energy storage cycle coalescence engine and coalescence with oxygen coalescence water injection part (88L) which makes superheated steam including oxygen + fuel + received high temperature water of optimum temperature heated to the ideal combustion chamber (4Q) combustion etc. 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) and heating the oxygen + fuel + superheated steam at the optimum temperature on each inner wall and aiming at ultra high pressure combustion (4Q) near the center oxygen fuel combustion 3000 ° C or more multiple combustion Various energy storage cycle coalescence engines and coalescence methods for an oxygen coalescence water injection unit (88L) aimed at superheated steam suction pyrolysis electrolysis.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) + electricity and heats oxygen + fuel + superheated steam at the optimum temperature on each inner wall and aims at ultra high pressure combustion. Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence water injection part (88L) aimed at superheated steam suction pyrolysis electrolysis by combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical liquid oxygen (5K) + electricity + hot water is received, oxygen + fuel + superheated steam is heated at the optimum temperature on each inner wall, and the theoretical combustion chamber (4Q) near the center oxygen fuel combustion 3000 Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence water injection part (88L) aimed at superheated steam suction pyrolysis electrolysis with multiple combustion at ℃ or more.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) and heating the oxygen + fuel + superheated steam at the optimum temperature on each inner wall and aiming at ultra high pressure combustion (4Q) near the center oxygen fuel combustion 3000 ° C or more multiple combustion Various energy storage cycle coalescence engine and coalescence method in an oxygen coalescence water injection part (88L) aimed at superheated steam suction pyrolysis electrolysis oxygen hydrogen augmentation combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and heats oxygen + fuel + superheated steam at the optimum temperature on each inner wall and aims at ultra high pressure combustion. Various energy storage cycle coalescence engine and coalescence method in an oxygen coalescence water injection part (88L) aimed at combustion with superheated steam suction pyrolysis electrolysis oxygen hydrogen hydrogen 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 liquid oxygen (5K) + electricity + hot water is received, oxygen + fuel + superheated steam is heated at the optimum temperature on each inner wall, and the theoretical combustion chamber (4Q) near the center oxygen fuel combustion 3000 Various energy storage cycle coalescence engine and coalescence method in an oxygen coalescence water injection part (88L) aimed at superheated steam suction pyrolysis electrolysis oxygen hydrogen hydrogen augmentation combustion by multiple combustion at ℃.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) and heating the oxygen + fuel + superheated steam at the optimum temperature on each inner wall and aiming at ultra high pressure combustion (4Q) near the center oxygen fuel combustion 3000 ° C or more multiple combustion Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence water injection part (88L) for heating and injecting superheated steam (50) of a combustion flow inner wall (5d) 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) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and heats oxygen + fuel + superheated steam at the optimum temperature on each inner wall and aims at ultra high pressure combustion. Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence water injection section (88L) that heats and injects superheated steam (50) of a combustion flow inner wall (5d) high-temperature water heating pipe (5H) by 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 liquid oxygen (5K) + electricity + hot water is received, oxygen + fuel + superheated steam is heated at the optimum temperature on each inner wall, and the theoretical combustion chamber (4Q) near the center oxygen fuel combustion 3000 Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence water injection section (88L) that heats and injects superheated steam (50) of a combustion flow inner wall (5d) high-temperature water heating pipe (5H) by multiple combustion at a temperature of 0 ° C or higher.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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, oxygen + fuel + superheated steam is heated at the optimum temperature on each inner wall, aiming for ultra high pressure combustion (4Q) near the center oxygen fuel combustion 3000 ° C or more Various energy storage cycle coalescence engine and coalescence method with oxygen coalescence water injection part (88L) for heating and injecting superheated steam (50) including superheated steam received in combustion flow inner wall (5d) high temperature water heating pipe (5H) in multiple 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) ) Oxygen combined water injection unit (88L) that receives cheaper liquid oxygen (5K), and also injects combustion into the air (28a) at the optimum location of the suction injection flow in the same manner as the theoretical combustion chamber (4Q) aiming at a plurality of streamline type ultra high pressure combustion ) 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) ) Oxygen combined water injection unit that receives cheaper liquid oxygen (5K) + electricity, and also injects air (28a) into the optimum location of the suction injection flow and also has a plurality of streamline type ultra high pressure combustion aiming combustion chambers (4Q) (88L) various energy storage cycle coalescence engines and coalescence methods.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Oxygen coal that receives cheaper liquid oxygen (5K) + electricity + hot water and burns and jets the air (28a) in the optimal location of the suction injection flow as well as a plurality of theoretical combustion chambers (4Q) aiming at super high pressure combustion Various energy storage cycle coalescence engine and coalescence method made into water injection part (88L).   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Various energy storage cycle coalescence engines and coalescence methods that receive cheaper liquid oxygen (5K) and have an oxygen coalescence water injection section (88L) that expands the air inlet forward.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 receive cheaper liquid oxygen (5K) + electricity and have an oxygen coalescence water injection section (88L) that expands the air inlet forward.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 receive cheaper liquid oxygen (5K) + electricity + high-temperature water and have an oxygen coalescence water injection section (88L) that expands the air inlet forward.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 receive cheaper liquid oxygen (5K), use the oxygen coalescence water injection part (88L), expand the air inlet forward, approach the straight line, and inject maximum bubbles into 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) ) Various energy conservation cycle coalescence engines and coalescence that receive cheaper liquid oxygen (5K) + electricity, make the oxygen coalescence water injection part (88L) expand the air inlet forward, approach the straight line, and inject maximum bubbles into the ship bottom 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 + high-temperature water, oxygen combined water injection unit (88L), expanding the air inlet forward, approaching a straight line, and various energy conservation cycle coalescence that injects bubbles to the bottom of the ship at the maximum 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) ) Various energy storage cycle coalescence engines that receive cheaper liquid oxygen (5K) + high temperature water, make the oxygen coalesced water injection section (88L) expand the air inlet forward, approach the straight line, and inject the bubbles to the bottom of the ship at the maximum Merge method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Various liquid oxygen (5K) was received, and various types of combustion gas (49) injection accelerating injection oxygen combined air injection unit (88B) with a plurality of series of theoretical combustion chambers (4Q) aiming at ultra-high pressure combustion and streamlined 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) ) Receiving cheaper liquid oxygen (5K) + electricity, the theoretical combustion chamber (4Q) aiming at ultra-high pressure combustion is streamlined, and the combustion gas (49) injection accelerating injection oxygen combined air injection section (88B) is provided in series 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) ) Combustion gas (49) Oxygen combined air injection unit (acceleration injection injection) with a plurality of series of theoretical combustion chambers (4Q) that receive cheaper liquid oxygen (5K) + electricity + hot water and aim at ultra high pressure combustion and streamline 88B), 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), the combustion chamber (4) equipped with multiple theoretical combustion chambers (4Q) aiming at ultra-high pressure combustion in a streamlined form (4Q) and oxygen on the inner wall (5d) and combustion flow inner wall (5d) + Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence air injection unit (88B) that uses fuel + superheated steam heated 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) ) Receive the cheaper liquid oxygen (5K) + electricity, and the combustion chamber (4Q) and the combustion flow inner wall (5d) of the combustion chamber (4Q) with a plurality of in-line combustion gas (49) with a streamlined combustion chamber (4Q) aiming at ultra-high pressure combustion Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence air injection unit (88B) that uses oxygen + fuel + superheated steam heated at an optimum temperature.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) By receiving cheaper liquid oxygen (5K) + electricity + high-temperature water, the theoretical combustion chamber (4Q) aiming at ultra-high pressure combustion is a streamlined combustion gas (49) equipped with multiple series (4Q) inner wall and combustion flow inner wall ( 5d) Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence air injection unit (88B) that uses oxygen + fuel + superheated steam heated at an optimum temperature.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper liquid oxygen (5K), the combustion chamber (4) equipped with multiple theoretical combustion chambers (4Q) aiming at ultra-high pressure combustion in a streamlined form (4Q) and oxygen on the inner wall (5d) and combustion flow inner wall (5d) + Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence air injection unit (88B) for the theoretical combustion chamber (4Q) combustion, etc., aiming at super high pressure combustion by heating fuel + superheated steam 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) ) Receive the cheaper liquid oxygen (5K) + electricity, and the combustion chamber (4Q) and the combustion flow inner wall (5d) of the combustion chamber (4Q) with a plurality of in-line combustion gas (49) with a streamlined combustion chamber (4Q) aiming at ultra-high pressure combustion Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence air injection section (88B) that converts oxygen + fuel + superheated steam to an optimal temperature by heating to an optimal temperature combustion chamber (4Q) aiming at ultra high pressure 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) ) By receiving cheaper liquid oxygen (5K) + electricity + high-temperature water, the theoretical combustion chamber (4Q) aiming at ultra-high pressure combustion is a streamlined combustion gas (49) equipped with multiple series (4Q) inner wall and combustion flow inner wall ( 5d) Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence air injection section (88B) for theoretical combustion chamber (4Q) combustion, etc., in which oxygen + fuel + superheated steam is heated at an optimum temperature to aim at ultrahigh pressure 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) ) By receiving cheaper liquid oxygen (5K) + high temperature water, the combustion chamber (4Q) and the combustion flow inner wall (5d) Various energy storage cycle coalescence engine and coalescence with oxygen coalescence air injection part (88B) for ideal combustion chamber (4Q) combustion aiming at super high pressure combustion by heating superheated steam including oxygen + fuel + received high temperature water 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) and heating the oxygen + fuel + superheated steam at the optimum temperature on each inner wall and aiming at ultra high pressure combustion (4Q) near the center oxygen fuel combustion 3000 ° C or more multiple combustion Various energy storage cycle coalescence engines and coalescence methods for an oxygen coalescence air injection unit (88B) aimed at superheated steam suction pyrolysis electrolysis.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) + electricity and heats oxygen + fuel + superheated steam at the optimum temperature on each inner wall and aims at ultra high pressure combustion. Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence air injection unit (88B) aimed at superheated steam suction pyrolysis electrolysis by combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical liquid oxygen (5K) + electricity + hot water is received, oxygen + fuel + superheated steam is heated at the optimum temperature on each inner wall, and the theoretical combustion chamber (4Q) near the center oxygen fuel combustion 3000 Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence air injection unit (88B) aimed at superheated steam suction pyrolysis electrolysis with multiple combustion at ℃ or higher.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) and heating the oxygen + fuel + superheated steam at the optimum temperature on each inner wall and aiming at ultra high pressure combustion (4Q) near the center oxygen fuel combustion 3000 ° C or more multiple combustion Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence air injection unit (88B) aimed at superheated steam suction pyrolysis electrolysis oxygen oxygen hydrogen increase combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical combustion chamber (4Q) that receives cheaper liquid oxygen (5K) + electricity and heats oxygen + fuel + superheated steam at the optimum temperature on each inner wall and aims at ultra high pressure combustion. Various energy storage cycle coalescence engine and coalescence method in an oxygen coalescence air injection unit (88B) aimed at combustion with superheated steam suction pyrolysis electrolysis oxygen hydrogen hydrogen 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 liquid oxygen (5K) + electricity + hot water is received, oxygen + fuel + superheated steam is heated at the optimum temperature on each inner wall, and the theoretical combustion chamber (4Q) near the center oxygen fuel combustion 3000 Various energy storage cycle coalescence engine and coalescence method in an oxygen coalescence air injection unit (88B) aimed at superheated steam suction pyrolysis electrolysis oxygen hydrogen hydrogen augmentation combustion with multiple combustion at ℃ or higher.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) and heating the oxygen + fuel + superheated steam at the optimum temperature on each inner wall and aiming at ultra high pressure combustion (4Q) near the center oxygen fuel combustion 3000 ° C or more multiple combustion Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence air injection section (88B) for heating and injecting superheated steam (50) of a combustion flow inner wall (5d) high-temperature water heating pipe (5H).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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) + electricity and heats oxygen + fuel + superheated steam at the optimum temperature on each inner wall and aims at ultra high pressure combustion. Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence air injection section (88B) that heats and injects superheated steam (50) of a combustion flow inner wall (5d) high-temperature water heating pipe (5H) by combustion.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Theoretical liquid oxygen (5K) + electricity + hot water is received, oxygen + fuel + superheated steam is heated at the optimum temperature on each inner wall, and the theoretical combustion chamber (4Q) near the center oxygen fuel combustion 3000 Various energy storage cycle coalescence engines and coalescence methods in an oxygen coalescence air injection section (88B) that heats and injects superheated steam (50) of a combustion flow inner wall (5d) high-temperature water heating pipe (5H) by multiple combustion at a temperature of 0 ° C or higher.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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, oxygen + fuel + superheated steam is heated at the optimum temperature on each inner wall, aiming for ultra high pressure combustion (4Q) near the center oxygen fuel combustion 3000 ° C or more Various energy storage cycle coalescence engines and coalescence methods in the oxygen coalescence air injection section (88B) for heating and injecting superheated steam (50) including the superheated steam received from the combustion flow inner wall (5d) high-temperature water heating pipe (5H) in multiple 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) ) Oxygen combined air injection unit (88B) that receives cheaper liquid oxygen (5K), and also injects the air (28a) into the optimum location of the suction injection flow, and also has a plurality of streamlined ultrahigh pressure combustion aiming combustion chambers (4Q) ) 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) ) Oxygen combined air injection unit that receives cheaper liquid oxygen (5K) + electricity, and also injects air (28a) into the optimum location of the suction injection flow and also has a plurality of streamline type ultra high pressure combustion aiming combustion chambers (4Q). (88B) 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) ) Oxygen coal that receives cheaper liquid oxygen (5K) + electricity + hot water and burns and jets the air (28a) in the optimal location of the suction injection flow as well as a plurality of theoretical combustion chambers (4Q) aiming at super high pressure combustion Various energy storage cycle coalescence engines and coalescence methods in the air injection section (88B).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 receive cheaper liquid oxygen (5K) and rotate the oxygen coalescence air injection section (88B) to enable vertical ascent and descent.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 receive cheaper liquid oxygen (5K) + electricity and rotate the oxygen coalescence air injection section (88B) to allow vertical ascent and descent.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 receive cheaper liquid oxygen (5K) + electricity + high temperature water and rotate the oxygen coalescence air injection section (88B) to enable vertical ascent and descent.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 receive cheaper liquid oxygen (5K) and rotate the oxygen coalescence air injection section (88B) to enable reverse 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) ) Various energy storage cycle coalescence engines and coalescence methods that receive cheaper liquid oxygen (5K) + electricity and rotate the oxygen coalescence air injection section (88B) to enable reverse injection.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 receive cheaper liquid oxygen (5K) + electricity + hot water and rotate the oxygen coalescence air injection section (88B) to enable reverse 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) ) Various energy storage cycle coalescence engines and coalescence methods that receive cheaper liquid oxygen (5K) + hot water and rotate the oxygen coalescence air injection section (88B) to enable reverse injection.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 energies that were made into an electrically driven theoretical gas compressor (3T) that receives cheaper electricity + hot water (52b) and compresses the gas volume from the outer peripheral long compression blade to the central short compression blade with the gas volume inversely proportional to the pressure. 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) ) Various energy conservation cycle coalescing engines and coalescences that receive less expensive electricity and that are electrically driven theoretical gas compressors (3T) that compress the gas volume from the outer peripheral large compression blades to the central short compression blades with the gas volume inversely proportional to the pressure 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) ) Combined with various energy storage cycles, receiving less expensive electricity + superheated steam, and compressing the gas volume from the outer peripheral large compression blade to the central short compression blade with the gas volume inversely proportional to the pressure. 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 electricity + hot water (52b) and sucking air as an electrically driven theoretical gas compressor (3T) that compresses from the large outer peripheral compression wing to the central short compression wing aiming the gas volume inversely proportional to the pressure Various energy storage cycle coalescence engines and coalescence methods for compression.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Various energy storage cycles that take in and compress air as an electrically driven theoretical gas compressor (3T) that receives cheaper electricity and compresses the gas volume from the outer peripheral large compression blades to the central short compression blades in inverse proportion to the pressure Merger engine and merger method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Various types of electric-driven theoretical gas compressors (3T) that receive cheaper electricity + superheated steam and compress the gas volume from the outer peripheral large compression blades to the central short compression blades with the gas volume inversely proportional to the pressure. 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) ) Receiving cheaper electricity + hot water (52b) and sucking air as an electrically driven theoretical gas compressor (3T) that compresses from the large outer peripheral compression wing to the central short compression wing aiming the gas volume inversely proportional to the pressure Various energy storage cycle coalescence engine and coalescence method for producing compressed heat exchange superheated steam.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper electricity, the gas volume is inversely proportional to the pressure. The electric driven theoretical gas compressor (3T) that compresses the outer large compression blade from the outer peripheral long compression blade to the central short compression blade. Various energy storage cycle coalescence engines and coalescence methods to be manufactured.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receiving cheaper electricity + superheated steam, and compressing heat by suction air as an electrically driven theoretical gas compressor (3T) that compresses gas from the outer peripheral large compression blades to the central short compression blades, whose gas volume is inversely proportional to the pressure Various energy storage cycle coalescence engine and coalescence method for producing superheated steam.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) As an electrically driven theoretical gas compressor (3T) that receives cheaper electricity + hot water (52b) + superheated steam and compresses the gas volume from the outer peripheral large compression blades to the central short compression blades, which is inversely proportional to the pressure 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) ) Receiving cheaper electricity + hot water (52b) and sucking air as an electrically driven theoretical gas compressor (3T) that compresses from the large outer peripheral compression wing to the central short compression wing aiming the gas volume inversely proportional to the pressure Various energy storage cycle coalescence engines and coalescence methods for producing superheated steam with a compressed air compressor (2Y).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 electrically driven theoretical gas compressor (3T) that receives cheaper electricity and compresses the gas volume from the outer peripheral large compression blades to the central short compression blades, which is aimed at the inverse proportion of the pressure, the air is sucked in compressed air Various energy storage cycle coalescence engine and coalescence method for producing superheated steam at (2Y).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 electricity + superheated steam, and compressing compressed air by sucking air as an electrically driven theoretical gas compressor (3T) that compresses gas from the outer peripheral large compression blades to the central short compression blades, whose gas volume is inversely proportional to the pressure Various energy storage cycle coalescence engine and coalescence method for producing superheated steam with a heat exchanger (2Y).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 electricity + hot water (52b) and sucking air as an electrically driven theoretical gas compressor (3T) that compresses from the large outer peripheral compression wing to the central short compression wing aiming the gas volume inversely proportional to the pressure Various energy storage cycle coalescence engines and coalescence methods for supplying superheated steam to the production supply facility (3D) with a compressed air compressor (2Y).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 electrically driven theoretical gas compressor (3T) that receives cheaper electricity and compresses the gas volume from the outer peripheral large compression blades to the central short compression blades, which is aimed at the inverse proportion of the pressure, the air is sucked in compressed air (2Y) Various energy storage cycle coalescence engines and coalescence methods for supplying 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) ) Receiving cheaper electricity + superheated steam, and compressing compressed air by sucking air as an electrically driven theoretical gas compressor (3T) that compresses gas from the outer peripheral large compression blades to the central short compression blades, whose gas volume is inversely proportional to the pressure Various energy storage cycle coalescence engines and coalescence methods for supplying superheated steam to the production supply facility (3D) with a heat exchanger (2Y).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 electricity + hot water (52b) and sucking air as an electrically driven theoretical gas compressor (3T) that compresses from the large outer peripheral compression wing to the central short compression wing aiming the gas volume inversely proportional to the pressure Various energy storage cycle coalescence engines and coalescence methods for supplying compressed air + superheated steam to the production supply facility (3D) with a compressed air compressor heat exchanger (2Y).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 electrically driven theoretical gas compressor (3T) that receives cheaper electricity and compresses the gas volume from the outer peripheral large compression blades to the central short compression blades, which is aimed at the inverse proportion of the pressure, the air is sucked in compressed air Various energy storage cycle coalescence engines and coalescence methods for supplying compressed air + superheated steam to the production supply facility (3D) at (2Y).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 electricity + superheated steam, and compressing compressed air by sucking air as an electrically driven theoretical gas compressor (3T) that compresses gas from the outer peripheral large compression blades to the central short compression blades, whose gas volume is inversely proportional to the pressure Various energy storage cycle coalescence engines and coalescence methods for supplying compressed air + superheated steam to the production supply facility (3D) with a heat exchanger (2Y).   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 electrically driven theoretical gas compressor (3T) that receives cheaper electricity + hot water (52b) + superheated steam and compresses the gas volume from the outer peripheral large compression blades to the central short compression blades, which is inversely proportional to the pressure Various energy storage cycle coalescence engines and coalescence methods for supplying compressed air + superheated steam to the production supply facility (3D) with a suction compressed air heat exchanger (2Y).   Horizontally-moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 and ultra-high speed circumferential speed Extremely inexpensive power generation electric drive, theoretical gas compressor (3T) gas volume inversely proportional to pressure Various energy storage cycle coalescing engines and coalescence methods configured to compress from the outer peripheral long compressor blade (8) to the central short compressor blade (8).   Horizontally-moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 and ultra-high speed circumferential speed Extremely inexpensive power generation electric drive, theoretical gas compressor (3T) gas volume inversely proportional to pressure Various energy storage cycle coalescence engines and coalescence methods for compressing air as a configuration in which the outer peripheral long compression blade (8) is compressed to the central short compression blade (8).   Horizontally-moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 and ultra-high speed circumferential speed Extremely inexpensive power generation electric drive, theoretical gas compressor (3T) gas volume inversely proportional to pressure Various energy storage cycle coalescence engines and coalescence methods for compressing air (28a) as a configuration for compressing from the outer peripheral large compression blade (8) to the central short compression blade (8).   Horizontally-moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 and ultra-high speed circumferential speed Extremely inexpensive power generation electric drive, theoretical gas compressor (3T) gas volume inversely proportional to pressure Various energy storage cycle coalescence engines and coalescence methods for compressing air (28a) from the outer periphery to the suction center as a configuration for compressing from the outer peripheral large compression blade (8) to the central short compression blade (8).   Horizontally-moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 and ultra-high speed circumferential speed Extremely inexpensive power generation electric drive, theoretical gas compressor (3T) gas volume inversely proportional to pressure Various energy storage cycle coalescence engines and coalescence methods for heating air (28a) compressed water from the outer circumference to the suction center as a configuration for compressing the outer circumference long large compression blade (8) to the center short compression blade (8).   Horizontally-moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 and ultra-high speed circumferential speed Extremely inexpensive power generation electric drive, theoretical gas compressor (3T) gas volume inversely proportional to pressure Various energy storage cycle coalescence engines and coalescence methods for heating air (28a) compressed high-temperature water from the outer circumference to the suction center as a configuration for compressing the outer circumference long large compression blade (8) to the center short compression blade (8).   Horizontally-moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 and ultra-high speed circumferential speed Extremely inexpensive power generation electric drive, theoretical gas compressor (3T) gas volume inversely proportional to pressure Various energy storage cycle coalescence engines and coalescence methods for heating air (28a) compressed superheated steam from the outer circumference to the suction center as a configuration for compressing from the outer peripheral large compression blade (8) to the central short compression blade (8).   Horizontally-moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 and ultra-high speed circumferential speed Extremely inexpensive power generation electric drive, theoretical gas compressor (3T) gas volume inversely proportional to pressure As an arrangement for compressing from the outer peripheral large compression blade (8) to the central short compression blade (8), various energy storage cycle combined engines for heating water from the outer periphery to the suction center with air (28a) compressed air compressor (2Y) And coalescing method.   Horizontally-moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 and ultra-high speed circumferential speed Extremely inexpensive power generation electric drive, theoretical gas compressor (3T) gas volume inversely proportional to pressure As a structure for compressing from the outer peripheral long large compression blade (8) to the central short compression blade (8), the air (28a) is compressed from the outer periphery to the suction center, and various energy storage cycle coalesces are used to heat high-temperature water in the compressed air heat exchanger (2Y). Organization and coalescence method.   Horizontally-moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 and ultra-high speed circumferential speed Extremely inexpensive power generation electric drive, theoretical gas compressor (3T) gas volume inversely proportional to pressure As a structure for compressing from the outer peripheral large compression blade (8) to the central short compression blade (8), the air (28a) is heated from the outer periphery to the suction center, and the superheated steam is heated by the compressed compression air heat exchanger (2Y). Organization and coalescence method.   Horizontally-moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 and ultra-high speed circumferential speed Extremely inexpensive power generation electric drive, theoretical gas compressor (3T) gas volume inversely proportional to pressure Various energy storage cycle coalescence engines and coalescence methods for producing superheated steam with a compressed air heat exchanger (2Y) as a configuration for compressing from the outer peripheral large compression blade (8) to the central short compression blade (8).   Horizontally-moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 and ultra-high speed circumferential speed Extremely inexpensive power generation electric drive, theoretical gas compressor (3T) gas volume inversely proportional to pressure Various energy storage cycle coalescence engines and coalescence methods for producing compressed air + superheated steam with a compressed air heat exchanger (2Y) as a configuration for compressing from the outer peripheral long large compression blade (8) to the central short compression blade (8).   Horizontally-moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 and ultra-high speed circumferential speed Extremely inexpensive power generation electric drive, theoretical gas compressor (3T) gas volume inversely proportional to pressure Various energy storage cycle coalescence engines and coalescence methods for producing high-pressure compressed air + high-pressure superheated steam with a compressed air heat exchanger (2Y) as a configuration for compressing from the outer peripheral long large compression blade (8) to the central short compression blade (8).   Horizontally-moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 and ultra-high speed circumferential speed Extremely inexpensive power generation electric drive, theoretical gas compressor (3T) gas volume inversely proportional to pressure Various energy storage cycle coalescence engine and coalescence method for producing ultra-high pressure compressed air + ultra-high pressure superheated steam with a compressed air heat exchanger (2Y) as a configuration for compressing from the outer peripheral large compression blade (8) to the central short compression blade (8) .   Horizontally-moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 and ultra-high speed circumferential speed Extremely inexpensive power generation electric drive, theoretical gas compressor (3T) gas volume inversely proportional to pressure Various energy storage cycle coalescence engines that supply compressed air + superheated steam production and supply equipment (3D) with a compressed air heat exchanger (2Y) as a configuration that compresses from a large outer peripheral compressor blade (8) to a central short compressor blade (8) And coalescing method.   Horizontally-moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 and ultra-high speed circumferential speed Extremely inexpensive power generation electric drive, theoretical gas compressor (3T) gas volume inversely proportional to pressure As an arrangement for compressing from the outer peripheral large compression blade (8) to the central short compression blade (8), various energy storage cycles for supplying high pressure compressed air + high pressure superheated steam production and supply equipment (3D) with a compressed air heat exchanger (2Y) Merger engine and merger method.   Horizontally-moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 and ultra-high speed circumferential speed Extremely inexpensive power generation electric drive, theoretical gas compressor (3T) gas volume inversely proportional to pressure Various types of energy supplied to the super high pressure compressed air + super high pressure superheated steam production and supply facility (3D) by the compressed air heat exchanger (2Y) as a configuration for compressing from the outer peripheral large compression blade (8) to the central short compression blade (8) Storage cycle coalescence engine and coalescence method.   Horizontally-moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 and ultra-high speed circumferential speed Extremely inexpensive power generation electric drive, theoretical gas compressor (3T) gas volume inversely proportional to pressure Various energy storage cycles for supplying liquid air + super-high pressure superheated steam production and supply equipment (3D) with a compressed air heat exchanger (2Y) as a configuration for compressing from the outer peripheral large compression blade (8) to the central short compression blade (8) Merger engine and merger method.   Horizontally-moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 and ultra-high speed circumferential speed Extremely inexpensive power generation electric drive, theoretical gas compressor (3T) gas volume inversely proportional to pressure As a structure for compressing from the outer peripheral large compression blade (8) to the central short compression blade (8), various types of supply to the liquid oxygen + liquid nitrogen + super high pressure superheated steam production / supply facility (3D) by the compressed air heat exchanger (2Y) Energy conservation cycle coalescence engine and coalescence method.   Horizontally-moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 and ultra-high speed circumferential speed Extremely inexpensive power generation electric drive, theoretical gas compressor (3T) gas volume inversely proportional to pressure As a configuration for compressing from the outer peripheral large compression blade (8) to the central short compression blade (8), supply to electricity + liquid oxygen + liquid nitrogen + ultra high pressure superheated steam production and supply equipment (3D) with a compressed air heat exchanger (2Y) 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 less expensive liquid oxygen (5K), fuel injection and combustion, and in the process of expansion of 380 degrees in the circumferential direction, fuel pipe (25a) extended upper expansion blade group (8d) fuel injection combustion from multiple locations combined with various energy storage cycle 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) ) Low energy liquid oxygen (5K) + electricity is received and injected and burned, and in the process of expansion 380 degrees in the circumferential direction, fuel pipe (25a) extended upper expansion blade group (8d) fuel injection and combustion from a plurality of locations to save various energy Cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Received fuel injection combustion of cheaper liquid oxygen (5K) + electricity + hot water, and fuel injection combustion from multiple locations of the fuel pipe (25a) extended upper expansion blade group (8d) in the expansion process of 380 degrees in the circumferential direction 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 less expensive liquid oxygen (5K) and injecting and burning, various energies that increase the amount of fuel injection combustion combustion from multiple locations of the fuel pipe (25a) extended upper expansion blade group (8d) in the expansion process in the circumferential direction of 380 degrees 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) ) Fuel injection combustion that receives cheaper liquid oxygen (5K) + electricity, and in the expansion process of 380 degrees in the circumferential direction, the amount of fuel injection combustion combustion increases from a plurality of locations in the fuel pipe (25a) extended upper expansion blade group (8d) Various energy storage cycle coalescence engines and coalescence methods.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Fuel injection combustion with receiving cheaper liquid oxygen (5K) + electricity + hot water, and fuel injection combustion combustion from multiple locations of fuel pipe (25a) extended upper expansion blade group (8d) in the circumferential expansion process of 380 degrees Various energy storage cycle coalescence engines and coalescence methods that increase in volume.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Various energy storage cycle coalescence engines and coalescence methods in which cheaper liquid oxygen (5K) is received and injected and burned and compressed with the turbine outer casing (77a) in the circumferential expansion process of 380 degrees.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 receive cheaper liquid oxygen (5K) + electricity and inject and burn fuel and compress air with the turbine outer casing (77a) in the circumferential expansion process of 380 degrees.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 coalescing engines that receive and inject and burn cheaper liquid oxygen (5K) + electricity + high-temperature water and compress air with the turbine outer box (77a) in the circumferential expansion process of 380 degrees, 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) ) Various energy storage cycle coalescence engine and coalescence method in which cheaper liquid oxygen (5K) + hot water is received and injected and burned and compressed with the turbine outer casing (77a) in the circumferential expansion process of 380 degrees .   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 fuel injection and combustion of cheaper liquid oxygen (5K), and compressed air part (9D) with the turbine outer casing (77a) in the circumferential expansion direction of 380 degrees to compress the air injection nozzle (5 ) Various energy storage cycle coalescence engines and coalescence methods that inject at multiple locations.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 is received and fuel injected and combusted, and compressed air part (9D) is compressed between the outer casing (77a) and the air injection nozzle in the circumferential direction of 380 degrees expansion process (5) Various energy storage cycle coalescence engines and coalescence methods for injecting at a plurality of locations.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 fuel injection combustion of cheaper liquid oxygen (5K) + electricity + hot water, and compressed air (9D) with the turbine outer box (77a) in the circumferential expansion process of 380 degrees Air injection nozzle (5) Various energy storage cycle coalescence engine and coalescence method for injecting at a plurality of locations   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 fuel injection and combustion of cheaper liquid oxygen (5K), and compressed air part (9D) with the turbine outer casing (77a) in the circumferential expansion direction of 380 degrees to compress the air injection nozzle (5 ) Various energy storage cycle coalescing engines and coalescence methods for a theoretical expansion engine (3Q) that increases the fuel combustion quantity at multiple locations.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 is received and fuel injected and combusted, and compressed air part (9D) is compressed between the outer casing (77a) and the air injection nozzle in the circumferential direction of 380 degrees expansion process (5) Various energy storage cycle coalescing engines and coalescence methods that increase the amount of fuel injected at multiple locations.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 fuel injection combustion of cheaper liquid oxygen (5K) + electricity + hot water, and compressed air (9D) with the turbine outer box (77a) in the circumferential expansion process of 380 degrees Air injection nozzle (5) Various energy storage cycle coalescence engine and coalescence method for increasing the fuel combustion quantity at multiple locations.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Receives and injects cheaper liquid oxygen (5K), and injects and burns fuel from a plurality of locations on the upper expansion blade group (8d) on the upper side of the fuel pipe (25a) in the circumferential expansion process of 380 degrees, 77a), a compressed air portion (9D), and an air injection nozzle (5) various energy storage cycle coalescence engines and coalescence methods for increasing the amount of fuel injected at a plurality of locations.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Fuel injection combustion with receiving cheaper liquid oxygen (5K) + electricity, fuel injection combustion from multiple locations of the fuel pipe (25a) extended upper expansion blade group (8d) in the circumferential direction of 380 degrees expansion, outside the turbine Various energy storage cycle coalescence engines and coalescence methods in which the compressed air portion (9D) is compressed between the box (77a) and the air injection nozzle (5) increases the fuel combustion amount at a plurality of locations.   Horizontally moving blade ratio critical material gravity turbine (8U) with magnetic bearing load approaching 0 + super high speed circumferential speed Electricity + liquid air cold heat + hot water to superheated steam heat supply equipment (3D) ) Fuel injection combustion with receiving cheaper liquid oxygen (5K) + electricity + high temperature water, and fuel injection combustion from multiple locations in the fuel pipe (25a) extended upper expansion blade group (8d) in the expansion process of 380 degrees in the circumferential direction , Various energy storage cycle coalescence engines and coalescence methods for compressing the compressed air portion (9D) with the turbine outer box (77a) and increasing the amount of fuel injected by the air injection nozzle (5) at a plurality of locations.   Horizontally moving blade ratio critical material gravity turbine (8U) with 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 fuel injection and combustion of cheaper liquid oxygen (5K) + hot water, and injected and combusted fuel from multiple locations of the fuel pipe (25a) extended upper expansion blade group (8d) in the circumferential expansion process of 380 degrees, turbine Various energy storage cycle coalescence engines and coalescence methods in which the compressed air portion (9D) is compressed between the outer box (77a) and the air injection nozzle (5) increases the fuel combustion amount at a plurality of locations.   Cylindrical turbine blade group with a gravity-accelerated acceleration of gravitational acceleration (mixed injection under ultra-high pressure vertically under vacuum) 8A) A horizontal shaft (16A), an opposed synchronous gear (4C), an in-series rotating gear (4D), and various energy storage cycle coalescing engines and coalescence methods for generating electric power with a plurality of turbines.   Cylindrical turbine blade group with a gravity-accelerated acceleration of gravitational acceleration (mixed injection under ultra-high pressure vertically under vacuum) 8A) Various energy storage cycle coalescing engines and coalescence methods for rotating the horizontal shaft (16A) in series with the same rotating gear (4D) and generating electric power with a plurality of turbines.   Horizontally moving blade ratio critical material gravity turbine (8U) with a magnetic bearing load approaching 0 and super high speed circumferential speed. Ultra-high pressure vertically below the vacuum in the vacuum, accelerating gravitational acceleration and cylindrical turbine blade group (8A) horizontal Various energy storage cycle coalescence engines and coalescence methods for rotating a shaft (16A) and generating a large number of cylindrical turbine blade groups (8A).   Horizontally moving blade ratio critical material gravity turbine (8U) with a magnetic bearing load approaching 0 and super high speed circumferential speed. Ultra-high pressure vertically below the vacuum in the vacuum, accelerating gravitational acceleration and cylindrical turbine blade group (8A) horizontal Various energy storage cycle coalescence engines and coalescence methods for generating 20 sets of cylindrical turbine blade groups (8A) by rotating a shaft (16A).   Horizontally moving blade ratio critical material gravity turbine (8U) with a magnetic bearing load approaching 0 and super high speed circumferential speed. Ultra-high pressure vertically below the vacuum in the vacuum, accelerating gravitational acceleration and cylindrical turbine blade group (8A) horizontal Various energy storage cycle coalescence engines and coalescence methods for generating 40 sets of cylindrical turbine blade groups (8A) by rotating a shaft (16A).   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. Various energy storage cycle coalescence engines and coalescence methods for generating 80 sets of cylindrical turbine blade groups (8A) by rotating a shaft (16A).   Horizontally moving blade ratio critical material gravity turbine (8U) with a magnetic bearing load approaching 0 and super high speed circumferential speed. Ultra-high pressure vertically below the vacuum in the vacuum, accelerating gravitational acceleration and cylindrical turbine blade group (8A) horizontal Various energy storage cycle coalescence engines and coalescence methods for generating 100 sets of cylindrical turbine blade groups (8A) by rotating a shaft (16A).   Horizontally moving blade ratio critical material gravity turbine (8U) with a magnetic bearing load approaching 0 and super high speed circumferential speed. Ultra-high pressure vertically below the vacuum in the vacuum, accelerating gravitational acceleration and cylindrical turbine blade group (8A) horizontal Various energy storage cycle coalescence engines and coalescence methods for generating 150 sets of cylindrical turbine blade groups (8A) by rotating a shaft (16A).   Horizontally moving blade ratio critical material gravity turbine (8U) with a magnetic bearing load approaching 0 and super high speed circumferential speed. Ultra-high pressure vertically below the vacuum in the vacuum, accelerating gravitational acceleration and cylindrical turbine blade group (8A) horizontal Various energy storage cycle coalescence engines and coalescence methods for generating 200 sets of cylindrical turbine blade groups (8A) by rotating a shaft (16A).   Magnetically utilized bearing load approaching 0 + ultra-high speed circumferential speed with full blade ratio critical material gravity turbine (8U) power generation electrical product + rocket combustion + various energy conservation to drive oxygen combined water injection part (88L) as jet combustion Cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) power generation electric product + 2 rocket combustion + jet combustion 2 locations driven by oxygen combined water injection unit (88L) with magnetic bearing load approaching 0 + super high speed circumferential speed Various energy storage cycle coalescence engine and coalescence method.   Horizontally-moving blade ratio critical material gravity turbine (8U) power generation electrical product + 3 rocket combustion + jet combustion 3 locations driven by oxygen combined water injection unit (88L) with magnetic bearing load approaching 0 + super high speed circumferential speed Various energy storage cycle coalescence engine and coalescence method.   Horizontally-moving blade ratio critical material gravity turbine (8U) power generation electrical product +4 rocket combustion + jet combustion 4 locations driven by oxygen combined water injection unit (88L) with magnetic bearing load approaching 0 + super high speed circumferential speed Various energy storage cycle coalescence engine and coalescence method.   Horizontally-moving blade ratio critical material gravity turbine (8U) power generation electric product + 5 rocket combustion + 5 jet combustion 5 sites driven by oxygen combined water injection unit (88L) Various energy storage cycle coalescence engine and coalescence method.   Horizontally-moving blade ratio critical material gravity turbine (8U) power generation electric product + 6 rocket combustion + 6 jet combustion 6 locations driven by oxygen combined water injection unit (88L) with magnetic bearing load approaching 0 + super high speed circumferential speed Various energy storage cycle coalescence engine and coalescence method.   Horizontal type full blade ratio critical material gravity turbine (8U) power generation electrical product + rocket combustion + jet combustion as oxygen combined air injection unit (88B) driven by magnetically combined bearing load 0 approach + super high speed circumferential speed Various energy conservation Cycle coalescence engine and coalescence method.   Horizontally moving blade ratio critical material gravity turbine (8U) power generation electrical product + 2 rocket combustion + jet combustion 2 locations driven by oxygen combined air injection unit (88B) with magnetic bearing load approaching 0 + super high speed circumferential speed Various energy storage cycle coalescence engine and coalescence method.   Horizontally-moving blade ratio critical material gravity turbine (8U) power generation electrical product + 3 rocket combustion + jet combustion 3 locations driven by oxygen combined air injection unit (88B) with magnetic bearing load approaching 0 + super high speed circumferential speed Various energy storage cycle coalescence engine and coalescence method.   Horizontally-moving blade ratio critical material gravity turbine (8U) power generation electric product +4 rocket combustion +4 jet combustion 4 locations driven by oxygen combined air injection unit (88B) Various energy storage cycle coalescence engine and coalescence method.   Horizontally-moving blade ratio critical material gravity turbine (8U) power generation electric product + 5 rocket combustion + 5 jet combustion 5 oxygen drive air injection unit (88B) drive with magnetic bearing load approaching 0 + super high speed circumferential speed Various energy storage cycle coalescence engine and coalescence method.   Horizontally-moving blade ratio critical material gravity turbine (8U) power generation electrical product + 6 rocket combustion + jet combustion 6 locations driven by oxygen combined air injection unit (88B) with magnetic bearing load approaching 0 + super high speed circumferential speed Various energy storage cycle coalescence engine and coalescence method.   Horizontal type whole blade ratio material gravity turbine (8U) Receives cheap liquid oxygen (5K) from electricity + liquid air cold heat + high temperature water to superheated steam temperature supply equipment (3D) of extremely low cost electric power production, oxygen combined water Various energy storage cycle coalescence engines and coalescence methods for jetting bubbles into the bottom vertical parallel plate (9Q) as an injection unit (88L) driven oxygen coalescence injection ship (39R).   Horizontal type whole blade ratio material gravity turbine (8U) Receives cheap liquid oxygen (5K) from electricity + liquid air cold heat + high temperature water to superheated steam temperature supply equipment (3D) of extremely low cost electric power production, oxygen combined water Various energy storage cycle coalescence engine and coalescence method in which an injection unit (88L) driven oxygen coalescence screw injection vessel (39S) is used to inject a maximum amount of bubbles into the bottom vertical parallel plate (9Q).   Horizontal type whole blade ratio material gravity turbine (8U) Receives cheap liquid oxygen (5K) from electricity + liquid air cold heat + high temperature water to superheated steam temperature supply equipment (3D) of extremely low cost electric power production, oxygen combined water Various energy storage cycle coalescence engines and coalescence methods that maximize the air levitation amount by making the injection unit (88L) driven oxygen coalescence injection ship (39R) wide in the bottom vertical parallel plate (9Q).   Horizontal type whole blade ratio material gravity turbine (8U) Receives cheap liquid oxygen (5K) from electricity + liquid air cold heat + high temperature water to superheated steam temperature supply equipment (3D) of extremely low cost electric power production, oxygen combined water Various energy storage cycle coalescence engines and coalescence methods that make the injection part (88L) driven oxygen coalescence screw injection ship (39S) wide and provide a wide bottom vertical plate (9Q) to maximize the amount of air floating.   Horizontal type whole blade ratio material gravity turbine (8U) Receives cheap liquid oxygen (5K) from electricity + liquid air cold heat + high temperature water to superheated steam temperature supply equipment (3D) of extremely low cost electric power production, oxygen combined water Various energy storage cycle coalescence engines and coalescence methods that maximize the friction reduction amount by making the injection section (88L) driven oxygen coalescence injection ship (39R) wide in the bottom vertical parallel plate (9Q).   Horizontal type whole blade ratio material gravity turbine (8U) Receives cheap liquid oxygen (5K) from electricity + liquid air cold heat + high temperature water to superheated steam temperature supply equipment (3D) of extremely low cost electric power production, oxygen combined water Various energy storage cycle coalescence engines and coalescence methods for making the injection part (88L) driven oxygen coalescence screw injection ship (39S) wide and providing a bottom vertical parallel plate (9Q) wide to maximize friction reduction.