JP2014211146A - Various kind energy conservation cycle combination engine - Google Patents

Abstract

PROBLEM TO BE SOLVED: To provide a various kind energy conservation cycle combination engine by which the most amount of producible energy on the earth with power generation can produce water 3E jetting speed, vacuum and difference in height infinitely with gravity acceleration in vacuum or difference in height of large specific gravity substance by virtue of human kind wisdom.SOLUTION: A column pipe 12B of a gravity power generation building 12 for producing a difference in height is used as a transverse total moving blade water gravity turbine 11C and a large-specific gravity substance raising device 2F which raises water 3E to the highest part, conserves and jets the water, and accelerates the water with gravity acceleration in vacuum to perform power generation. As a target 1,000 times power generation amount of the existing water elevation power generation by the use of the same water quantity, a simple gas engine 89 P+a vertical total moving blade steam turbine 11F is used. As a target 1,000 times power generation amount of the existing thermal power generation, steam expansion speed+gravity acceleration use in vacuum is used. As a target 10 times speed of air planes and ships and as a target 1/100 fuel expenses of automobiles, various kinds of engines such as 100 times rotation output+100 times jetting propulsion output are used. As a target 1/500,000 space arrival expenses, an airplane which has the best application profitability in the world capable of applying all products so as to permit a day's trip to everywhere in the world is used.

Description

The horizontal full-blade water gravity turbine 11C power generation electric product-containing drive of the present invention has practically used a full-rotation counter-rotating engine that is difficult to manufacture, with cutting-edge science and technology being avoided. Although it is proportional to the third power, the power generation amount is proportional to the square of the water speed, and the rotation output and the injection propulsion output that challenge the infinite increase in speed are set, and the adiabatic compression air temperature is 13 times the compression ratio of 8 The compressed air heat exchanger 2Y that compresses the air 28a heated by the solar heater 21 is used, and the production ratio of the superheated steam 5H with a compression ratio of 80 to 100 is aimed at 100 times that of the existing fuel boiler. Type full rotor blade steam turbine 11F Gravity acceleration while raising the vacuum degree + superheated steam 5H expansion speed power generation, the same heat amount 10 times the speed of existing steam turbine power generation 100 times power generation target, the same amount of fuel including the unexpected fire Assuming that the amount of power generation is 1000 times that of power generation and that the amount of power generation is proportional to the mass of water × square of speed × head, the height and strength of the gravity power generation building 12 + specific material rising device 2F are the most important, and the column 12B Is used as the specific material rising device 2F to increase the diameter of the steel frame 12A by increasing the tube diameter, and as a high-rise building with a height suitable for the application, the horizontal full-blade water gravity turbine 11C Various types of bearings 12C are provided at both ends of the inner shaft device 60A and the outer shaft device 60B, respectively, as power generation and vertical-type full blade steam turbine 11F power generation. Each of the inner shaft device 60A and the outer shaft device 60B is temporarily assembled separately, and both ends are held by a machine tool. Combined engine with various energy storage cycles driven by a horizontal full blade hydrogravity turbine 11C power generation electric product containing the A / cylindrical inner blade group 60C and the outer shaft device 60B / cylindrical outer blade group 60D. Further, the present invention relates to a technique for combining various energy conservation methods.

In the horizontal type full-blade water gravity turbine 11C power generation electric drive engine and the electric product-containing drive engine, the inner shaft device 60A + the outer shaft device 60B is used as the rotational balance adjustment processing at the time of ultra-high speed rotation in the same manner as described above. Various bearings 12C are provided at both ends, the inner shaft device 60A and the outer shaft device 60B are each temporarily assembled separately, and both ends are held by a machine tool. And a liquid oxygen production machine 89A, a simple multistage compressor 89B, a simple gas engine 89C, and a simple air injection engine 89D, in which an unprecedented cylindrical inner blade group 60C and a cylindrical outer blade group 60D are double-reversed. Alternatively, the simple injection engine 89E is driven, and the production amount of the superheated steam 5H is most important in the driving process, and the compressed air heat exchanger 2Y compression ratio existing gas turbine compression ratio 30 to 40 is changed to 50 to 1. Aiming at zero, simple gas engine 89C + vertical moving blade steam turbine 11F thermal vacuum gravity power generation, simple gas engine car 89F, simple gas engine ship 89G, simple gas engine airplane 89H, simple air injection engine ship 89I, simple jet engine airplane 89J, rotary wing airplane 89K, rotary wing jet airplane 89L, extra large Osprey 89M and large Osprey 89N are driven. Oxygen and CO2 supply Microorganisms and seaweeds will increase, and food such as fish will greatly increase in the food chain, etc., and by plane and automobile drive, CO2 emissions will be 1/100, fuel costs will be 1/100, and 1 / 500,000 will reach the universe Aiming at 10x speed for airplanes and ships, each aiming to be the world's most eternally sustainable operating profit rate. It relates to a technique of formic save coalescence method.

From the practical use of the existing state-of-the-art science and technology, the pumping input of pumped-storage power generation becomes an input proportional to the cube of the rotational speed, so the power generation amount is proportional to the cube of the water speed to the square of the water speed by adopting a variable speed motor. Since the water speed of the existing pumped-storage power generation of the existing state-of-the-art science technology that is assumed to be too lazy is Mach 1/7 or Mach 1/5, the experimental result is not expected with Mach 10 that is 1/5 of Russian falling meteorite speed Mach 50 When the water injection speed Mach 3 having the same water mass as that of the existing pumped storage power generation is manufactured and the gravitational acceleration during the increase in the vacuum degree is manufactured and used as the Mach 10, the same water mass Mach 10 ÷ 1/5 = 50 as that of the existing pumped storage power generation is used. Double water velocity = 50 times × 50 times power generation amount = 2500 times power generation amount, and there is a background technology in which the power generation amount after subtracting the input of Mach 3 injection is about 1000 times, manufacturing the water mass rate and manufacturing the head Is infinite due to architectural and manufacturing technologies Japan's budget deficit of 1,000 trillion yen is relatively short due to the global warming prevention revolution, the economic growth strategy revolution, and the world's most eternal revolution with outstanding operational profit rate. There is a background technology that can aim at zero in between.

  The boiler of thermal power generation of the existing state-of-the-art technology produces superheated steam by atmospheric pressure fuel combustion and power generation by steam turbine, but the temperature rise of adiabatic compression is 260 ° C which is 13 times the air temperature 20 ° C and the compression ratio 8 Because of the existing state-of-the-art science and technology that is too lazy, as a simple gas engine 89P, a compressed air heat exchanger 2Y aimed at a compression ratio 80 to 100 aimed at 10 times the compression ratio 8, and a fuel injection combustion heat exchange superheated steam 5H When manufactured, the combustion temperature becomes about 130 times, and the same fuel amount that needs experimentation may become about 130 times the amount of superheated steam 5H production of existing boilers. The rotor blades are alternately provided about 20 each, and the steam speed is set to brown-free expansion that repeats damming direction change injection about 20 times with the stationary blades, and the stationary speed blades that do not generate rotational output with the steam speed set to 1/10, etc. Therefore, aiming at 100 times the power generation of existing steam turbine power generation by using gravity moving acceleration production while steam expansion speed + vacuum degree increase as a fully-rotating double-rotating vertical all-blade steam turbine 11F that completely abolished stationary blades As a simple gas engine 89P + vertical all-blade steam turbine 11F power generation, aiming to generate the same fuel amount 1000 times that of the existing thermal power generation, including the amount of superheated steam 5H produced and unexpected, the result of the experiment is the existing double power generation There are background technologies that can aim to reduce Japan's fiscal deficit of 1,000 trillion yen to 0 in a relatively short period of time due to the global warming prevention revolution, economic growth strategy revolution, and the world's most eternal revolution with a high return on investment. .

Existing state-of-the-art science and technology airplanes and marine gas turbines are equipped with alternating stationary blades and moving blades. The wings are swelled repeatedly by changing the direction of damming, and half of the stationary blades with no work are alternately provided with the moving blades. Since the airplane speed and ship speed are reduced to 1/10, etc., the superheated steam 5H of the compressed air heat exchanger 2Y aimed at a compression ratio of 50 to 100 is manufactured, and heat exchange such as a combustion temperature of 30 times to 50 times is performed. A simple gas engine 89C, a simple air injection engine 89D, a simple injection engine 89E, etc., with the same fuel amount and 30 to 50 times the superheated steam 5H production amount of the existing boiler, with all rotor blades counter-rotating. Output already Aiming for 100 to 1000 times the speed of gas turbines, aiming for 10 times the speed of airplanes and ships, aiming for the prime of space flight, the space arrival cost 1 / 500,000, orbiting the earth 16 times a day, etc. There is also a background technology that can aim to reduce Japan's budget deficit of 1,000 trillion yen to 0 in a relatively short time due to the world's most eternal revolution.

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PCT International Application Publication No. There are applications of WO 2010/101017 PCT / JP2010 / 052171, and the filing date of Japanese Patent Application 2007-179204: July 9, 2007 to the filing date of Japanese Patent Application 2007-265115: October 11, 2007 No. 2008-006612 filing date: January 16, 2008 to No. 2008-327045 filing date: There are 45 applications from December 24, 2008, filing date of Japanese Patent Application No. 2009-011656: From January 22, 2009, the filing date of the Japanese Patent Application 2009-298004: There were 322 applications until December 28, 2009, and the filing date of the Japanese Patent Application 2010-000841: the Japanese Patent Application 2010 from January 6, 2010 -0332424 Submission date: There were 32 applications until February 18, 2010, and Japanese Patent Application No. 2011-055078 submission date: 2011 There are 22 applications from March 14 to the date of submission of the Japanese Patent Application 2011-267508 to December 7, 2011, the date of submission of the Japanese Patent Application 2012-032245: the date of submission of the Japanese Patent Application 2012-271355 from February 17, 2012 : There are 29 applications until December 12, 2012, and the filing date of Japanese Patent Application 2013-7975: From January 21, 2013, the filing date of Japanese Patent Application 2013-59199: six until March 22, 2013 There is an application.

  In the power generation part of the existing state-of-the-art science and technology, the unit code violation of the work load kg weight m / sec is obvious, such as using only potential energy and generating less than the pumped power. The power generation increase is nothing, and the point that is too unreasonable is improved with the same water mass 1000 times aiming at the power generation amount, the thermal power generation of the existing state-of-the-art technology that is too lazy is the compressed air heat exchanger 2Y + vertical moving blade steam turbine 11F Therefore, the improvement of the compressor and turbine of the gas turbine that drives airplanes and ships by improving the target fuel generation by 1000 times the same fuel amount is provided with alternating stationary blades and moving blades, and the compressor uses compressed air. Repeated damming with stationary blades and repeated unreserved compression, turbines repeatedly damped with stationary blades and reversing injection, consuming almost all of gas velocity with stationary blades that do not work at all, etc. To improve the Gil point, there is a problem that the 1000-fold rotational output and the injection propulsion output aimed.

Water injection speed production + gravity acceleration production in vacuum + head production, horizontal water turbine 11C power generation with the same water mass aiming at 1000 times the power generation capacity of existing pumped storage power generation, for example, liquid oxygen production machine 89A of this electric drive A simple gas engine 89C including a solar heater 21 + compressed air heat exchanger 2Y, and a vertical all blade steam turbine 11F including a liquid oxygen drive manufactured in the above, and a compression work rate of 21/60000 volumetric compression work rate of air compression. The simple gas engine 89C, the simple air injection engine 89D, and the simple injection engine that can be connected to the simple multi-stage compressor 89B with the aim of generating the same fuel amount 1000 times that of the existing thermal power generation. The 89E drive is used to drive vehicles such as automobiles, ships, and airplanes that are 1000 times the rotation output and injection propulsion output of existing gas turbines. Then, the plane will inject superheated steam rockets from around the existing highest flight altitude, and the space arrival cost will be about 1 / 500,000 of the existing space arrival cost, which is about the fuel cost of the existing aircraft, aiming at the prime of space flight and the earth on the day 16 laps, etc. A day trip anywhere on the earth and CO2 exhaust in the atmosphere aiming for a little flight, 100% world-wide monopolized power generation, ships, airplanes, automobiles, etc. Improve the unreasonable point of power. Make it a revolution of 2 to 1000 times the existing output, make it the world's most eternal aim with outstanding operating profit rate for all product operations and the world's best for new employment, and prevent global warming.

The experimental result is long-awaited, but when adding gravity acceleration production + injection velocity production + head production in vacuum to the power generation part of the existing pumped storage power generation, the power generation amount with the same head and the same head is more than 10 times that of the existing pumped power generation If the heat production that compresses the air heated by the solar heater 21 in the electrically driven liquid oxygen production machine 89A with the low cost power generation of the horizontal all-blade water gravity turbine 11C, the fuel cost is great. Superheated steam 5H thermal production + 0% near infinity + liquid oxygen 5K cold production + liquid nitrogen 5L cold production, for example, has a great effect on heat utilization such as methane recovery in the sea near Japan, and by-product liquid nitrogen and liquid oxygen are also enormous Therefore, liquid nitrogen has a great effect that it can be used as various types of cold heat such as ice production. When liquid oxygen is used instead of air compression, the compression work rate is 21/6000 of air compression. In order to drive the volumetric compression power, drive the simple gas engine 89C, the simple air injection engine 89D, the simple injection engine 89E, and the like to drive the vehicles such as automobiles, ships, and airplanes by rotational force driving and jet driving, It has a great effect of targeting 10 fuel costs and 10 times the speed, and an effect of reducing the space arrival cost to about 1 / 500,000 of existing rockets, and has the effect of making a global warming prevention revolution.

  Compressed air heat exchanger 2Y + all-blade counter-rotating ultra-high pressure compressed air Injecting combustion heat exchange superheated steam 5H, the adiabatic compression air temperature is 13 times the compression ratio 8, so the compression ratio is 50-100 The production of superheated steam 5H has the effect of bringing the amount of superheated steam 5H produced with the same fuel amount closer to 100 times that of existing boilers, and the fuel combustion mass can be made four times that of existing gas turbines to the stoichiometric air-fuel ratio. This has the effect of bringing the rotational output and injection propulsion output of the gas 49 closer to four times other than full rotor blade reversal. In full rotor blade reversal thermal power generation, air heated by the solar heater 21 of the simple gas engine 89P Because the superheated steam 5H is produced by the fuel injection combustion in the compressed air heat exchanger 2Y, the same fuel amount has a great effect on the production quantity of the superheated steam 5H that is 100 times that of the existing boiler. The vertical all blade steam turbine 11F accelerates by the gravitational acceleration while the steam expansion speed + the degree of vacuum rises, and produces a rotational output. This has the effect of bringing the superheated steam speed closer to 10 times that of the existing steam turbine. The same amount of fuel, including the production amount, has the great effect of bringing it closer to 1000 times the amount of electricity generated by existing thermal power generation.

Illustration of gravity power building 12 (Example 1) Explanatory drawing of a horizontal type full-blade water gravity turbine 11C (Example 2) Explanatory drawing of the horizontal type full-blade water gravity turbine 11C bearing 12C (Example 3) Explanatory drawing of the solar heater 21 (Example 4) Explanatory drawing of liquid oxygen production machine 89A (Example 5) Explanatory drawing of simple multistage compressor 89B (Example 6) Illustration of simple gas engine 89C (Example 7) Explanatory drawing of compressed air heat exchanger 2Y (Example 8) Explanatory drawing of vertical all blade steam turbine 11F (Example 9) Explanatory drawing of simple air injection engine 89D (Example 10) Explanatory drawing of the simple injection engine 89E (Example 11) Illustration of simple gas locomotive 89F (Example 12) Explanatory drawing of simple gas engine ship 89G (Example 13) Explanatory drawing of simple gas engine airplane 89H (Example 14) Explanatory drawing of the simple air injection engine ship 89I (Example 15) Explanatory drawing of simple injection engine airplane 89J (Example 16) Explanatory drawing of rotary wing airplane 89K (Example 17) Explanatory drawing of rotary wing jet airplane 89L (Example 18) Illustration of oversized Osprey 89M (Example 19) Illustration of Large Osprey 89N (Example 20)

  Since there is no precedent of counter-rotating engines in the existing technology, and almost all of the present invention except counter meshing rotation is related to counter-rotating engines, the cylindrical inner rotor blade group 60C and the cylindrical outer rotor blade group 60D are respectively connected in the manufacturing process. Separately tentatively assembled, equipped with various bearings 12C at both ends, which can be rotated and machined with machine tools in the same way as during operation, and each of them can be disassembled and assembled after processing with good balance operation even at ultra-high speed rotation. Focusing on new processing technology, aiming to generate 1000 times the same amount of pumped power as existing pumped power generation, aiming to generate 1,000 times the same amount of fuel as existing thermal power generation, and aiming for 1 / 500,000 of the same fuel amount to reach the space We will try to demonstrate the latest state-of-the-art science technology that is too unreasonable by experimenting with the aim of astronautics in spaceflight and planes and ships with 10 times the same amount of fuel.

The gravity power generation building 12 in FIG. 1 calculates 1/7 to 1/5 of pumped water generation water speed sound speed as gravity acceleration production in vacuum + injection speed Mach 1 to 3 production, and water 3E speed Mach 10 is calculated with the same head power generation. The same water 3E mass pumped-storage power generation 10 ÷ 1/5 = 50 times speed = 50 × 50 power generation amount = 2500 power generation amount, aiming at 1000 times power generation amount including the increase in injection speed input and unexpected In the process of accelerating the gravitational acceleration while raising the vacuum degree, aiming at the infinite production power generation amount infinite increase in the gravitational power generation building 12, the water 3E of a specific critical material is jetted at high speed from the top of the gravitational power generation building 12 In order to drive the outer blade group 60D + cylindrical inner blade group 60C by inversion and driving each of the horizontal all blade water gravity turbines 11C one after another, the specific material 3E by the specific material raising device 2F And luck to the top of 2E The carrying speed is important. Therefore, the column of the gravitational power generation building 12 is used as the column tube 12B and the significant substance rising device 2F, and the diameter of the column tube 12B is enlarged to make it a sturdy column, and the pumping power is reduced at a low rate of rise. In accordance with the steel frame 12A, the upper and lower sides of the steel frame 12A are bolted and assembled to the square flange 12D, and the gravity power generation building 12 is used inside the column tube 12B as the specific material raising device 2F. 3E is stored at the top, and is injected with Mach 1 to 3 by the specific material accelerator 6W to make the acceleration of gravity acceleration while raising the degree of vacuum to produce a horizontal all blade hydrogravity turbine 11C power generation. Combined engine power generation and combined method power generation.

The horizontal full-blade hydrogravity turbine 11C power generation of FIG. 2 includes a counter synchronous gear 4C4C that enables counter meshing rotation corresponding to heavy-weight linear ultra-high-speed injection, assuming that the amount of power generation is proportional to the square of the speed. Thus, the number of rotation shafts of the unified generator 1 is increased by the series rotation gear 4D, and the column pipe 12B of the gravity power generation building 12 is adjusted to the height of the generator 1, and 50 to 100 sets, etc. The column tube 12B having the square flange 12D for assembling the steel frame 12A is also provided, and the column tube 12B and the significant substance raising device 2F is used to store the water 3E at the top by a variable speed motor, and the pumping input is the rotational speed. Corresponding to the third power, water 3E is injected by Mach 3 etc. with a specific material accelerator 6W, and the acceleration of gravity in vacuum is increased to a higher degree of vacuum than the existing steam turbine. In the existing pumping Same water mass as electricity Mach 10 ÷ 1/5 = 50 times water speed, 50 times × 50 times power generation amount = 2500 times power generation amount, Mach 3 injection input after subtracting power generation amount after 1000 times, horizontal type Fully bladed water gravity turbine 11C series intermeshing mesh rotation drive, water 3E speed and water 3E head are infinitely manufactured, greatly improve the existing state-of-the-art science and technology, and the same pumping amount can be double that of existing pumping power generation Experiments are required to aim for 1000 times the amount of power generation, but the power generation amount is infinitely increased at zero fuel cost, making it the best in the world to prevent global warming, making the energy conservation cycle coalescence engine power generation and coalescence method power generation .

The horizontal full-blade hydrogravity turbine 11C shown in FIG. 3 is manufactured and driven so that the amount of power generation is proportional to the square of the speed, so that it corresponds to a heavy-weight linear ultra-high speed, and the husband rotates counter-meshing at ultra-high speed. The turbine blade group 8A + cylindrical turbine blade group 8A is provided with an optimum bearing 12C, a horizontal shaft plate 16 and a horizontal shaft 16A at both ends, respectively. Precisely finish, the horizontal shaft plate 16 and the horizontal shaft 16A are fixed with precision finish bolting, etc., and bearings 12C are provided at both ends, so that both ends are held by a machine tool. As the processing, each of the high-speed balance adjustment processing operation after good processing is disassembled and precision main assembly, etc., and a completely long cylindrical turbine blade group 8A is recorded with completely new assembly processing technology and assembly technology. The column pipe 12B and the specific material rising device 2F store the water 3E in the uppermost position and inject the water 3E with the specific material accelerator 6W of the turbine outer box 77a by the Mach 3 or the like. Manufacturing and driving the horizontal full-blade water gravity turbine 11C, the power generation aiming to construct around 100 sets, around 800m drop and infinite places with the gravity power generation building 12, and the world's most profitable prevention of global warming Energy conservation cycle coalescence engine power generation and coalescence method power generation.

Since the heat production of the solar heater 21 in FIG. 4 is 260 ° C. with an adiabatic compression ratio of 8 at 20 ° C., the air 28a heated by the solar heater 21 with a simple gas engine 89P is compressed to an ultrahigh pressure such as 20 MPa. , The fuel injection combustion heat exchange superheated steam 5H is produced by the compressed air heat exchanger 2Y, and the superheated steam 5H production amount of the same fuel amount is aimed at 100 times that of the existing boiler, and the vertical all blade steam turbine 11F is driven identically. Aiming at a power generation amount 1000 times that of the existing thermal power generation, when the liquid oxygen producing machine 89A is driven in the same manner, the superheated steam 5H heat + liquid air 28a is produced cold, and the electricity + liquid air cold heat + superheated steam heat supply equipment 3D is produced. In this figure, the solar heater 21 is provided with buoyancy on the water surface or a circular railroad on the flat surface, and the solar light is maintained at right angles from the east to the west. No As an upper device or a land device, the solar heater 21 is provided with a rotation support portion 4f and is equipped with a gear device 4d and a roller 4e. A device that controls rotation at right angles in the east-west direction by using a circular railroad, and that controls the rotation of sunlight at two angles at right angles to maximize the air temperature in the heat absorption tube 4H that is aimed at the maximum amount of heat stored and preserved. The light is collected in a straight line by the rectangular long lens 2d, the heat absorption tube 4H is provided near the focal length, the internal air passage 28A air 28a temperature is maximized, the external air passage 28A air 28a temperature rises, As the long lens 2d that extends linearly, the entire lens material can be used, and the heat insulating material 2c such as foamed plastic is surrounded by a cylindrical rotating portion 77G or the like as a long cylinder such as a cylinder. The long length lens 2d and sealed with joint 80A + fasteners 80B, the external air passage 28A the internal heat absorbing tube 4H top as an internal air passage 28A, to solar heater 21 of second air passage 28A selection inhalation.

  The liquid oxygen producing machine 89A in FIG. 5 uses the horizontal full-blade water gravity turbine 11C fuel cost 0 power generation electric drive and the vertical full-rotor blade steam turbine 11F power generation electric drive, and the air 28a heated by the solar heater 21 is Including simple multi-stage compressor 89B connection and water jet cooling compression selection, ultra-high pressure compression is performed by simple compressor 3s, and heat is recovered by compressed air heat exchanger 2Y water pipe 52B + low temperature air heat exchanger 2w alcohol pipe 52C, 100 Water 52A production such as ° C. + alcohol 52C—cooling air 28a around 100 ° C. In the process of air turbine 3t drive adiabatic expansion impulse drive, liquid oxygen 5K and liquid according to the impulse pressure and liquefaction temperature of each turbine blade stage Nitrogen 5L liquefied injection, divided from the lower outer periphery of each paragraph, recovered with liquid oxygen 5K, liquid nitrogen 5L, etc., and heat exchange with air turbine 3t exhaust approaching absolute 0 degree The low-temperature exhaust heat exchanger 2V is driven, the low-temperature exhaust heat exchanger 2V alcohol pipe 52C is set to about -100 ° C., the alcohol pipe 52C is extended to the low-temperature air heat exchanger 2w, and the compressed air 28a is supplied. The temperature is set to the lowest possible cooling, and the exhaust temperature of the air turbine 3t is made to circulate close to absolute 0 °, and the mass production of liquid oxygen 5K + liquid nitrogen 5L is aimed at mass production. Bearings 12C are provided at the optimum positions on both ends of each of the blade group 60D and the outer shaft device 60B. Enables holding precision processing, enables ultra-high speed rotation balance adjustment processing, and also serves as inner shaft device 60A, inner compression blade 8q, inner output blade 8s, and outer shaft device 60B. As a manufacturing balance adjustment process for the side compressor blades 8r and the outer output blades 8t, the main shaft device 60A and the outer shaft device 60B are super-high-speed double-reversed by this assembly and injected into methane hydrate by mass production of water 52A. By making the best use of isothermal heat to recover methane, liquid oxygen 5K and liquid nitrogen 5L are used in various engines, and the compression work rate is set to various engines of selective driving of ultra-high pressure combustion parts such as 21/60000 and 79/60000. A liquid oxygen production machine 89A is used for driving various types of rotation or ultra-high-speed jet propulsion to a ship or a car.

A simple multi-stage compressor 89B shown in FIG. 6 is connected to various engines to produce ultra-high pressure compressed air 28a including selection of water jet cooling compression, and includes a cylindrical inner blade group 60C and inner shaft device 60A and a cylindrical outer side. Bearings 12C are provided at the optimum positions at both ends of the blade group 60D and the outer shaft device 60B, respectively. For precision holding processing, ultra-high-speed rotation balance adjustment processing, etc., a plurality of inner shaft devices 60A and inner compression blades 8q and outer shaft devices 60B and outer compression blades 8r are manufactured and balanced, and each is disassembled and assembled. In this way, the inner shaft device 60A and the outer shaft device 60B have excellent ultra-high speed double reversal, and the air 28a sucked from the outer casing blade 6G is compressed by ultra-high speed rotation and ultra-high pressure, and heat exchange is performed by the compressed air heat exchanger 2Y. Excessive As a simple multistage compressor 89B for producing high-pressure compressed air 28a at an optimum temperature, such as two-time compression or three-time compression for producing steam 5H, it is connected to various engines, a liquid oxygen production machine 89A, a simple gas engine 89C, Micro super high speed simple multi-stage that drives simple air injection engine 89D, simple injection engine 89E, etc. to generate rotation output and injection propulsion output to make various rotation drive and ultra high speed injection propulsion drive for airplanes, ships, automobiles, etc. A simple multistage compressor 89B including the compressor 89B is connected in various ways.

In the simple gas engine 89C experimental result prediction and manufacturing method of FIG. 7, the air 28a sucked from the outer box nozzle 6G is compressed by the outer compression blades 8r and the inner compression blades 8q. The production of superheated steam 5H in the compressed air heat exchanger 2Y is a combustion heat exchange aimed at 50-100 with a compression ratio of 30-40 or more of the existing gas turbine. Aiming for production volume, combustion gas 49 + superheated steam 5H is injected into the outer output blade 8t and the inner output blade 8s, and the entire rotor blade double reversal linear expansion drive + superheated steam 5H production volume increases, resulting in 1000 times rotation of the existing gas turbine. Aiming at the output and the jet propulsion output, the manufacturing method is as follows. The bearing 1 is located at the optimum positions at both ends of the cylindrical inner blade group 60C and inner shaft device 60A and the cylindrical outer blade group 60D and outer shaft device 60B. C, and each of the assembly assembly parts 9M screw assembly screw fixing and press-fitting screw fixing, etc. after temporary assembly in the same way as in this assembly, both ends are precision-machined with machine tools, and ultra-high-speed rotation balance adjustment processing is performed well. As a manufacturing balance adjustment process for the device 60A, the inner compression blade 8q, the inner output blade 8s, the outer shaft device 60B, the outer compression blade 8r, and the outer output blade 8t, the inner shaft device 60A Long-distance compression of the outer shaft device 60B with closed inlet, including ultra-high-speed counter-rotating air compression and rotational output generation, including the drive of liquid oxygen turbine 5C + liquid nitrogen 5L of horizontal full-blade water gravity turbine 11C In the process of using the air heat exchanger 2Y, liquid oxygen 5H or liquid nitrogen 5L is injected from the oxygen / nitrogen injection nozzle 6M, and fuel is injected and combusted from the fuel injection nozzle 6X. 0000 + 79/60000 Ultra high-pressure combustion, aiming at 1000 times rotation output and injection propulsion output of existing gas turbine with the same fuel amount Various types of rotation drive as airplanes, ships and automobiles aiming for 10 times speed and 1/100 fuel cost Or a simple gas engine 89C, which is driven by ultra-high speed injection propulsion.

  FIG. 8 is a developed view showing various usage examples of the compressed air heat exchanger 2Y. The experimental result shows that the temperature rise in adiabatic compression is 260 ° C., which is 13 times the air temperature 20 ° C. with a compression ratio of 8. Thermal power generation and airplanes that make space use costs 1 / 500,000, etc. by using the vessel 2Y to the utmost, aiming for space use with zero air resistance, and fuel consumption close to 1/1000 of the existing state-of-the-art science and technology Liquid oxygen 5K as a part of an infinite use case for the purpose of preventing the extinction of extreme weather and earthquake tsunami, preventing global warming and preventing the extinction of humankind. In the case of the drive containing the horizontal horizontal bladed water gravity turbine 11C power generation electrical product, the open / close valve 1Q that opens and closes by hydraulic pressure, screw rotation, etc. is used, and the open / close valve 1Q at the inlet and outlet of the compressed air heat exchanger 2Y is closed. If by liquid compression Oxygen / nitrogen injection nozzle 6M and oxygen injection nozzle 6L, such as oxygen nitrogen injection nozzle 6M and oxygen injection nozzle 6L aiming at a reduction work rate of 1/600 or less, and fuel injection nozzle 6X including liquid fuel injection combustion, challenge the pressure limit of the pressure vessel by ultra high pressure combustion The simple gas engine 89C, the simple air injection engine 89D, and the simple injection engine 89E are driven, the combustion gas 49 is injected into the rocket outer box 77B from the combustion gas injection nozzle 6Y, and the superheated steam 5H is supplied from the superheated steam rocket nozzle 6A. Injected into the rocket outer box 77B, sucked and injected forward air in the atmosphere and propelled into rocket injection injection in the vacuum. As with the case without 1Q, various opening injections of the combustion gas injection nozzle 6Y, the superheated steam rocket nozzle 6A, and the superheated steam injection nozzle 6Z can be selected, and the same fuel Superheated steam 5H production volume aim of 30 to 50 times the existing boiler, to the compressed air heat exchanger 2Y.

The vertical all blade steam turbine 11F in FIG. 9 uses a simple gas engine 89P that sucks and compresses air heated by the solar heater 21 and produces water for superheated steam by water jet cooling and compression. The amount of superheated steam 5H produced in the reactor 2Y is set as a target for 50 to 100 combustion heat exchange with an existing gas turbine compression ratio of 30 to 40 or more, and the amount of superheated steam 5H more than 50 times that of an existing boiler In the simple gas engine 89P, a vertical all-blade steam turbine 11F aiming at 100-fold rotation output of an existing steam turbine is used for full-rotation counter-rotating air compression and combustion gas 49 injection output drive, superheated steam 5H expansion speed + water speed production + In the process of acceleration driven by gravitational acceleration while the degree of vacuum is rising, and driving with 10 times speed Mach 10 etc. of existing steam turbine, injection mass increase or saturated steam liquefaction amount by water suction injection or water injection selection Aiming at a large target, with a minimum steam volume in the low-pressure part and an easy design of maximum water output, aiming to generate the same amount of superheated steam with 100 times the amount of heat generated, and using the same amount of fuel to generate power including the amount of superheated steam and unexpected power generation The production method is a cylindrical inner rotor blade group 60C / inner shaft device 60A and a cylindrical outer rotor blade group 60D / outer shaft device 60B. Separately fitting assembly part 9M screw assembly Screw fixing, press-fitting screw fixing, etc. After temporary assembly as in the main assembly, both ends can be precisely processed with a machine tool, ultra-high-speed rotation balance adjustment processing is enabled, the inner shaft device 60A The balance adjustment processing of the outer shaft device 60B is made good, and this assembly makes the ultra-high speed double reversal of the inner shaft device 60A and the outer shaft device 60B good. In the process of construction, the gravity power generation building 12 for producing the head is provided, the column pipe 12B is also used as the superheated steam pipe 5H, and the upper on-off valve 1Q is released in a manner similar to the description of FIG. The cylinder outer rotor blade group 60D and the cylinder inner rotor blade group 60C are driven in a reverse rotation, aiming at the minimum steam volume with the maximum water output of the final blade drive, and evacuating the condenser 2h in the same manner as the existing technology. In this way, a vertical all-blade steam turbine 11F that is converted into water and fed by the condensate pump 2i is used.

The simple air injection engine 89D shown in FIG. 10 has bearings 12C at the optimum positions at both ends of the cylindrical inner blade group 60C and inner shaft device 60A and the cylindrical outer blade group 60D and outer shaft device 60B. Joint assembly part 9M Screw assembly Screw fixing, press-fitting screw fixing, etc. After temporary assembly as in this assembly, it is possible to hold both ends with precision machining with machine tools, enable ultra-high speed rotation balance adjustment processing, inner shaft device 60A and inner compression blade 8q, the inner output blade 8s, the outer shaft device 60B, the outer compression blade 8r, and the outer output blade 8t are manufactured by adjusting the ultra-high-speed counter-rotating air of the inner shaft device 60A and the outer shaft device 60B. Compressed, superheated steam 5H production with the same amount of fuel As the superheated steam 5H production of the compressed air heat exchanger 2Y, aiming 100 times that of the existing boiler, fuel injection combustion + superheated to the super high pressure compressed air 28a 5H production simple air injection engine 89D drive, fuel injection combustion of mass increase of ultra high pressure compressed air 28a, rotation output generation + superheated steam 5H is injected into the production rocket outer box 77B, 10 times speed by air suction injection In the process of aiming at the air, air suction is also injected from the outer periphery, and the inlet is closed in the process of using the long compressed air heat exchanger 2Y including the drive of the horizontal full-blade water gravity turbine 11C power generation electric product, and the oxygen nitrogen injection nozzle Liquid oxygen 5H and liquid nitrogen 5L are injected from 6M, fuel is injected and burned from the fuel injection nozzle 6X, and the superheated steam 5H is produced as a mass production of superheated steam 5H combined with normal combustion. Mass production of production with 4 times combustion amount, liquid oxygen 5K and liquid nitrogen 5L are used for fuel combustion, compression work rate is 21/60000, 79/60000, etc. ultra high pressure combustion To comprise, aiming to 10 double speed or 1/100 fuel costs, the vessel or the ultra high-speed jet propulsion drive, to simplify the air injection engine 89D.

The simple injection engine 89E of FIG. 11 includes bearings 12C at the optimum positions at both ends of the cylindrical inner rotor blade group 60C and inner shaft device 60A and the cylindrical outer rotor blade group 60D and outer shaft device 60B. Assembly part 9M Screw assembly Screw fixing, press-fitting screw fixing, etc. After temporary assembly, both ends can be precisely processed by machine tools, ultra-high speed rotation balance adjustment processing is possible, and inner shaft device 60A and inner compression blade 8q As a manufacturing balance adjustment process for the inner output blade 8s, the outer shaft device 60B and the outer compression blade 8r, and the outer output blade 8t, ultra-high-speed counter-rotating air compression of the inner shaft device 60A and the outer shaft device 60B is achieved by assembling the main assembly. As the superheated steam 5H production of the compressed air heat exchanger 2Y, aiming 100 times the amount of superheated steam 5H production with the same fuel amount as the existing boiler, fuel injection combustion + superheated steam into the super high pressure compressed air 28a The H-type simple injection engine 89E is driven, fuel injection combustion is performed with an increase in the mass of the ultra-high pressure compressed air 28a, and rotational output generation + superheated steam 5H is injected into the production rocket outer box 77B. The inlet is closed in the process of using the long compressed air heat exchanger 2Y including the turbine 11C power generation electric product drive, and the liquid oxygen 5H and liquid nitrogen 5L are injected from the oxygen nitrogen injection nozzle 6M, and the fuel injection nozzle 6X. Fuel injection combustion, mass production of superheated steam 5H combined with normal combustion, mass production of 4 times combustion amount of superheated steam 5H normal combustion with theoretical air-fuel ratio combustion even with normal combustion, liquid oxygen 5K and liquid nitrogen 5L are fuel combustion Use it for aircraft, ships, etc. aiming at 10 times speed and 1/100 fuel cost with compression work rate of 21/60000 and 79/60000 etc. Rolling to drive and ultra-high-speed jet propulsion drive, to simplify injection engine 89E.

The simple gas engine car 89F in FIG. 12 is driven by the simple gas engine 89C, which is an improved invention of the existing micro gas turbine car. Experiments are required, but the production amount of superheated steam 5H is 50 times that of the existing boiler. As a simple gas engine 89C power generation aiming at 100 times rotation output of the existing gas turbine as steam 5H production and 100 times the same fuel amount as the existing thermal power generation, the simple gas engine 89C uses ordinary air compression fuel injection combustion and liquid Fuel injection combustion to compression injection of oxygen liquid nitrogen, respectively, superheated steam 5H is injected at 30MPa, etc., combustion gas 49 is sucked and injected respectively, and the same fuel amount as a 10 times rotational output of existing micro gas turbine, etc. The generator 1 is driven to store electricity in the storage battery 1A, and the storage battery driving wheel 4J is rotated to make a normal automobile operation. 0 aim to simplify gas engine automobile 89F, the operating profit margin by bus or taxi to the prevention preeminent world of global warming.

The simple gas engine ship 89G shown in FIG. 13 is an improved gas turbine ship driven by the simple gas engine 89C of the existing gas turbine ship. Although it requires experiments, the amount of superheated steam 5H produced is 50 times that of the existing boiler. The superheated steam 5H is produced by a simple gas engine 89C aiming at a 100-fold rotation output of the existing gas turbine, and the fuel is injected and burned into the normal air compression fuel injection combustion and the liquid oxygen liquid nitrogen compression injection to produce the superheated steam 5H, respectively. Etc., the respective combustion gases 49 are sucked and injected, the simple gas engine 89C is driven by the drive screw 7C, the exhaust gas is injected at a high speed to generate a propulsive force, and the air suction and injection is also performed on the outer periphery. Fuel amount Ultra-high-speed injection over and over approaching air-floating superheated steam levitation airplanes on a flat sea as a target for 100-times rotation output and 100-times injection propulsion output of existing gas turbines To proceed, by close to 10 times speed of the same amount of fuel existing vessels, the operating margins of the simple gas engine vessels 89G to outstanding world global warming.

The simple gas engine airplane 89H in FIG. 14 is a simple gas engine 89C-driven airplane that is an improvement invention of the existing turbo flop engine, and requires experimentation, but the amount of superheated steam 5H produced is 50 times the target of the existing boiler, As superheated steam 5H production, a simple gas engine 89C with 100 times rotational output and 100 times injection propulsion output of an existing gas turbine is used, and fuel injection combustion is performed for normal air compression fuel injection combustion and liquid oxygen liquid nitrogen compression injection, respectively. Superheated steam 5H is produced at an ultra-high speed injection of 30 MPa, etc., each combustion gas 49 is sucked and injected, the simple gas engine 89C is driven by the driving propeller 7A, and the exhaust gas is injected at an ultra-high speed to generate a propulsive force. Fuel amount As a target of 100 times rotation output and 100 times injection propulsion output of existing turbo flop engines, normal air-compressed fuel injection combustion is required when flying in the atmosphere. Increase the production and storage of steam 5H, and normally perform compression injection and fuel injection combustion of liquid oxygen liquid nitrogen fuel 30MPa, etc. from around the highest flight altitude, and make the combustion gas 49 into a suction injection linear expansion with 30MPa superheated steam 5H, simple gas By making the engine 89C drive straight exhaust injection, the space arrival cost is 1 / 500,000, etc., and the space arrival cost is about the same as the existing airplane, the operating profit rate of the simple gas engine airplane 89H is outstanding and the world's best global warming prevention To.

The simple air-injection engine ship 89I in FIG. 15 is a simple air-injection engine 89D-driven ship that is an improved invention of an existing gas turbine ship. Experiments are required, but the amount of superheated steam 5H production is 50 times that of an existing boiler, As a manufacture of blades + superheated steam 5H, a simple air injection engine 89D with 100 times rotation output and 100 times injection propulsion output of an existing gas turbine is used as fuel injection combustion for normal air compression fuel injection combustion and liquid oxygen liquid nitrogen compression injection In the process of injecting the superheated steam 5H into the rocket outer box 77B at a production of 30 MPa, etc., and injecting the air 28a forward to the bottom of the suction vessel, the air suction injection is again aimed at the 100 times injection propulsion output of the existing gas turbine ship. Then, after rotating and driving the simple air injection engine 89D with each combustion gas 49, the air in front of the exhaust injection is sucked and injected, and an existing gas turbine with the same fuel amount Easier by aiming at 10 times the speed of an existing ship with the same amount of fuel by propelling over a flat surface of the sea with combustion gas 49 levitation + superheated steam 5H levitation plane over and approaching ultra high speed injection, etc. The operating profit rate of the air jet engine ship 89I is the world's best global warming prevention.

The simple injection engine airplane 89J in FIG. 16 is a simple injection engine 89E driven airplane that is an improvement invention of the existing jet engine, and requires experimentation, but the amount of superheated steam 5H produced is 50 times the target of the existing boiler, or the entire blade + superheat For steam 5H production, a simple injection engine 89E with 100 times rotation output and 100 times injection propulsion output of an existing gas turbine is used, and fuel injection combustion is performed for normal air compression fuel injection combustion and liquid oxygen liquid nitrogen compression injection, respectively. Steam 5H is manufactured and injected into the rocket outer box 77B at 30MPa, etc., and the air 28a in the front is aimed at 100-times injection promotion of the existing jet aircraft by suction injection, and the exhaust gas is injected after rotating the simple injection engine 89E with each combustion gas 49 The front air is sucked and injected, and the same amount of fuel is used, aiming at 100 times the injection propulsion output of the existing jet, combustion gas 49 + superheated steam 5H super high speed Propellation propulsion, increase the production and storage of superheated steam 5H by normal air compression fuel injection combustion when flying in the atmosphere, usually compression and fuel injection combustion of liquid oxygen liquid nitrogen fuel 30MPa etc. from near the highest flight altitude, By making the combustion gas 49 into 30MP superheated steam 5H by suction injection linear expansion exhaust injection, the space arrival cost is 1 / 500,000, etc., and the space arrival cost is about the same as the existing aircraft, the operating profit rate of the simple injection engine airplane 89J Is the best global warming prevention in the world.

The rotary wing airplane 89K shown in FIG. 17 is a simple gas engine 89C driven airplane that is an improved invention of the existing helicopter, and requires experimentation, but the amount of superheated steam 5H produced is 50 times the target of the existing boiler, or the total moving blade + superheated steam 5H As a manufacture, a simple gas engine 89C with 100 times rotational output or 100 times injection propulsion output of an existing gas turbine is used, and fuel injection combustion is performed for normal air compression fuel injection combustion and compression injection of liquid oxygen liquid nitrogen, respectively, and superheated steam 5H Is produced at a high speed of 30 MPa, the respective combustion gases 49 are sucked and injected, the simple gas engine 89C is driven for linear expansion, the exhaust is injected at a high speed to generate a propulsive force, and the same fuel amount of the existing helicopter The rotary blade 7B is driven to rotate with the aim of 100 times rotation output, and the superheated steam 5H is produced and increased by normal air compression fuel injection combustion when flying in the atmosphere. Compression and fuel injection combustion of liquid oxygen liquid nitrogen fuel 30MPa etc. from near high flight altitude, the combustion gas 49 exhaust is made into suction injection linear expansion with 30MPa superheated steam 5H, simple gas engine 89C drive linear exhaust injection, By making the space arrival cost 1 / 500,000, etc., and making the space arrival cost comparable to that of existing airplanes, the operating profit rate of the rotary wing airplane 89K will be the world's best global warming prevention.

The rotary wing jet airplane 89L in FIG. 18 is a simple jet engine 89E driven airplane that is an improved invention of the existing helicopter and requires experimentation, but the amount of superheated steam 5H produced is 50 times the target of the existing boiler. As 5H production, a simple injection engine 89E with 100 times rotation output and 100 times injection propulsion output of an existing gas turbine is used, and fuel injection combustion is performed for normal air compression fuel injection combustion and compression injection of liquid oxygen liquid nitrogen, respectively, and superheated steam, respectively. 5H is manufactured and injected into the rocket outer box 77B at 30MPa, etc., and the upper air 28a and the combustion gas 49 are aimed at 100-times injection propulsion of the suction jet existing jet, and the simple injection engine 89E is rotated by each combustion gas 49. , After driving the rotor blade 7B, the air above the exhaust injection and the combustion gas 49 are sucked and injected, and the same fuel amount is aimed at 100 times injection propulsion output of the existing jet Combustion gas 49 + superheated steam 5H super-high speed injection propulsion, and superheated steam 5H is produced and increased by normal air compression fuel injection combustion when flying in the atmosphere, usually liquid oxygen liquid nitrogen fuel 30MPa from around the highest flight altitude etc. Compression and fuel injection combustion, the combustion gas 49 is suction-expanded linear expansion exhaust injection with 5MPa superheated steam 5H, the space arrival cost is 1 / 500,000, etc., and the space arrival cost is about the same as the existing airplane fuel cost Therefore, the operating profit rate of the rotary wing jet airplane 89L will be the world's best global warming prevention.

The oversized Osprey 89M in FIG. 19 is an airplane driven by the simple injection engine 89E, which is an improved invention of the existing Osprey, and requires experimentation, but the production amount of superheated steam 5H is aimed at 50 times that of the existing boiler, and all rotor blades + superheated steam 5H are produced. As a simple injection engine 89E with 100 times rotation output and 100 times injection propulsion output of an existing gas turbine, fuel injection combustion is performed for normal air compression fuel injection combustion and compression injection of liquid oxygen liquid nitrogen, and superheated steam 5H is respectively produced. Inject into the rocket outer box 77B at 30MPa, etc., and rotate the simple injection engine 89E with each combustion gas 49 linear injection with the aim of 100% injection propulsion of the upper air 28a and the combustion gas 49 of the existing jet aircraft. , After driving the propeller 7A, the air above the exhaust injection and the combustion gas 49 are sucked and injected, aiming at 100 times the injection propulsion output of the existing jet with the same fuel amount The combustion gas 49 + superheated steam 5H super-high speed injection propulsion, the superheated steam 5H is produced and increased by normal air compressed fuel injection combustion when flying in the atmosphere, and normally liquid oxygen liquid nitrogen fuel 30MPa from around the highest flight altitude Compression and fuel injection combustion, etc., the combustion gas 49 is made into a suction injection linear expansion exhaust injection with 30MPa superheated steam 5H, the space arrival cost is 1 / 500,000, etc., and the space arrival cost is about the same as the existing airplane fuel cost In this way, we will make the operating profit rate of the oversized Osprey 89M the best global warming prevention in the world.

The large Osprey 89N shown in Fig. 20 is a simple gas engine 89C-driven airplane that is an improved invention of the existing Osprey, and requires experimentation, but the amount of superheated steam 5H produced is 50 times the target of the existing boiler, and all blades + superheated steam 5H are produced. As a simple gas engine 89C with 100 times rotation output and 100 times injection propulsion output of an existing gas turbine, fuel injection combustion is performed for normal air compression fuel injection combustion and compression injection of liquid oxygen liquid nitrogen, and superheated steam 5H is respectively produced. Manufacturing Ultra-high-speed injection at 30 MPa, etc., sucking and injecting each combustion gas 49 to drive the simple gas engine 89C to drive linear expansion, generating ultra-high-speed injection of its exhaust to generate injection propulsion output, and the same fuel amount existing helicopter The propeller 7A is driven to rotate with the aim of 100 times rotation output, and the superheated steam 5H is produced and stored in the normal air compressed fuel injection combustion when flying in the atmosphere. Usually, compression and fuel injection combustion of liquid oxygen liquid nitrogen fuel 30MPa etc. from the vicinity of the highest flight altitude is performed, and the combustion gas 49 exhaust is made into suction injection linear expansion with 30MPa superheated steam 5H, and simple gas engine 89C drive linear exhaust injection is made. By making the space arrival cost 1 / 500,000, etc., and making the space arrival cost comparable to that of existing airplanes, the operating profit rate of the large Osprey 89N will be the world's best global warming prevention.

Since there is no brainwashing and long-term improvement of the existing state-of-the-art science and technology, in the calculation of internet search that can be understood by elementary school science without brainwashing, water injection speed Mach 3 production + gravity acceleration production in vacuum + head production When the horizontal full-blade water gravity turbine 11C power generation is compared with the existing pumped-storage power generation, the water speed Mach 10 production is 50 times faster than the existing pumped-power generation, and the same water mass is existing when the power generation is proportional to the water speed. Since the amount of power generation is 50 times that of pumped-storage power generation, and the amount of power generation is proportional to the square of the water speed, the same water mass is 2500 times the amount of power generation of existing pumped-power generation. If the new pumped storage power generation is infinitely increased, there is a possibility that the existing world thermal power generation and nuclear power generation will be abolished and the new pumped storage power generation will become all.

The existing state-of-the-art science and technology thermal power generation boilers are brainwashed and have not been improved for a long time, so the temperature rise of adiabatic compression takes advantage of the fact that the air temperature is 20 ° C and the compression ratio is 8 times 13 times 260 ° C. The air 28a heated at 21 and made as hot as possible is compressed and recovered by heat, and the entire blade is double-reversed by a simple gas engine 89P to obtain a compression ratio of 80 to 100, and the compressed air is used in an environment where the air temperature is 100 times. Because the heat exchanger 2Y fuel injection combustion superheated steam 5H is manufactured, the amount of superheated steam 5H produced with the same fuel combustion amount may be 100 times the target of existing boilers. There is a possibility that the superheated steam 5H is entirely produced by the gas engine 89P compressed air heat exchanger 2Y.

  Steam turbine power generation of the existing state-of-the-art science and technology thermal power generation is brainwashed and there is no improvement for a long time, so the pumping pump input of pumped storage power generation is proportional to the cube of the rotational speed, but the power generation amount is proportional to the water speed and superheated steam 5H speed In addition, the gravity acceleration in the vacuum is added to the superheated steam 5H expansion speed to make it a vertical type full-blade steam turbine 11F power generation with superheated steam 5H speed such as Mach 10 Is proportional to the superheated steam velocity, the same superheated steam heat amount is 10 times that of the existing steam turbine, and if the generated power is proportional to the square of the superheated steam velocity, the same superheated steam heat amount is 100 times that of the existing steam turbine. For this reason, there is a possibility that the steam turbine power generation in the existing world will be completely abolished, and all the vertical blade moving steam turbine 11F power generation will be performed.

In addition to the production of superheated steam 5H, the existing state-of-the-art science and technology gas turbine is equipped with half each of stationary blades and moving blades. In the turbine, the combustion gas is dammed with the stationary blades, and the rotation is repeated without changing the direction, and the rotational output and the injection propulsion output are set to 1/10 to 1/100. A simple gas engine 89C, a simple air injection engine 89D, a simple injection engine 89E, etc., that are double-reversed with the inner rotor blade group 60C, and the rotation output and injection propulsion output in the manufacture of the compressed air heat exchanger 2Y superheated steam 5H. To 100 times, add a horizontal full blade water gravity turbine 11C power generation electrical product drive, use solar heater 21 superheated steam 5H thermal production by-product liquid oxygen 5K + liquid nitrogen 5L, A simple gas engine 89C, a simple air injection engine 89D, and a simple injection engine 89E are driven at a volumetric compression work rate of 21/60000 + 79/60000 volumetric compression work rate. There is a possibility, the ship may approach 10 times the speed with the same fuel cost, the plane will be 1500,000 to reach the space, and as a prime use of space, take a day trip anywhere on earth to prevent global warming There is also the possibility of making a major revolution in the use of heat and cold.

0: Various energy storage cycle coalescence engine, 0: Various energy conservation cycle coalescence engine and coalescence method, 1: Generator, 1A: Storage battery, 1B: Pressure engine (oxygen pressure gear engine, oxygen pressure reciprocating engine, water pressure gear engine, 1C: alcohol, 1D: fuel injection pump, 1F: condensate pump, 1G: 1 to multistage heat pump (heat energy 1K: Liquid fuel control valve, 1L: Fuel heating pipe, 1Q: On-off valve, 1Y Air temperature and heat pump (various air compressors) multiple times compression 2C 2X2Y2Z multiple times heat recovery temperature 50 + cold heat 28a) : Multistage combustion chamber, 1b: fuel (liquid fuel + liquefiable gas fuel) 1b: fuel (liquid fuel + liquefiable gas fuel) 1b: fuel pipe (fuel injection temperature is at optimum temperature) 1c: Liquid fuel, 1d: Mercury, 1g: Gravity accelerating unit, 1h: Horizontal axis (axis that alternately rotates the outer shaft device and the inner shaft device) 1J: Fuel control valve, 1K: Liquid fuel Control valve, 2: Sunlight heater (collects sunlight in a straight line with a long lens and heats the high-temperature part forming intake air) 2a: Speeds up the natural phenomenon (in the air, there is almost zero leftovers in the nearby river 2a: Speeding up natural phenomena (by generating cold water 28a mixed with seawater for power generation, supplying seawater to the seabed with natural phenomena) Nitrogen, oxygen, CO2, etc. 2a: Speeding up natural phenomena (By ship, supplying nutrients such as nitrogen, oxygen and CO2 into the sea, aiming for the digestive capacity of microorganisms tens of thousands of times that of forests) Phytoplankton and seaweed 2b: Low water resistance (low-injection of air, combustion gas, superheated steam, etc. to the bottom of the ship to reduce water resistance) 2c: Thermal insulation, 2d: Long lens (Convex lens cross-section is linearly extended, and multiple lenses are used to aim at the shortest focal length lens width) 2e: Water surface, 2g: Specific material acceleration direction, 2h: Condenser, 2i: Condensate pump, 2A: Heat-resistant material, 2B: heat absorbing material, 2C: 1 to multiple-stage compression heat recovery device (heat energy is air temperature, heat pump is heat-recovered a plurality of times with a compression heat exchanger, and the rest is heated 50 + liquid cold 28a 2E: Specific critical substances (including alloys, platinum balls, gold balls, tungsten alloy powder sintered balls, silver balls, copper balls, tin balls, lead balls, zinc balls, aluminum balls, indium, cadmium, gallium, thallium, bismuth Specific gravity 2E: Specific critical substance (Manufacturing method reduces the impact energy as the diameter decreases. For example, molten steel is injected into the air to produce ultra-small diameter steel balls by high-speed collision crushing air cooling water cooling) 2E: Specific critical substance ( 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 sphere-Coated aluminum alloy sphere) 2F: Specific critical material raising device (gravity energy is increased and stored) 2H: Cold seawater mixer, 2V: Low temperature exhaust heat exchanger, 2W: Low temperature air heat exchanger, 2X: Air heat exchanger, 2Y: Compressed air heat exchanger (liquid air cold heat + heat production) 2Z: Specific critical material heat exchanger (used for temperature control of liquid metal below 500 degrees) 3a: Water repellent plating, 3i: Easy Multi-stage compressor, 3s: Simple compressor, 3t: Air turbine, 3u: Turbine, 3A: Water repellent coating, 3B: Water pressure reciprocating engine, 3D: Electricity + liquid air cold heat + superheated steam temperature heat supply equipment (with gravity power generation electricity Manufacturing of cold + hot and supplying liquid oxygen and liquid nitrogen Driving automobiles, ships and airplanes, and supplying with superheated steam Recovering methane injected into methane hydrate, etc. Electricity + cold + hot energy use prime) 3E: Specific material (mercury) 3E: Specific critical material (low melting point alloy liquid and stable high temperature liquid alloy) 3F: Oxygen pressure reciprocating engine 3G: Theoretical combustion gear engine, 3H: Reciprocating piston, 3J : Reciprocating combustion engine, 3K: External gear, 3L: Multistage combustion chamber, 3M: Steam pressure reciprocating engine, 3N: Steam pressure gear engine, 3P: Theoretical expansion engine (gas volume is 3Q: Theoretical expansion engine (best engine + aiming for the highest acceleration drive in vacuum) 3R: Theoretical gas turbine (the volume of gas is inversely proportional to the pressure) 3S: Theoretical steam turbine (Theoretical best steam turbine whose gas volume is inversely proportional to pressure) 3T: Theoretical gas compressor (Theoretical best gas compressor whose gas volume is inversely proportional to pressure) 3U: Theoretical turbine, 3V: Pump engine (Uses existing pumps in the engine) 3X: Compressor engine (Uses existing compressors in the engine) 3Y: Opposing meshing rotary engine (Gas volume is inversely proportional to pressure) 3Z: Oxygen pressure gear engine, 3a: Water repellent plating, 3b: Water repellent coating, 4C: Opposite synchronous gear, 4D: In-line rotating gear, 4F: Combustion gas reciprocation Engine, 4H: Heat absorption tube (collecting sunlight into the heat absorption tube in a straight line with the long lens 2d, heating the air temperature inside the tube to the maximum and raising the outside air temperature) 4J: Battery drive wheel, 4K: Theory Expansion engine vehicle, 4Q: Theoretical combustion chamber (theoretical air-fuel ratio combustion in the production of superheated steam, combustion chamber aiming at the existing 4-fold combustion amount and 20-fold pressure superheated steam injection), 4W: Theoretical compression chamber, 4Y: Theoretical combustion chamber (steam 4Z: Combustion gas gear engine, 4X: Turbine blade cross section (increase cross-sectional area to increase surface area) 4a: Liquid fuel pump, 4b: Liquid Oxygen pump, 4c: Water pump, 4d: Gear device, 4e: Roller, 4f: Rotation support part, 5: Air injection nozzle, 5a: High-pressure high-temperature combustion gas control valve, 5b: Compression intake air path, 5d: Combustion flow inner wall , 5e: Super High pressure oxygen, 5h: Rectification tower exhaust gas, 5h: Rectification tower exhaust gas pipe, 5A: Supply valve, 5B: Cooling fin, 5C: Exhaust chamber 5D: Exhaust valve 5E: Supply chamber 5F: Oxygen heating pipe, 5G: Steam heating pipe, 5G: High pressure high temperature water heating pipe, 5H: Superheated steam, 5H: High pressure high temperature superheated steam pipe, 5K: Liquid oxygen, 5K: Liquid oxygen chamber, 5L: Liquid nitrogen, 5L: Liquid nitrogen chamber, 5M: High pressure High temperature combustion chamber, 5M: High pressure high temperature combustion gas chamber, 5N: High pressure high temperature steam chamber, 5N: High pressure high temperature steam, 5P: Steam control valve, 5Q: Water control valve, 5R: Superheated steam control valve, 5S: Compressed air heating pipe 5T: liquid oxygen control valve, 6: final compression blade, 6A: superheated steam rocket nozzle, 6B: compressed air injection nozzle, 6E: specific material injection nozzle, 6F: water injection nozzle, 6G: outer box injection nozzle, 6H: Drain pipe, 6L: Oxygen Injection nozzle, 6M: Oxygen / nitrogen injection nozzle, 6W: Specific critical substance accelerator (liquid specific critical substance 3E pressure and specific gravity difference using specific gravity difference 3E or 2E mixed injection) 6X: Fuel injection nozzle, 6X: Afterburner (suction) 6Y: Combustion gas injection nozzle (cooling 28a combustion flow) 6Z: Superheated steam injection nozzle, 7A: Propeller, 7B: Rotation Wings, 7C: Screw, 7I: Simple gas engine vehicle, 7J: Simple gas engine ship, 7K: Simple gas engine airplane, 7L: Simple air injection engine ship, 7M: Simple injection engine airplane, 7N: Rotary wing airplane, 7O: Rotating blade injection plane, 7P: Oversized Osprey, 7Q: Large Osprey, 8b: Turbine blade (cycle number and specific material properties work speed and peripheral speed 8c: Turbine blade (a straight long turbine blade is provided on the outer surface of the cylinder, aiming for fully automatic machining and weight reduction of the inner and outer circumferences) 8d : Upper expansion blade group, 8e: Lower expansion blade group, 8f: Assembly turbine blade group, 8g: Upper compression blade group, 8h: Lower compression blade group, 8j: Assembly compression blade group, 8k: Inner compression blade, 8m : Outer compression blades, 8n: Inner output blades, 8p: Outer output blades, 8q: Inner compression blades (compressed blades with rotation and counter-rotating angles and curves according to rotational speed and peripheral speed) 8r: Outer compression Blades (compressed wings with rotational speed and circumferential speed, angle, curve and rotational radius opposed meshing rotation) 8s: Inner output blades (angle, curved line and rotational radius opposed meshing rotation according to rotational speed and circumferential speed) 8t: Outer output wing (rotation speed and 8A: Cylindrical turbine blade group (enables fully automatic machining and precision assembly as a horizontal cylindrical turbine blade group) 8B: Horizontal full blade dynamic gravity Turbine, 8C: Horizontal all blade ratio critical material gravity turbine, 8D: Horizontal total blade water gravity turbine, 8E: Horizontal total blade ratio critical material gravity turbine, 8V: Vertical all blade water gravity turbine, 8W: 竪Type all-blade specific gravity material gravity turbine, 8X: vertical all-blade water gravity turbine, 8Y: vertical type all-blade specific gravity gravity turbine, 9: wear-resistant annular assembly (only specific material flow path including 8c) 9b: Upper attracting and lower repulsive magnet, 9A: Cylindrical annular assembly (wear-resistant cylindrical annular assembly, 6 types of moving blade group, simple structure and few parts) Easy and fully automatic processing and assembly capacity 9A: Cylindrical annular assembly (inlet fixed outer blade 60E + outer annular blade 60G + outlet fixed outer blade 60J is fitted to form cylindrical turbine blade group 8A, inlet fixed inner blade 60F + inner annular blade 60H +) 9B: Repulsive permanent magnet, 9C: Suction permanent magnet, 9D: Compressed air part, 9E: Vacuum part, 9M: Fitting assembly part, 9Q : Vertical parallel plate (vertical parallel plate that guides the blast air to the storage stern) 10: Hull, 10A: Cabin, 10b: Control room, 10c: Control room, 10d: Guest room, 10e: Cargo room, 11: Vertical type all Rotor Steam Turbine 11FA: Vertical Type Fully Bladed Water Gravity Turbine, 11B: Vertical Type Fully Bladed Specific Material Gravity Turbine, 11C: Horizontal Type Fully Bladed Water Gravity Turbine, 11D: Gas Cooling Chamber, 11E: Horizontal Type Fully Dynamic Specific gravity gravity turbine, 11F: Vertical type full-blade steam turbine, 12: Gravity power generation building, 12A: Steel frame, 12B: Column tube, 12C: Bearing, 12D: Square flange, 12E: Flange, 16: Horizontal shaft plate (Disc that facilitates precision assembly) 16A: Horizontal axis, 21: Solar heater (mainly used with the intake air path provided in the heat absorption pipe 4H) 24: Combustion gas control valve, 24A: Compressed air control Valve, 25: superheated steam control valve, 25b: fuel control valve, 25c: fuel pipe, 28a: air, 28a: cold heat (compressed air 28a is compressed with a heat pump, heat of compressed air is heated 50 heat + liquid oxygen or liquid 28b: compressed air calorie, 28A: intake air passage, 28B: air passage inlet, 38: rotation guide, 38a: flight trunk, 38b: flight wing, 3 c: flying tail, 38d: vertical wing, 38e: leading edge of the wing, 38g: surface wing, 38h: floating boat, 38B: air suction jet ship (with 79S79T79Y79Z) 38C: water suction jet ship (with 79U79X) 38H: theory Screw ship, 38J: theoretical jet ship, 38T: theoretical jet airplane, 38U: theoretical propeller airplane, 39A: solar thermal gravity airplane, 39B: solar thermal gravity rotating airplane, 39C: solar thermal gravity helicopter, 39D: screw ship, 39G: solar thermal gravity flight Ship, 39H: Oxygen coalescence screw ship, 39J: Oxygen coalescence injection ship, 39K: Oxygen coalescence screw injection ship, 39L: Oxygen coalescence injection airplane, 39M: Oxygen coalescence propeller airplane, 39N: Oxygen coalescence propeller injection airplane, 39P: Oxygen coalescence Rotor plane, 39Q: Acid Combined screw ship, 39R: Oxygen combined injection ship, 39S: Oxygen combined screw injection ship, 39T: Oxygen combined injection airplane, 39U: Oxygen combined propeller airplane, 40A: Rudder, 49: Combustion gas, 50: Superheated steam, 50: Superheat Steam chamber, 50: Warmth (compressed air 28a is compressed with a heat pump, and is divided and stored into superheated steam 50 heat of compressed air calorie + compressed air 28a cold) 50A: steam, 50a: superheated steam injection pipe, 51: air extractor, 51: Confluence extractor (extractor for joining) 51A: Air extraction chamber, 52A: Low temperature water, 52B: Low temperature water pipe, 52C: Alcohol, 52C: Alcohol pipe, 52a: Deep ocean water, 52b: High temperature water, 52d : Thermal (change from 50) 52e: Cold (change from 28a) 55B: Transmission, 60A: Inner shaft device (turbine blade) Equipment 60B: Outer shaft device (equipment with turbine blades) 60C: Cylindrical inner blade group (Wear resistant cylindrical annular assembly fixed moving blade group, including fully automatic machining easy assembly) 60D: Cylindrical outer blade group (Ease of easy wear and assembly including wear-resistant cylindrical annular assembly fixed rotor blade group) 60E: Outer fixed outer blade (inlet blade for annular assembly fixing outer rotor blade group) 60F: Inlet fixed inner blade (inner motion) 60G: Outer annular blade (intermediate blade for annular assembly of outer blade group) 60H: Inner annular blade (intermediate blade for annular assembly of inner blade group) 60J: Outlet fixed outer blade (Outlet blade for annular assembly fixing outer rotor blade group) 60K: Outlet fixed inner blade (exit blade for annular assembly fixing inner rotor blade group) 60c: Inner rotor blade, 60d: Outer rotor blade, 60e: Outer inlet blade, 60f: Inner inlet blade, 60g: Outer intermediate blade, 6 0h: Inner intermediate blade, 60j: Inner outlet blade, 60k: Outer outlet blade, 76: Gear device (including magnetic friction power transmission device) 77B: Rocket outer box, 77C: Opposing meshing rotating machine outer box, 77F: Injection External box, 77G: Cylindrical rotating part, 77a: Turbine outer box, 77b: Compressor outer box, 80: Bearing (including magnetic bearing + air bearing) 80a: Thrust bearing (including magnetic bearing + air bearing) 80A: Fitting 80B: Fastener, 80Y: Liquid air suction water jet (high pressure high temperature combustion chamber 5M receiving high pressure high temperature steam chamber 5N, fuel injection combustion to 5M multiple times, 5N is heated multiple times from the inner periphery and inner periphery outer periphery 80Z: Liquid air suction water jet (receives high pressure high temperature combustion chamber 5M, high pressure high temperature steam chamber 5N, and injects and combusts multiple times to 5M, 5N inner circumference Heating and injecting multiple times from the inner and outer periphery, and fuel injection / combustion injection at a plurality of locations of air suction flow, air suction injection and water suction injection) 84: Opposing meshing rotary magnetic friction device (fixed portion) 84Y: Opposing meshing rotating gear device (same as in existing technology) 85: Opposing meshing rotating magnetic device (magnet gear height) 85Y: Opposite meshing rotating gear device (reciprocal reverse rotation with the existing horizontal shaft 1h gear) 88p: liquid oxygen production machine, 88q: simple gas engine, 88r: simple air injection engine, 88s: simple injection engine, 88A: oxygen combined air injection unit (rocket combustion + jet combustion + steam injection and combined injection) 88B: oxygen combined air injection unit (ultra-high pressure rocket combustion + di 88C: Theoretical air injection unit, 88M: Theoretical water injection unit, 88K: Oxygen combined water injection unit (rocket combustion + jet combustion + steam injection and combined injection) 88L: Oxygen combined water injection 89A: Liquid oxygen production machine, 89B: Simple multistage compressor, 89C: Simple gas engine, 89D: Simple air injection engine, 89E: Simple injection engine, 89F: Simple gas engine automobile, 89G: Simple gas engine ship, 89H: Simple gas engine airplane, 89I: Simple air injection engine ship, 89J: Simple injection engine airplane, 89K: Rotary wing airplane, 89L: Rotary wing injection airplane, 89M: Extra large Osprey, 89N: Large Osprey, 89P: Simple gas engine, 95a: Combustion gas reservoir, 95b: Compressed air reservoir, 95 : Superheated steam reservoir, 103: cold heat recovery unit,

Claims (193)

  Various energy storage cycle coalescence engines and coalescence methods comprising a simple gas engine (89P) + vertical all blade steam turbine (11F) power generation superheated steam pipe (5H) in a gravity power generation building (12).   Various energy storage cycle coalescence engine and coalescence method comprising a simple gas engine (89P) + vertical all blade steam turbine (11F) power generation superheated steam pipe (5H) in a column pipe (12B) of a gravity power generation building (12).   Various energy storage cycle coalescence engines and coalescence methods comprising a simple gas engine (89P) + vertical all blade steam turbine (11F) power generation superheated steam pipe (5H) on a column of a gravity power generation building (12).   Various energy storage cycle coalescence engines and coalescence methods comprising a simple gas engine (89P) + vertical all blade steam turbine (11F) power generation superheated steam pipe (5H) in a gravity power generation building (12).   Combined with various energy conservation cycles in which simple gas engine (89P) + vertical all blade steam turbine (11F) power generation superheated steam pipe (5H) is fixed to column pipe (12B) square flange (12D) of gravity power generation building (12) Organization and coalescence method.   Steel frame (12A) with simple gas engine (89P) + vertical all blade steam turbine (11F) power generation superheated steam pipe (5H) and gravity power generation building (12) column pipe (12B) square flange (12D) square Various energy storage cycle coalescence engines and coalescence methods fixed to   A simple gas engine (89P) + vertical all blade steam turbine (11F) power generation + superheated steam pipe (5H) gravity power generation building (12) column tube (12B) square flange (12D) square steel frame (12A ) Various energy storage cycle coalescence engines and coalescence methods bolted to   A simple gas engine (89P) + vertical all blade steam turbine (11F) power generation + superheated steam pipe (5H) gravity power generation building (12) column tube (12B) square flange (12D) square steel frame (12A ) Various energy storage cycle coalescence engines and coalescence methods fixed at the top and bottom.   A simple gas engine (89P) + vertical all blade steam turbine (11F) power generation + superheated steam pipe (5H) gravity power generation building (12) column tube (12B) square flange (12D) square steel frame (12A ) Various energy storage cycle coalescence engines and coalescence methods bolted up and down.   A simple gas engine (89P) + vertical all blade steam turbine (11F) power generation + superheated steam pipe (5H) gravity power generation building (12) column tube (12B) square flange (12D) square steel frame (12A ) Various energy conservation cycle coalescing engines and coalescence methods that increase the number of floors by bolting up and down.   A simple gas engine (89P) + vertical all blade steam turbine (11F) power generation + superheated steam pipe (5H) gravity power generation building (12) column tube (12B) square flange (12D) square steel frame (12A ) Various energy conservation cycle coalescing engines and coalescence methods that have upper and lower bolts to make the floor number one or more.   A simple gas engine (89P) + vertical all blade steam turbine (11F) power generation + superheated steam pipe (5H) gravity power generation building (12) column tube (12B) square flange (12D) square steel frame (12A ) Various energy conservation cycle coalescing engines and coalescence methods with upper and lower bolting to make the floor 20 floors or less.   A simple gas engine (89P) + vertical all blade steam turbine (11F) power generation + superheated steam pipe (5H) gravity power generation building (12) column tube (12B) square flange (12D) square steel frame (12A ) Various energy conservation cycle coalescing engines and coalescence methods with upper and lower bolts tightened to a floor number of 15 or less.   A simple gas engine (89P) + vertical all blade steam turbine (11F) power generation + superheated steam pipe (5H) gravity power generation building (12) column tube (12B) square flange (12D) square steel frame (12A ) Various energy conservation cycle coalescing engines and coalescence methods with upper and lower bolting to reduce the floor to 10 floors or less.   A simple gas engine (89P) + vertical all blade steam turbine (11F) power generation + superheated steam pipe (5H) gravity power generation building (12) column tube (12B) square flange (12D) square steel frame (12A ) Various energy conservation cycle coalescing engines and coalescence methods that have upper and lower bolts to make the floor 8 or less.   A simple gas engine (89P) + vertical all blade steam turbine (11F) power generation + superheated steam pipe (5H) gravity power generation building (12) column tube (12B) square flange (12D) square steel frame (12A ) Various energy conservation cycle coalescing engines and coalescing methods in which the number of floors is 6 or less by tightening the upper and lower bolts.   Simple energy engine (89P) + vertical all blade steam turbine (11F) power generation superheated steam pipe (5H) + various energy storage cycle coalescing engines that use superheated steam (5H) at the top of column pipe (12B) Merge method.   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation superheated steam pipe (5H) + column pipe (12B) raises superheated steam (5H) to the top Superheated steam (5H) expansion speed + vacuum Various energy conservation cycle coalescing engine and coalescence method for injecting with acceleration of gravitational acceleration while the temperature is rising.   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation superheated steam pipe (5H) + column pipe (12B) raises superheated steam (5H) to the top Superheated steam (5H) expansion speed + vacuum Various energy conservation cycle coalescing engine and coalescence method for injecting at gravitational acceleration acceleration Mach 3 or higher while the temperature is rising.   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation superheated steam pipe (5H) + column pipe (12B) raises superheated steam (5H) to the top Superheated steam (5H) expansion speed + vacuum Various energy conservation cycle coalescence engine and coalescence method for injecting at a gravitational acceleration acceleration Mach 3 or less while the temperature is rising.   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation superheated steam pipe (5H) + column pipe (12B) raises superheated steam (5H) to the top Superheated steam (5H) expansion speed + vacuum Various energy conservation cycle coalescence engines and coalescence methods for injection at a gravitational acceleration acceleration Mach of 1 or higher.   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation superheated steam pipe (5H) + column pipe (12B) raises superheated steam (5H) to the top Superheated steam (5H) expansion speed + vacuum Various energy conservation cycle coalescence engines and coalescence methods for injecting at a gravitational acceleration acceleration Mach of 1 or less.   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation superheated steam pipe (5H) + column pipe (12B) raises superheated steam (5H) to the top Superheated steam (5H) expansion speed + vacuum Various energy conservation cycle coalescence engine and coalescence method for accelerating gravitational acceleration in a jet vacuum by acceleration of gravitational acceleration while the temperature is rising.   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation superheated steam pipe (5H) + column pipe (12B) raises superheated steam (5H) to the top Superheated steam (5H) expansion speed + vacuum Various energy storage cycle coalescence engines and coalescence methods for accelerating gravitational acceleration in a jet vacuum with gravitational acceleration acceleration Mach 3 or higher.   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation superheated steam pipe (5H) + column pipe (12B) raises superheated steam (5H) to the top Superheated steam (5H) expansion speed + vacuum Various energy storage cycle coalescence engines and coalescence methods for accelerating gravitational acceleration in an injection vacuum at a gravitational acceleration acceleration Mach 3 or less.   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation superheated steam pipe (5H) + column pipe (12B) raises superheated steam (5H) to the top Superheated steam (5H) expansion speed + vacuum Gravity acceleration acceleration Mach 1 or higher, and various energy conservation cycle coalescence engine and coalescence method for accelerating gravity acceleration in injection vacuum.   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation superheated steam pipe (5H) + column pipe (12B) raises superheated steam (5H) to the top Superheated steam (5H) expansion speed + vacuum Gravity acceleration acceleration while increasing the temperature Mach 1 or less, various energy storage cycle coalescence engine and coalescence method for accelerating gravitational acceleration in injection vacuum.   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation superheated steam pipe (5H) + column pipe (12B) raises superheated steam (5H) to the top Superheated steam (5H) expansion speed + vacuum Various energy conservation cycle coalescence engines and coalescence methods for injecting into a vacuum gravity acceleration acceleration cylinder outer rotor blade group (60D) and cylinder inner rotor blade group (60C) in a vacuum with acceleration of gravitational acceleration while the temperature is rising.   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation superheated steam pipe (5H) + column pipe (12B) raises superheated steam (5H) to the top Superheated steam (5H) expansion speed + vacuum Various energy conservation cycle coalescence engine and coalescence method for injecting gravity acceleration acceleration cylinder outer rotor blade group (60D) and cylinder inner rotor blade group (60C) in injection vacuum with gravitational acceleration acceleration Mach 3 or higher.   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation superheated steam pipe (5H) + column pipe (12B) raises superheated steam (5H) to the top Superheated steam (5H) expansion speed + vacuum Various energy storage cycle coalescence engine and coalescence method for injecting gravity acceleration acceleration cylinder outer rotor blade group (60D) and cylinder inner rotor blade group (60C) in jet vacuum at gravitational acceleration acceleration Mach 3 or less.   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation superheated steam pipe (5H) + column pipe (12B) raises superheated steam (5H) to the top Superheated steam (5H) expansion speed + vacuum Various energy storage cycle coalescence engines and coalescence methods for injecting gravity acceleration acceleration cylinder outer moving blade group (60D) and cylinder inner moving blade group (60C) in jet vacuum at gravitational acceleration acceleration Mach 1 or higher.   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation superheated steam pipe (5H) + column pipe (12B) raises superheated steam (5H) to the top Superheated steam (5H) expansion speed + vacuum Various energy conservation cycle coalescence engines and coalescence methods for injecting gravity acceleration acceleration Mach 1 or less during gravity rise into gravity vacuum acceleration cylinder outer rotor blade group (60D) and cylinder inner rotor blade group (60C) in vacuum.   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation superheated steam pipe (5H) + column pipe (12B) raises superheated steam (5H) to the top Superheated steam (5H) expansion speed + vacuum Various energy storage cycle coalescence engines and coalescence methods for driving the jets to the cylinder outer rotor blade group (60D) and the cylinder inner rotor blade group (60C) in a jet vacuum by acceleration of gravitational acceleration while increasing the temperature.   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation superheated steam pipe (5H) + column pipe (12B) raises superheated steam (5H) to the top Superheated steam (5H) expansion speed + vacuum Accelerating Gravity Acceleration Mach 3 or higher during injection, Gravity Acceleration Acceleration in Vacuum Vacuum Outer Cylindrical Blade Group (60D), Cylindrical Inner Blade Group (60C) Method.   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation superheated steam pipe (5H) + column pipe (12B) raises superheated steam (5H) to the top Superheated steam (5H) expansion speed + vacuum Accelerating Gravity Acceleration Mach 3 or less, and accelerating Gravity Acceleration Cylinder Outer Blade Group (60D) and Cylindrical Inner Blade Group (60C) Method.   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation superheated steam pipe (5H) + column pipe (12B) raises superheated steam (5H) to the top Superheated steam (5H) expansion speed + vacuum Accelerating Gravity Acceleration Mach 1 or higher during injection, Gravity Acceleration Acceleration in Vacuum Vacuum Outer Cylindrical Blade Group (60D), Cylindrical Inner Blade Group (60C) Method.   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation superheated steam pipe (5H) + column pipe (12B) raises superheated steam (5H) to the top Superheated steam (5H) expansion speed + vacuum Accelerating Gravity Acceleration Mach 1 or less during injection, Gravity Acceleration Acceleration in Vacuum Vacuum Outer Cylinder Outer Blade Group (60D) and Cylindrical Inner Blade Group (60C) Method.   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation superheated steam pipe (5H) + column pipe (12B) raises superheated steam (5H) to the top Superheated steam (5H) expansion speed + vacuum Accelerating Gravity Acceleration with Increasing Degree of Gravity Acceleration in Gravity Acceleration in Cylindrical Outer Blade Group (60D) and Cylindrical Inner Blade Group (60C) Method.   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation superheated steam pipe (5H) + column pipe (12B) raises superheated steam (5H) to the top Superheated steam (5H) expansion speed + vacuum Accelerating Gravity Acceleration Mach 3 or higher during spraying Gravity Acceleration Acceleration in Vacuum Vacuum Outer Cylindrical Blade Group (60D) Cylindrical Inner Blade Group (60C) Organization and coalescence method.   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation superheated steam pipe (5H) + column pipe (12B) raises superheated steam (5H) to the top Superheated steam (5H) expansion speed + vacuum Combined with various energy conservation cycles to generate electricity by rotating the jets in reverse to the cylinder outer rotor blade group (60D) and the cylinder inner rotor blade group (60C) in the jet vacuum at gravitational acceleration acceleration Mach 3 or less. Organization and coalescence method.   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation superheated steam pipe (5H) + column pipe (12B) raises superheated steam (5H) to the top Superheated steam (5H) expansion speed + vacuum Combined with various energy conservation cycles to generate electricity by rotating the jets in the cylinder outer rotor blade group (60C) and the cylinder inner rotor blade group (60C) in a jet vacuum at a gravitational acceleration acceleration Mach of 1 or more while increasing the temperature. Organization and coalescence method.   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation superheated steam pipe (5H) + column pipe (12B) raises superheated steam (5H) to the top Superheated steam (5H) expansion speed + vacuum Combined with various energy storage cycles to generate power by driving the jets to reverse each other in the cylinder outer rotor blade group (60D) and the cylinder inner rotor blade group (60C). Organization and coalescence method.   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation outer shaft device (60B) / cylindrical outer blade group (60D) and inner shaft device (60A) / cylindrical inner blade group (60C) Various energy storage cycle coalescence engines and coalescence methods equipped with bearings (12C) at both ends of each.   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation outer shaft device (60B) / cylindrical outer blade group (60D) and inner shaft device (60A) / cylindrical inner blade group (60C) Bearings (12C) are provided at both ends of each of the various energy storage cycle coalescing engines and coalescence methods capable of supporting both ends with a temporary assembly machine tool.   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation outer shaft device (60B) / cylindrical outer blade group (60D) and inner shaft device (60A) / cylindrical inner blade group (60C) Bearings (12C) are provided at both ends of each of the various energy storage cycle coalescing engines and coalescing methods, wherein both ends are supported and ultra-high-speed balance adjustment processing is performed separately with a temporary assembly machine tool.   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation outer shaft device (60B) / cylindrical outer blade group (60D) and inner shaft device (60A) / cylindrical inner blade group (60C) Bearings (12C) are provided at both ends of each of the various energy storage cycle coalescence engines and coalescence methods, which are separately supported at both ends by a temporary assembly machine tool and ultra-high-speed balance adjustment ultra-precision machining.   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation outer shaft device (60B) / cylindrical outer blade group (60D) and inner shaft device (60A) / cylindrical inner blade group (60C) Bearings (12C) are provided at both ends of each of the various energy storage cycle coalescence engines and coalescence methods that are separately assembled in a temporary assembly machine tool and supported at both ends by super-high-speed balance adjustment and ultra-precision machining.   Simple gas engine (89P) + vertical all-blade steam turbine (11F) power generation electric drive liquid oxygen production machine (89A) outer shaft device (60B) and outer compression blade (8r) and inner shaft device (60A) and inner Various energy storage cycle coalescence engines and coalescence methods provided with bearings (12C) at both ends of the compression blades (8q).   Simple gas engine (89P) + vertical all-blade steam turbine (11F) power generation electric drive liquid oxygen production machine (89A) outer shaft device (60B) and outer compression blade (8r) and inner shaft device (60A) and inner Various energy storage cycle merging engines and merging methods in which bearings (12C) are provided at both ends of each of the compressor blades (8q), and both ends can be supported by a temporary assembly machine tool.   Simple gas engine (89P) + vertical all-blade steam turbine (11F) power generation electric drive liquid oxygen production machine (89A) outer shaft device (60B) and outer compression blade (8r) and inner shaft device (60A) and inner Various energy storage cycle coalescence engines and coalescence methods, in which bearings (12C) are provided at both ends of each of the compression blades (8q), and both ends are supported and ultra-high speed balance adjustment processing is performed by a temporary assembly machine tool.   Simple gas engine (89P) + vertical all-blade steam turbine (11F) power generation electric drive liquid oxygen production machine (89A) outer shaft device (60B) and outer compression blade (8r) and inner shaft device (60A) and inner Various energy storage cycle merging engines and merging methods in which bearings (12C) are provided at both ends of each of the compressor blades (8q), and both ends are supported and ultra-high-speed balance adjustment is performed with a temporary assembly machine tool.   Simple gas engine (89P) + vertical all-blade steam turbine (11F) power generation electric drive liquid oxygen production machine (89A) outer shaft device (60B) and outer compression blade (8r) and inner shaft device (60A) and inner Various energy storage cycle coalescence engines and coalescence methods that are equipped with bearings (12C) at both ends of each of the compression blades (8q), and that are assembled separately after ultra-high-precision balance adjustment and ultra-precision machining with both ends supported by a temporary assembly machine tool.   Simple gas engine (89P) + vertical all-blade steam turbine (11F) Electric generator-driven liquid oxygen production machine (89A) Outer shaft device (60B) and outer output blade (8t) and inner shaft device (60A) and inner Various energy storage cycle coalescence engines and coalescence methods provided with bearings (12C) at both ends of each of the output blades (8s).   Simple gas engine (89P) + vertical all-blade steam turbine (11F) Electric generator-driven liquid oxygen production machine (89A) Outer shaft device (60B) and outer output blade (8t) and inner shaft device (60A) and inner Bearings (12C) are provided at both ends of each of the output blades (8s), and various energy storage cycle merging engines and merging methods that enable both ends to be supported by a temporary assembly machine tool.   Simple gas engine (89P) + vertical all-blade steam turbine (11F) Electric generator-driven liquid oxygen production machine (89A) Outer shaft device (60B) and outer output blade (8t) and inner shaft device (60A) and inner Various energy storage cycle coalescence engines and coalescence methods, in which bearings (12C) are provided at both ends of each of the output blades (8s), and both ends are supported and ultra-high speed balance adjustment processing is performed by a temporary assembly machine tool.   Simple gas engine (89P) + vertical all-blade steam turbine (11F) Electric generator-driven liquid oxygen production machine (89A) Outer shaft device (60B) and outer output blade (8t) and inner shaft device (60A) and inner Bearings (12C) at both ends of each of the output wings (8s), and various energy storage cycle coalescence engines and coalescence methods, each of which is separately supported at both ends by a temporary assembly machine tool and ultra-high-speed balance adjustment ultra-precision machining.   Simple gas engine (89P) + vertical all-blade steam turbine (11F) Electric generator-driven liquid oxygen production machine (89A) Outer shaft device (60B) and outer output blade (8t) and inner shaft device (60A) and inner Bearings (12C) are provided at both ends of each of the output blades (8s), and various energy storage cycle coalescence engines and coalescence methods are separately assembled by temporary assembly machine tools after both ends are supported and ultra-high-speed balance adjustment is performed after ultra-precision machining.   Simple gas compressor equipped with bearings (12C) at both ends of a simple multistage compressor (89B) outer shaft device (60B) and outer compressor blade (8r) and inner shaft device (60A) and inner compressor blade (8q) that are connected and driven in various ways. Various energy storage cycle coalescence engine and coalescence method including engine (89P) + vertical all blade steam turbine (11F) power generation (11C) power generation electric product drive.   Bearings (12C) are provided separately at both ends of each of the simple multistage compressors (89B), outer shaft devices (60B) and outer compressor blades (8r), and inner shaft devices (60A) and inner compressor blades (8q) that are connected and driven in various ways. Simple gas engine (89P) + vertical all-blade steam turbine (11F) power generation (11C) power generation electric product drive and combined engine and combination method capable of supporting both ends with a temporary assembly machine tool .   Bearings (12C) are provided separately at both ends of each of the simple multistage compressors (89B), outer shaft devices (60B) and outer compressor blades (8r), and inner shaft devices (60A) and inner compressor blades (8q) that are connected and driven in various ways. Various energy storage cycle coalescence engine and coalescence method including horizontal full-blade hydrogravity turbine (11C) power generation electric product drive by both-end support processing ultra-high-speed balance adjustment processing with a temporary assembly machine tool.   Bearings (12C) are provided separately at both ends of each of the simple multistage compressors (89B), outer shaft devices (60B) and outer compressor blades (8r), and inner shaft devices (60A) and inner compressor blades (8q) that are connected and driven in various ways. Various energy storage cycle merging engines and merging methods that include both ends support processing ultra-high-speed balance adjustment ultra-precise processing with a temporary assembly machine tool, and a horizontal full-blade hydrogravity turbine (11C) generator electric product drive.   Bearings (12C) are provided separately at both ends of each of the simple multistage compressors (89B), outer shaft devices (60B) and outer compressor blades (8r), and inner shaft devices (60A) and inner compressor blades (8q) that are connected and driven in various ways. Various energy storage cycle merging engines and merging methods that include both full-width blade hydrogravity turbine (11C) power generation electric product drive after being assembled after ultra-high-speed balance adjustment and ultra-precision machining with temporary assembly machine tools.   Simple gas engine (89P) + vertical all-blade steam turbine (11F) power generation (11C) simple gas engine (89C) including power generation electric product drive outer shaft device (60B) and outer compression blade (8r) and inner shaft Various energy storage cycle merging engines and merging methods provided with bearings (12C) at both ends of the device (60A) and the inner compression blade (8q).   Simple gas engine (89P) + vertical all-blade steam turbine (11F) power generation (11C) simple gas engine (89C) including power generation electric product drive outer shaft device (60B) and outer compression blade (8r) and inner shaft Bearings (12C) are provided at both ends of each of the apparatus (60A) and the inner compression blade (8q), and various energy storage cycle coalescence engines and coalescence methods capable of supporting both ends separately with a temporary assembly machine tool.   Simple gas engine (89P) + vertical all-blade steam turbine (11F) power generation (11C) simple gas engine (89C) including power generation electric product drive outer shaft device (60B) and outer compression blade (8r) and inner shaft Bearings (12C) are provided at both ends of each of the apparatus (60A) and the inner compression blade (8q), and various energy storage cycle coalescence engines and coalescence methods are separately processed by a temporary assembly machine tool to perform both-end support processing and ultrahigh-speed balance processing.   Simple gas engine (89P) + vertical all-blade steam turbine (11F) power generation (11C) simple gas engine (89C) including power generation electric product drive outer shaft device (60B) and outer compression blade (8r) and inner shaft Bearings (12C) are provided at both ends of each of the apparatus (60A) and the inner compression blade (8q), and various energy storage cycle merging engines and merging methods are used to perform both-end support machining and ultra-high-speed balance adjustment ultra-precision machining with temporary assembly machine tools.   Simple gas engine (89P) + vertical all-blade steam turbine (11F) power generation (11C) simple gas engine (89C) including power generation electric product drive outer shaft device (60B) and outer compression blade (8r) and inner shaft Bearings (12C) at both ends of each of the apparatus (60A) and the inner compression blade (8q), each having a bearing (12C) separately, supporting both ends with a temporary assembly machine tool. Merge method.   Simple gas engine (89P) + vertical all-blade steam turbine (11F) power generation (11C) simple gas engine (89C) including power generation electric product drive outer shaft device (60B) and outer output blade (8t) and inner shaft Various energy storage cycle merging engines and merging methods provided with bearings (12C) at both ends of the device (60A) and the inner output blade (8s).   Simple gas engine (89P) + vertical all-blade steam turbine (11F) power generation (11C) simple gas engine (89C) including power generation electric product drive outer shaft device (60B) and outer output blade (8t) and inner shaft Bearings (12C) are provided at both ends of each of the apparatus (60A) and the inner output blade (8s), and various energy storage cycle coalescence engines and coalescence methods that enable both ends to be supported by a temporary assembly machine tool.   Simple gas engine (89P) + vertical all-blade steam turbine (11F) power generation (11C) simple gas engine (89C) including power generation electric product drive outer shaft device (60B) and outer output blade (8t) and inner shaft Bearings (12C) are provided at both ends of each of the apparatus (60A) and the inner output blade (8s), and various energy storage cycle coalescence engines and coalescence methods are separately processed at both ends by a temporary assembly machine tool to perform ultra-high speed balance adjustment processing.   Simple gas engine (89P) + vertical all-blade steam turbine (11F) power generation (11C) simple gas engine (89C) including power generation electric product drive outer shaft device (60B) and outer output blade (8t) and inner shaft Bearings (12C) are provided at both ends of each of the apparatus (60A) and the inner output blade (8s), and various energy storage cycle merging engines and merging methods are used to perform both-end support machining and ultra-high-speed balance adjustment ultra-precision machining with a temporary assembly machine tool.   Simple gas engine (89P) + vertical all-blade steam turbine (11F) power generation (11C) simple gas engine (89C) including power generation electric product drive outer shaft device (60B) and outer output blade (8t) and inner shaft Bearings (12C) at both ends of each of the apparatus (60A) and the inner output blade (8s), each having a bearing (12C) separately, supporting both ends with a temporary assembly machine tool, various high-speed balance adjustments, various energy storage cycle coalescing engines to be assembled after ultra-precision machining and Merge method.   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation (11C) simple air injection engine (89D) including power generation electric product drive outer shaft device (60B) and outer compression blade (8r) and inner Various energy storage cycle coalescence engines and coalescence methods comprising bearings (12C) at both ends of the shaft device (60A) and the inner compression blades (8q).   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation (11C) simple air injection engine (89D) including power generation electric product drive outer shaft device (60B) and outer compression blade (8r) and inner Various energy storage cycle coalescence engines and coalescence methods, in which both ends of the shaft device (60A) and the inner compression blades (8q) are respectively provided with bearings (12C) and can be both end supported by a temporary assembly machine tool.   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation (11C) simple air injection engine (89D) including power generation electric product drive outer shaft device (60B) and outer compression blade (8r) and inner Various energy storage cycle coalescence engines and coalescence methods, in which bearings (12C) are provided at both ends of each of the shaft device (60A) and the inner compression blades (8q), and both ends are supported by a temporary assembly machine tool and ultra-high speed balance adjustment processing is performed.   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation (11C) simple air injection engine (89D) including power generation electric product drive outer shaft device (60B) and outer compression blade (8r) and inner The shaft device (60A) and the inner compression blade (8q) have bearings (12C) at both ends, respectively, and are supported on both ends by a temporary assembly machine tool. .   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation (11C) simple air injection engine (89D) including power generation electric product drive outer shaft device (60B) and outer compression blade (8r) and inner Bearings (12C) are provided at both ends of each of the shaft device (60A) and the inner compression blade (8q). Both ends are supported separately by a temporary assembly machine tool. Ultra-high-speed balance adjustment. And coalescing method.   Simple gas engine (89P) + vertical all-blade steam turbine (11F) power generation (11C) simple air injection engine (89D) including power generation electric product drive outer shaft device (60B) and outer output blade (8t) and inner Various energy storage cycle merging engines and merging methods provided with bearings (12C) at both ends of the shaft device (60A) and the inner output blade (8s).   Simple gas engine (89P) + vertical all-blade steam turbine (11F) power generation (11C) simple air injection engine (89D) including power generation electric product drive outer shaft device (60B) and outer output blade (8t) and inner Various energy storage cycle merging engines and merging methods in which bearings (12C) are provided at both ends of each of the shaft device (60A) and the inner output blade (8s), and both ends can be supported by a temporary assembly machine tool.   Simple gas engine (89P) + vertical all-blade steam turbine (11F) power generation (11C) simple air injection engine (89D) including power generation electric product drive outer shaft device (60B) and outer output blade (8t) and inner Various energy storage cycle coalescence engines and coalescence methods, including bearings (12C) at both ends of each of the shaft device (60A) and the inner output blade (8s), each of which is separately supported at both ends by a temporary assembly machine tool and processed at a high speed balance.   Simple gas engine (89P) + vertical all-blade steam turbine (11F) power generation (11C) simple air injection engine (89D) including power generation electric product drive outer shaft device (60B) and outer output blade (8t) and inner The shaft device (60A) and the inner output blade (8s) have bearings (12C) at both ends, and support each end with a temporary assembly machine tool. .   Simple gas engine (89P) + vertical all-blade steam turbine (11F) power generation (11C) simple air injection engine (89D) including power generation electric product drive outer shaft device (60B) and outer output blade (8t) and inner Bearings (12C) are provided at both ends of the shaft device (60A) and the inner output blade (8s), respectively. Both ends are supported by a temporary assembly machine tool. Ultra-high-speed balance adjustment. And coalescing method.   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation (11C) simple injection engine (89E) including power generation electric product drive outer shaft device (60B) and outer compression blade (8r) and inner shaft Various energy storage cycle merging engines and merging methods provided with bearings (12C) at both ends of the device (60A) and the inner compression blade (8q).   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation (11C) simple injection engine (89E) including power generation electric product drive outer shaft device (60B) and outer compression blade (8r) and inner shaft Bearings (12C) are provided at both ends of each of the apparatus (60A) and the inner compression blade (8q), and various energy storage cycle coalescence engines and coalescence methods capable of supporting both ends separately with a temporary assembly machine tool.   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation (11C) simple injection engine (89E) including power generation electric product drive outer shaft device (60B) and outer compression blade (8r) and inner shaft Bearings (12C) are provided at both ends of each of the apparatus (60A) and the inner compression blade (8q), and various energy storage cycle coalescence engines and coalescence methods are separately processed by a temporary assembly machine tool to perform both-end support processing and ultrahigh-speed balance adjustment processing.   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation (11C) simple injection engine (89E) including power generation electric product drive outer shaft device (60B) and outer compression blade (8r) and inner shaft Bearings (12C) are provided at both ends of each of the apparatus (60A) and the inner compression blade (8q), and various energy storage cycle merging engines and merging methods are used to perform both-end support machining and ultra-high-speed balance adjustment ultra-precision machining with temporary assembly machine tools.   Simple gas engine (89P) + vertical all blade steam turbine (11F) power generation (11C) simple injection engine (89E) including power generation electric product drive outer shaft device (60B) and outer compression blade (8r) and inner shaft Bearings (12C) at both ends of each of the apparatus (60A) and the inner compression blade (8q), each having a bearing (12C) separately, supporting both ends with a temporary assembly machine tool. Merge method.   Simple gas engine (89P) + vertical all-blade steam turbine (11F) power generation (11C) simple injection engine (89E) including power generation electric product drive outer shaft device (60B) and outer output blade (8t) and inner shaft Various energy storage cycle merging engines and merging methods provided with bearings (12C) at both ends of the device (60A) and the inner output blade (8s).   Simple gas engine (89P) + vertical all-blade steam turbine (11F) power generation (11C) simple injection engine (89E) including power generation electric product drive outer shaft device (60B) and outer output blade (8t) and inner shaft Bearings (12C) are provided at both ends of each of the apparatus (60A) and the inner output blade (8s), and various energy storage cycle coalescence engines and coalescence methods that enable both ends to be supported by a temporary assembly machine tool.   Simple gas engine (89P) + vertical all-blade steam turbine (11F) power generation (11C) simple injection engine (89E) including power generation electric product drive outer shaft device (60B) and outer output blade (8t) and inner shaft Bearings (12C) are provided at both ends of each of the apparatus (60A) and the inner output blade (8s), and various energy storage cycle coalescence engines and coalescence methods are separately processed at both ends by a temporary assembly machine tool to perform ultra-high speed balance adjustment processing.   Simple gas engine (89P) + vertical all-blade steam turbine (11F) power generation (11C) simple injection engine (89E) including power generation electric product drive outer shaft device (60B) and outer output blade (8t) and inner shaft Bearings (12C) are provided at both ends of each of the apparatus (60A) and the inner output blade (8s), and various energy storage cycle merging engines and merging methods are used to perform both-end support machining and ultra-high-speed balance adjustment ultra-precision machining with a temporary assembly machine tool.   Simple gas engine (89P) + vertical all-blade steam turbine (11F) power generation (11C) simple injection engine (89E) including power generation electric product drive outer shaft device (60B) and outer output blade (8t) and inner shaft Bearings (12C) at both ends of each of the apparatus (60A) and the inner output blade (8s), each having a bearing (12C) separately, supporting both ends with a temporary assembly machine tool, various high-speed balance adjustments, various energy storage cycle coalescing engines to be assembled after ultra-precision machining and Merge method.   A simple gas engine (89C) in which the existing stationary blades are completely abolished and the rotor blades are double-reversed is equipped with a compressed air heat exchanger (2Y), and the production amount of superheated steam (5H) is the same as that of an existing boiler. Various energy storage cycle coalescence engine and coalescence method including horizontal full-blade hydrogravity turbine (11C) power generation electric product drive with rotation output and injection propulsion output over 20 times that of existing gas turbine.   A simple gas engine (89C) in which the existing stationary blades are completely abolished and the rotor blades are double-reversed is equipped with a compressed air heat exchanger (2Y), and the production amount of superheated steam (5H) is the same as that of the existing boiler. Various energy storage cycle coalescence engine and coalescence method including horizontal full-blade hydrogravity turbine (11C) power generation electrical product drive with rotational output and injection propulsion output over 40 times that of existing gas turbines.   A simple gas engine (89C), which completely abolishes existing stationary blades and double-rotates all moving blades, is equipped with a compressed air heat exchanger (2Y) and produces the same amount of superheated steam (5H) with the same fuel amount. Various energy storage cycle coalescence engine and coalescence method including horizontal full-blade hydrogravity turbine (11C) power generation electrical product drive with rotation output and injection propulsion output at least 16 times that of existing gas turbine.   A simple gas engine (89C) in which the existing stationary blades are completely abolished and the rotor blades are double-reversed is equipped with a compressed air heat exchanger (2Y), and the production amount of superheated steam (5H) is the same as that of the existing boiler. Various energy storage cycle coalescence engine and coalescence method including horizontal full-blade hydrogravity turbine (11C) power generation electric product drive with rotational output over 80 times that of existing gas turbine.   A simple gas engine (89C), which completely abolishes existing stationary blades and double-rotates all moving blades, is equipped with a compressed air heat exchanger (2Y) and produces the same amount of superheated steam (5H) with the same fuel amount. Various energy storage cycle coalescence engines and coalescence methods including a horizontal full-blade water gravity turbine (11C) power generation electric product drive with a rotational output of 16 times or more that of an existing gas turbine.   A simple gas engine (89C) in which the existing stationary blades are completely abolished and the rotor blades are double-reversed is equipped with a compressed air heat exchanger (2Y), and the production amount of superheated steam (5H) is the same as that of the existing boiler. More than twice the rotation output of a simple gas engine automobile (89F) 80 times that of an existing gas turbine, combined with various energy storage cycle coalescence engines and coalescence containing horizontal full-blade water gravity turbine (11C) power generation electric product drive Method.   A simple gas engine (89C), which completely abolishes existing stationary blades and double-rotates all moving blades, is equipped with a compressed air heat exchanger (2Y) and produces the same amount of superheated steam (5H) with the same fuel amount. More than twice the rotation output of a simple gas engine vehicle (89F) that is 16 times that of an existing gas turbine, combined with various energy storage cycle coalescence engines and coalescence that include a horizontal all blade water gravity turbine (11C) power generation electric product drive Method.   A simple gas engine (89C) in which the existing stationary blades are completely abolished and the rotor blades are double-reversed is equipped with a compressed air heat exchanger (2Y), and the production amount of superheated steam (5H) is the same as that of the existing boiler. Various energy storage cycle coalescence engine and coalescence method including horizontal full-blade water-gravity turbine (11C) power generation electric product drive, with a rotational output more than 80 times that of existing gas turbines.   A simple gas engine (89C), which completely abolishes existing stationary blades and double-rotates all moving blades, is equipped with a compressed air heat exchanger (2Y) and produces the same amount of superheated steam (5H) with the same fuel amount. Various energy storage cycle coalescence engine and coalescence method including horizontal full-blade water gravity turbine (11C) power generation electric product drive, with a rotational output of 16 times or more that of existing gas turbines.   A simple gas engine (89C) in which the existing stationary blades are completely abolished and the rotor blades are double-reversed is equipped with a compressed air heat exchanger (2Y), and the production amount of superheated steam (5H) is the same as that of the existing boiler. Various energy storage cycle coalescence engines and coalescence methods including horizontal full-blade water gravity turbine (11C) power generation electric product drive, with a rotational output of 80 times or more of existing gas turbines, and a drive of a horizontal all-blade water gravity turbine (11C) generator and electric product drive.   A simple gas engine (89C), which completely abolishes existing stationary blades and double-rotates all moving blades, is equipped with a compressed air heat exchanger (2Y) and produces the same amount of superheated steam (5H) with the same fuel amount. Various energy storage cycle coalescence engines and coalescence methods including horizontal full-blade hydrogravity turbine (11C) power generation electrical product drive, with a rotational output of 16 times or more than existing gas turbines and a rotational output of more than double.   A simple gas engine (89C) in which the existing stationary blades are completely abolished and the rotor blades are double-reversed is equipped with a compressed air heat exchanger (2Y), and the production amount of superheated steam (5H) is the same as that of an existing boiler. Rotating output and injection propulsion output with a simple gas engine ship (89G) more than 20 times that of the existing gas turbine, and various energy storage cycles that include a horizontal all-bladed water gravity turbine (11C) power generation electric product drive Merger engine and merger method.   A simple gas engine (89C) in which the existing stationary blades are completely abolished and the rotor blades are double-reversed is equipped with a compressed air heat exchanger (2Y), and the production amount of superheated steam (5H) is the same as that of the existing boiler. Rotating output and injection propulsion output with a simple gas engine ship (89G) more than 40 times that of the existing gas turbine, and various energy storage cycles including a horizontal all blade hydrogravity turbine (11C) power generation electric product drive Merger engine and merger method.   A simple gas engine (89C), which completely abolishes existing stationary blades and double-rotates all moving blades, is equipped with a compressed air heat exchanger (2Y) and produces the same amount of superheated steam (5H) with the same fuel amount. Rotating output and injection propulsion output with a simple gas engine ship (89G) more than 8 times that of an existing gas turbine, and various energy storage cycles that include a horizontal all blade hydrogravity turbine (11C) power generation electric product drive Merger engine and merger method.   A simple gas engine (89C) in which the existing stationary blades are completely abolished and the rotor blades are double-reversed is equipped with a compressed air heat exchanger (2Y), and the production amount of superheated steam (5H) is the same as that of an existing boiler. Rotating power and injection propulsion power with a simple gas engine airplane (89H) more than 20 times that of the existing gas turbine, and various energy storage cycles that include a horizontal all blade hydrogravity turbine (11C) power generation electric product drive Merger engine and merger method.   A simple gas engine (89C) in which the existing stationary blades are completely abolished and the rotor blades are double-reversed is equipped with a compressed air heat exchanger (2Y), and the production amount of superheated steam (5H) is the same as that of the existing boiler. Rotating output and injection propulsion output with a simple gas engine airplane (89H) more than 40 times that of the existing gas turbine, and various energy storage cycles that include a horizontal all blade hydrogravity turbine (11C) power generation electric product drive Merger engine and merger method.   A simple gas engine (89C), which completely abolishes existing stationary blades and double-rotates all moving blades, is equipped with a compressed air heat exchanger (2Y) and produces the same amount of superheated steam (5H) with the same fuel amount. Rotating power and injection propulsion power with a simple gas engine airplane (89H) more than 8 times that of the existing gas turbine, and various energy storage cycles that include a horizontal all blade hydrogravity turbine (11C) power generation electric product drive Merger engine and merger method.   A simple gas engine (89C) in which the existing stationary blades are completely abolished and the rotor blades are double-reversed is equipped with a compressed air heat exchanger (2Y), and the production amount of superheated steam (5H) is the same as that of an existing boiler. Combined with various energy storage cycles including horizontal full-blade hydrogravity turbine (11C) power generation electric product drive with rotary output and injection propulsion output more than 20 times that of existing gas turbines Organization and coalescence method.   A simple gas engine (89C) in which the existing stationary blades are completely abolished and the rotor blades are double-reversed is equipped with a compressed air heat exchanger (2Y), and the production amount of superheated steam (5H) is the same as that of the existing boiler. Combined with various energy storage cycles including horizontal full-blade hydrogravity turbine (11C) power generation electric product drive with rotary output and injection propulsion output more than 40 times that of existing gas turbines Organization and coalescence method.   A simple gas engine (89C), which completely abolishes existing stationary blades and double-rotates all moving blades, is equipped with a compressed air heat exchanger (2Y) and produces the same amount of superheated steam (5H) with the same fuel amount. Combined with various energy storage cycles including horizontal full-blade hydrogravity turbine (11C) power generation electric product drive with rotary output and injection propulsion output more than 8 times that of existing gas turbines Organization and coalescence method.   A simple gas engine (89C) in which the existing stationary blades are completely abolished and the rotor blades are double-reversed is equipped with a compressed air heat exchanger (2Y), and the production amount of superheated steam (5H) is the same as that of an existing boiler. More than twice the rotation output and propulsion propulsion output is a large Osprey (89N) that is 20 times or more that of the existing gas turbine, combined with various energy storage cycle coalescence engines that include a horizontal full-blade hydrogravity turbine (11C) power generation electric product drive And coalescing method.   A simple gas engine (89C) in which the existing stationary blades are completely abolished and the rotor blades are double-reversed is equipped with a compressed air heat exchanger (2Y), and the production amount of superheated steam (5H) is the same as that of the existing boiler. More than twice the rotation output and injection propulsion output is 40 times or more large osprey (89N) of the existing gas turbine, combined with various energy storage cycle coalescence engine containing horizontal all blade water gravity turbine (11C) power generation electric product drive And coalescing method.   A simple gas engine (89C), which completely abolishes existing stationary blades and double-rotates all moving blades, is equipped with a compressed air heat exchanger (2Y) and produces the same amount of superheated steam (5H) with the same fuel amount. More than twice the rotation output and injection propulsion output is 8 times or more large osprey (89N) of the existing gas turbine, combined with various energy storage cycle combined engine containing horizontal all-blade water gravity turbine (11C) power generation electric product drive And coalescing method.   A simple injection engine (89E) in which the existing stationary blades are completely abolished and the rotor blades are double-reversed is equipped with a compressed air heat exchanger (2Y), and the production amount of superheated steam (5H) is the same as that of the existing boiler. Rotating output and injection propulsion output with a simple air injection engine ship (89I) more than 20 times that of the existing gas turbine, and various energy storage including a horizontal all blade hydrogravity turbine (11C) power generation electrical product drive Cycle coalescence engine and coalescence method.   A simple injection engine (89E) in which the existing stationary blades are completely abolished and the rotor blades are double-reversed is equipped with a compressed air heat exchanger (2Y), and the amount of superheated steam (5H) produced is the same fuel amount. Rotation output and injection propulsion output more than 40 times that of existing gas turbines, with a simple air injection engine ship (89I), and storage of various types of energy including horizontal all-bladed water gravity turbine (11C) power generation electrical product drive Cycle coalescence engine and coalescence method.   Equipped with a simple injection engine (89E) that completely abolishes existing stationary blades and double-rotating blades, and is equipped with a compressed air heat exchanger (2Y) to produce superheated steam (5H) with the same fuel amount. Rotating output and injection propulsion output more than double that of a simple air-injection engine ship (89I) that is 8 times or more that of an existing gas turbine, and various types of energy storage including a horizontal all blade hydrogravity turbine (11C) power generation electric product drive Cycle coalescence engine and coalescence method.   A simple injection engine (89E) in which the existing stationary blades are completely abolished and the rotor blades are double-reversed is equipped with a compressed air heat exchanger (2Y), and the production amount of superheated steam (5H) is the same as that of the existing boiler. Rotating power and injection propulsion power with a simple injection engine airplane (89J) more than 20 times that of the existing gas turbine, and various energy storage cycles that include a horizontal full-blade water gravity turbine (11C) power generation electrical product drive Merger engine and merger method.   A simple injection engine (89E) in which the existing stationary blades are completely abolished and the rotor blades are double-reversed is equipped with a compressed air heat exchanger (2Y), and the amount of superheated steam (5H) produced is the same fuel amount. Rotating power and injection propulsion power with a simple injection engine airplane (89J) more than 40 times that of the existing gas turbine, and various energy storage cycles that include a horizontal all blade hydrogravity turbine (11C) power generation electrical product drive Merger engine and merger method.   Equipped with a simple injection engine (89E) that completely abolishes existing stationary blades and double-rotating blades, and is equipped with a compressed air heat exchanger (2Y) to produce superheated steam (5H) with the same fuel amount. Rotating output and injection propulsion output with a simple injection engine airplane (89J) more than 8 times that of an existing gas turbine, and various energy storage cycles that include a horizontal all blade hydrogravity turbine (11C) power generation electric product drive Merger engine and merger method.   A simple injection engine (89E) in which the existing stationary blades are completely abolished and the rotor blades are double-reversed is equipped with a compressed air heat exchanger (2Y), and the production amount of superheated steam (5H) is the same as that of the existing boiler. Rotating power and injection propulsion power with a rotary blade injection airplane (89L) more than 20 times that of the existing gas turbine, and various energy storage cycles that include a horizontal all blade hydrogravity turbine (11C) power generation electric product drive Merger engine and merger method.   A simple injection engine (89E) in which the existing stationary blades are completely abolished and the rotor blades are double-reversed is equipped with a compressed air heat exchanger (2Y), and the amount of superheated steam (5H) produced is the same fuel amount. Rotation output and injection propulsion output with a rotary blade injection airplane (89L) more than 40 times that of an existing gas turbine, and various energy storage cycles that include a horizontal full blade hydrogravity turbine (11C) power generation electrical product drive Merger engine and merger method.   Equipped with a simple injection engine (89E) that completely abolishes existing stationary blades and double-rotating blades, and is equipped with a compressed air heat exchanger (2Y) to produce superheated steam (5H) with the same fuel amount. Rotating power and injection propulsion power with a rotary blade injection airplane (89L) more than 8 times that of an existing gas turbine, and various energy storage cycles that include a horizontal full blade hydrogravity turbine (11C) power generation electrical product drive Merger engine and merger method.   A simple injection engine (89E) in which the existing stationary blades are completely abolished and the rotor blades are double-reversed is equipped with a compressed air heat exchanger (2Y), and the production amount of superheated steam (5H) is the same as that of the existing boiler. More than twice the rotation output and propulsion propulsion output over 20 times the extra large Osprey (89M) of the existing gas turbine, combined with various energy storage cycle coalescence engine containing a horizontal all blade water gravity turbine (11C) power generation electric product drive And coalescing method.   A simple injection engine (89E) in which the existing stationary blades are completely abolished and the rotor blades are double-reversed is equipped with a compressed air heat exchanger (2Y), and the amount of superheated steam (5H) produced is the same fuel amount. More than twice the rotation output and propulsion propulsion output over 40 times that of the existing gas turbine Osprey (89M), combined with various energy storage cycle coalescence engines that include horizontal all-blade water gravity turbine (11C) power generation electrical product drive And coalescing method.   Equipped with a simple injection engine (89E) that completely abolishes existing stationary blades and double-rotating blades, and is equipped with a compressed air heat exchanger (2Y) to produce superheated steam (5H) with the same fuel amount. More than twice the rotation output and injection propulsion output over 8 times larger than the existing gas turbine Osprey (89M), combined with various energy storage cycle combined engine including horizontal all blade water gravity turbine (11C) power generation electric product drive And coalescing method.   Equipped with a simple air injection engine (89D) that completely abolishes existing stationary blades and double-rotates all blades, and has a compressed air heat exchanger (2Y), producing superheated steam (5H) with the same fuel amount as the existing boiler Various energies containing a horizontal all blade hydrogravity turbine (11C) power generation electric product drive, with a rotary output and injection propulsion output of 20 times or more and a simple air injection engine ship (89I) 20 times or more that of an existing gas turbine Storage cycle coalescence engine and coalescence method.   Equipped with a simple air injection engine (89D) that completely abolishes existing stationary blades and double-rotates all blades, and has a compressed air heat exchanger (2Y), producing superheated steam (5H) with the same fuel amount as the existing boiler Various energies containing a horizontal all-blade water gravity turbine (11C) power generation electric product drive with a rotary output and injection propulsion output of 40 times or more and a simple air injection engine ship (89I) 40 times or more that of an existing gas turbine Storage cycle coalescence engine and coalescence method.   Equipped with a simple air injection engine (89D) that completely abolishes existing stationary blades and double-rotates all blades, and has a compressed air heat exchanger (2Y), producing superheated steam (5H) with the same fuel amount as the existing boiler More than 8 times the rotation output and propulsion propulsion output is 8 times or more simple air injection engine ship (89I) of the existing gas turbine, and various energies including horizontal all blade water gravity turbine (11C) power generation electric product drive Storage cycle coalescence engine and coalescence method.   Various types of energy storage that can include a horizontal full-blade hydrogravity turbine (11C) power generation electrical product drive as a simple gas engine (89P) that sucks and compresses air (28a) heated to high temperature with a solar heater (21) Cycle coalescence engine and coalescence method.   It can contain a horizontal all blade hydrogravity turbine (11C) generator electric product drive that is a simple gas engine (89P) that makes the air (28a) heated to high temperature by the solar heater (21) to a suction compression ratio of 50 Various energy storage cycle coalescence engine and coalescence method.   It can contain a horizontal all blade hydrogravity turbine (11C) generator and electric product drive that is a simple gas engine (89P) that makes the air (28a) heated to high temperature in the solar heater (21) to a suction compression ratio 60 Various energy storage cycle coalescence engine and coalescence method.   It can contain a horizontal full-blade hydrogravity turbine (11C) power generation electric product drive that is a simple gas engine (89P) that makes the air (28a) heated to high temperature by the solar heater (21) to a suction compression ratio 70 Various energy storage cycle coalescence engine and coalescence method.   It can contain a horizontal all blade hydrogravity turbine (11C) generator electric product drive that is a simple gas engine (89P) that makes the air (28a) heated to high temperature by the solar heater (21) to a suction compression ratio 80 Various energy storage cycle coalescence engine and coalescence method.   It can contain a horizontal all blade hydrogravity turbine (11C) generator electric product drive that is a simple gas engine (89P) that makes the air (28a) heated to high temperature by the solar heater (21) to a suction compression compression ratio of 90 Various energy storage cycle coalescence engine and coalescence method.   It can contain a horizontal all blade hydrogravity turbine (11C) generator and electric product drive that is a simple gas engine (89P) that makes the air (28a) heated to high temperature by the solar heater (21) to a suction compression ratio of 100 Various energy storage cycle coalescence engine and coalescence method.   Horizontal full-blade water gravity turbine as a simple gas engine (89P) that injects air (28a) heated at a high temperature by a solar heater (21) into a compressed air heat exchanger (2Y) with a suction compression ratio of 50 (11C) Various energy storage cycle coalescence engines and coalescence methods that can contain power generation product drives.   Horizontal full-blade water gravity turbine as a simple gas engine (89P) that injects air (28a) heated at a high temperature by a solar heater (21) into a compressed air heat exchanger (2Y) with a suction compression ratio 60. (11C) Various energy storage cycle coalescence engines and coalescence methods that can contain power generation product drives.   A horizontal full-blade hydrogravity turbine as a simple gas engine (89P) that injects air (28a) heated to high temperature by a solar heater (21) into a compressed air heat exchanger (2Y) with a suction compression ratio 70. (11C) Various energy storage cycle coalescence engines and coalescence methods that can contain power generation product drives.   Horizontal full-blade water gravity turbine as a simple gas engine (89P) that injects air (28a) heated at a high temperature by a solar heater (21) into a compressed air heat exchanger (2Y) with a suction compression ratio 80. (11C) Various energy storage cycle coalescence engines and coalescence methods that can contain power generation product drives.   Horizontal full-blade water gravity turbine as a simple gas engine (89P) that injects air (28a) heated at a high temperature by a solar heater (21) into a compressed air heat exchanger (2Y) at a suction compression ratio 90. (11C) Various energy storage cycle coalescence engines and coalescence methods that can contain power generation product drives.   Horizontal full-blade water gravity turbine as a simple gas engine (89P) that injects air (28a) heated at a high temperature by a solar heater (21) into a compressed air heat exchanger (2Y) with a suction compression ratio of 100 (11C) Various energy storage cycle coalescence engines and coalescence methods that can contain power generation product drives.   Air (28a) heated to high temperature by the solar heater (21) is heated with superheated steam by suction compressed water jet cooling compression, and is injected into the compressed air heat exchanger (2Y) with a compression ratio of 50 ( 89P), various energy storage cycle coalescence engines and coalescence methods capable of containing a horizontal full-blade water gravity turbine (11C) power generation electric product drive.   Air (28a) heated to a high temperature by the solar heater (21) is heated by superheated steam water by suction compressed water injection cooling compression, and is injected into the compressed air heat exchanger (2Y) at a compression ratio of 60 ( 89P), various energy storage cycle coalescence engines and coalescence methods capable of containing a horizontal full-blade water gravity turbine (11C) power generation electric product drive.   Air (28a) heated to high temperature by the solar heater (21) is heated by superheated steam water by suction compressed water jet cooling compression, and is injected into the compressed air heat exchanger (2Y) with a compression ratio of 70 ( 89P), various energy storage cycle coalescence engines and coalescence methods capable of containing a horizontal full-blade water gravity turbine (11C) power generation electric product drive.   Air (28a) heated to a high temperature by the solar heater (21) is heated with superheated steam by suction compressed water jet cooling compression, and is injected into the compressed air heat exchanger (2Y) with a compression ratio of 80 ( 89P), various energy storage cycle coalescence engines and coalescence methods capable of containing a horizontal full-blade water gravity turbine (11C) power generation electric product drive.   Air (28a) heated to high temperature by the solar heater (21) is heated with superheated steam by suction compressed water jet cooling compression, and is injected into the compressed air heat exchanger (2Y) with a compression ratio of 90 ( 89P), various energy storage cycle coalescence engines and coalescence methods capable of containing a horizontal full-blade water gravity turbine (11C) power generation electric product drive.   Air (28a) heated to high temperature by the solar heater (21) is heated with superheated steam by suction compressed water injection cooling compression, and is injected into the compressed air heat exchanger (2Y) with a compression ratio of 100 ( 89P), various energy storage cycle coalescence engines and coalescence methods capable of containing a horizontal full-blade water gravity turbine (11C) power generation electric product drive.   A simple gas engine (89P) that produces air (28a) heated at a high temperature by a solar heater (21) with an intake compression ratio of 50 and produces compressed fuel injection combustion heat exchange superheated steam 5H in a compressed air heat exchanger (2Y) Various energy storage cycle coalescence engine and coalescence method capable of containing a horizontal all blade hydrogravity turbine (11C) generator electric product drive.   A simple gas engine (89P) for producing a heated air (28a) heated by a solar heater (21) at a suction compression compression ratio of 60 and producing an injection fuel injection combustion heat exchange superheated steam 5H in a compressed air heat exchanger (2Y) Various energy storage cycle coalescence engine and coalescence method capable of containing a horizontal all blade hydrogravity turbine (11C) generator electric product drive.   A simple gas engine (89P) that produces air (28a) heated to a high temperature by a solar heater (21) with a suction compression compression ratio of 70 and produces a fuel injection fuel injection combustion heat exchange superheated steam 5H in a compressed air heat exchanger (2Y) Various energy storage cycle coalescence engine and coalescence method capable of containing a horizontal all blade hydrogravity turbine (11C) generator electric product drive.   A simple gas engine (89P) for producing a heated air (28a) heated by a solar heater (21) at a suction compression ratio 80 and producing an injection fuel injection combustion heat exchange superheated steam 5H in a compressed air heat exchanger (2Y) Various energy storage cycle coalescence engine and coalescence method capable of containing a horizontal all blade hydrogravity turbine (11C) generator electric product drive.   A simple gas engine (89P) that produces air (28a) heated at a high temperature by a solar heater (21) at a suction compression ratio 90 and is produced in a compressed air heat exchanger (2Y) by injection fuel injection combustion heat exchange superheated steam 5H Various energy storage cycle coalescence engine and coalescence method capable of containing a horizontal all blade hydrogravity turbine (11C) generator electric product drive.   A simple gas engine (89P) that produces air (28a) heated at a high temperature by a solar heater (21) with an intake compression ratio of 100, and produces compressed fuel injection combustion heat exchange superheated steam 5H in a compressed air heat exchanger (2Y) Various energy storage cycle coalescence engine and coalescence method capable of containing a horizontal all blade hydrogravity turbine (11C) generator electric product drive.   Air (28a) heated to a high temperature by the solar heater (21) is set to a suction compression ratio 50, and the compressed air heat exchanger (2Y) is injected with the same amount of fuel as the injection fuel injection combustion heat exchange superheated steam 5H of the existing boiler 50. Various energy storage cycle coalescence engine and coalescence method capable of containing a horizontal all-blade water gravity turbine (11C) generator electric product drive as a simple gas engine (89P) to produce more than twice.   The air (28a) heated to high temperature by the solar heater (21) is set to a suction compression ratio 60, and the compressed air heat exchanger (2Y) is injected with the same amount of fuel as the injected fuel injection combustion heat exchange superheated steam 5H 60 of the existing boiler. Various energy storage cycle coalescence engine and coalescence method capable of containing a horizontal all-blade water gravity turbine (11C) power generation electric product drive as a simple gas engine (89P) manufactured and manufactured more than twice.   The air (28a) heated to a high temperature by the solar heater (21) is set to a suction compression ratio 70, and the compressed air heat exchanger (2Y) is injected with the same amount of fuel by the injected fuel injection combustion heat exchange superheated steam 5H of the existing boiler 70. Various energy storage cycle coalescence engine and coalescence method capable of containing a horizontal all-blade water gravity turbine (11C) power generation electric product drive as a simple gas engine (89P) manufactured and manufactured more than twice.   Air (28a) heated to a high temperature by the solar heater (21) is set to a suction compression ratio 80, and the compressed air heat exchanger (2Y) is injected with the same amount of fuel by the injection fuel injection combustion heat exchange superheated steam 5H of the existing boiler 80. Various energy storage cycle coalescence engine and coalescence method capable of containing a horizontal all-blade water gravity turbine (11C) power generation electric product drive as a simple gas engine (89P) manufactured and manufactured more than twice.   The air (28a) heated to a high temperature by the solar heater (21) is set to a suction compression ratio 90, and the compressed air heat exchanger (2Y) is injected with the injected fuel injection combustion heat exchange superheated steam 5H with the same fuel amount 90 of the existing boiler. Various energy storage cycle coalescence engine and coalescence method capable of containing a horizontal all-blade water gravity turbine (11C) power generation electric product drive as a simple gas engine (89P) manufactured and manufactured more than twice.   Air (28a) heated to high temperature by the solar heater (21) is set to a suction compression ratio 100, and the compressed air heat exchanger (2Y) is injected with the same amount of fuel by the injected fuel injection combustion heat exchange superheated steam 5H of the existing boiler 100. Various energy storage cycle coalescence engine and coalescence method capable of containing a horizontal all-blade water gravity turbine (11C) power generation electric product drive as a simple gas engine (89P) manufactured and manufactured more than twice.   A simple gas engine (89P) which produces air (28a) heated at a high temperature by the solar heater (21) with an intake compression compression ratio of 50 or more and produces the injected fuel injection combustion heat exchange superheated steam 5H in the compressed air heat exchanger (2Y). ) + Energy storage cycle coalescence engine and coalescence method capable of containing horizontal all blade hydrogravity turbine (11C) power generation electric product drive as vertical all blade steam turbine (11F).   A simple gas engine (89P) that produces high-temperature air (28a) heated by the solar heater (21) at a suction compression compression ratio of 60 or more and produces the injected fuel injection combustion heat exchange superheated steam 5H in the compressed air heat exchanger (2Y). ) + Energy storage cycle coalescence engine and coalescence method capable of containing horizontal all blade hydrogravity turbine (11C) power generation electric product drive as vertical all blade steam turbine (11F).   A simple gas engine (89P) that produces high-temperature air (28a) heated by the solar heater (21) with a suction compression ratio of 70 or more and produces the injected fuel injection combustion heat exchange superheated steam 5H in the compressed air heat exchanger (2Y) ) + Energy storage cycle coalescence engine and coalescence method capable of containing horizontal all blade hydrogravity turbine (11C) power generation electric product drive as vertical all blade steam turbine (11F).   A simple gas engine (89P) that produces high-temperature air (28a) heated by the solar heater (21) at a suction air compression ratio of 80 or more and is produced in the compressed air heat exchanger (2Y) by injection fuel injection combustion heat exchange superheated steam 5H. ) + Energy storage cycle coalescence engine and coalescence method capable of containing horizontal all blade hydrogravity turbine (11C) power generation electric product drive as vertical all blade steam turbine (11F).   A simple gas engine (89P) which produces air (28a) heated at a high temperature by the solar heater (21) with an intake compression compression ratio of 90 or more and produces the injected fuel injection combustion heat exchange superheated steam 5H in the compressed air heat exchanger (2Y). ) + Energy storage cycle coalescence engine and coalescence method capable of containing horizontal all blade hydrogravity turbine (11C) power generation electric product drive as vertical all blade steam turbine (11F).   A simple gas engine (89P) that produces high-temperature air (28a) heated by the solar heater (21) at a suction compression compression ratio of 100 or more and produces the injected fuel injection combustion heat exchange superheated steam 5H in the compressed air heat exchanger (2Y). ) + Energy storage cycle coalescence engine and coalescence method capable of containing horizontal all blade hydrogravity turbine (11C) power generation electric product drive as vertical all blade steam turbine (11F).   A simple gas engine (89P) which produces air (28a) heated at a high temperature by the solar heater (21) with an intake compression compression ratio of 50 or more and produces the injected fuel injection combustion heat exchange superheated steam 5H in the compressed air heat exchanger (2Y). ) + Energy storage cycle coalescence engine and coalescence method capable of containing a horizontal all blade hydrogravity turbine (11C) power generation electrical product drive that is a vertical all blade steam turbine (11F) power generation.   A simple gas engine (89P) that produces high-temperature air (28a) heated by the solar heater (21) at a suction compression compression ratio of 60 or more and produces the injected fuel injection combustion heat exchange superheated steam 5H in the compressed air heat exchanger (2Y). ) + Energy storage cycle coalescence engine and coalescence method capable of containing a horizontal all blade hydrogravity turbine (11C) power generation electrical product drive that is a vertical all blade steam turbine (11F) power generation.   A simple gas engine (89P) that produces high-temperature air (28a) heated by the solar heater (21) with a suction compression ratio of 70 or more and produces the injected fuel injection combustion heat exchange superheated steam 5H in the compressed air heat exchanger (2Y) ) + Energy storage cycle coalescence engine and coalescence method capable of containing a horizontal all blade hydrogravity turbine (11C) power generation electrical product drive that is a vertical all blade steam turbine (11F) power generation.   A simple gas engine (89P) that produces high-temperature air (28a) heated by the solar heater (21) at a suction air compression ratio of 80 or more and is produced in the compressed air heat exchanger (2Y) by injection fuel injection combustion heat exchange superheated steam 5H. ) + Energy storage cycle coalescence engine and coalescence method capable of containing a horizontal all blade hydrogravity turbine (11C) power generation electrical product drive that is a vertical all blade steam turbine (11F) power generation.   A simple gas engine (89P) which produces air (28a) heated at a high temperature by the solar heater (21) with an intake compression compression ratio of 90 or more and produces the injected fuel injection combustion heat exchange superheated steam 5H in the compressed air heat exchanger (2Y). ) + Energy storage cycle coalescence engine and coalescence method capable of containing a horizontal all blade hydrogravity turbine (11C) power generation electrical product drive that is a vertical all blade steam turbine (11F) power generation.   A simple gas engine (89P) that produces high-temperature air (28a) heated by the solar heater (21) at a suction compression compression ratio of 100 or more and produces the injected fuel injection combustion heat exchange superheated steam 5H in the compressed air heat exchanger (2Y). ) + Energy storage cycle coalescence engine and coalescence method capable of containing a horizontal all blade hydrogravity turbine (11C) power generation electrical product drive that is a vertical all blade steam turbine (11F) power generation.   A simple gas engine (89P) which produces air (28a) heated at a high temperature by the solar heater (21) with an intake compression compression ratio of 50 or more and produces the injected fuel injection combustion heat exchange superheated steam 5H in the compressed air heat exchanger (2Y). ) + Vertical all-blade steam turbine (11F) power generation and the same fuel amount Various energy that can contain horizontal all-blade water gravity turbine (11C) power generation electric product drive with 20 times more power generation than existing thermal power generation Storage cycle coalescence engine and coalescence method.   A simple gas engine (89P) that produces high-temperature air (28a) heated by the solar heater (21) at a suction compression compression ratio of 60 or more and produces the injected fuel injection combustion heat exchange superheated steam 5H in the compressed air heat exchanger (2Y). ) + Vertical type full-blade steam turbine (11F) power generation and the same fuel amount Various energy that can contain horizontal type full-blade water gravity turbine (11C) power generation electric product drive with 40 times more power generation than existing thermal power generation Storage cycle coalescence engine and coalescence method.   A simple gas engine (89P) that produces high-temperature air (28a) heated by the solar heater (21) with a suction compression ratio of 70 or more and produces the injected fuel injection combustion heat exchange superheated steam 5H in the compressed air heat exchanger (2Y) ) + Vertical all blade steam turbine (11F) power generation and the same fuel amount Various energy that can contain horizontal all blade hydrogravity turbine (11C) power generation electric product drive with power generation amount more than 60 times that of existing thermal power generation Storage cycle coalescence engine and coalescence method.   A simple gas engine (89P) that produces high-temperature air (28a) heated by the solar heater (21) at a suction air compression ratio of 80 or more and is produced in the compressed air heat exchanger (2Y) by injection fuel injection combustion heat exchange superheated steam 5H. ) + Vertical type full-blade steam turbine (11F) power generation and the same fuel amount Various energy that can contain horizontal type full-blade water gravity turbine (11C) power generation electric product drive with 80 times more power generation than existing thermal power generation Storage cycle coalescence engine and coalescence method.   A simple gas engine (89P) which produces air (28a) heated at a high temperature by the solar heater (21) with an intake compression compression ratio of 90 or more and produces the injected fuel injection combustion heat exchange superheated steam 5H in the compressed air heat exchanger (2Y). ) + Vertical all-blade steam turbine (11F) power generation and the same fuel amount Various energy that can contain horizontal all-blade water gravity turbine (11C) power generation electric product drive that is more than 100 times the power generation of existing thermal power generation Storage cycle coalescence engine and coalescence method.   A simple gas engine (89P) that produces high-temperature air (28a) heated by the solar heater (21) at a suction compression compression ratio of 100 or more and produces the injected fuel injection combustion heat exchange superheated steam 5H in the compressed air heat exchanger (2Y). ) + Vertical type all-blade steam turbine (11F) power generation and the same fuel amount Various energy that can contain horizontal type full-blade water gravity turbine (11C) power generation electric product drive with 120 times more power generation than existing thermal power generation Storage cycle coalescence engine and coalescence method. The superheated steam (5H) manufactured by the simple gas engine (89P) is raised by the superheated steam pipe (5H) to the top of the vertical all blade steam turbine (11F), the open / close valve (1Q) is released, and the superheated steam (5H) is injected. Various energy storage cycle coalescing engines capable of containing a horizontal full-blade water gravity turbine (11C) generating electric product drive that double-rotates the cylindrical outer blade group (60D) + cylindrical inner blade group (60C). And coalescing method. The superheated steam (5H) manufactured by the simple gas engine (89P) is raised by the superheated steam pipe (5H) to the top of the vertical all blade steam turbine (11F) to release the on-off valve (1Q), and the superheated steam (5H) A horizontal full-blade hydrogravity turbine (11C) power generation electric product driven to reduce the volume of impulse liquefied steam in the process of contra-rotation drive by injecting the cylinder outer blade group (60D) + cylinder inner blade group (60C) Various energy storage cycle coalescence engines and coalescence methods that can be contained. The superheated steam (5H) manufactured by the simple gas engine (89P) is raised by the superheated steam pipe (5H) to the top of the vertical all blade steam turbine (11F) to release the on-off valve (1Q), and the superheated steam (5H) Horizontal full-blade hydrogravity turbine (11C) power generation electric manufacturing that sucks blast water and reduces impulse liquefied steam volume in the process of double reversal drive of cylindrical outer blade group (60D) + cylindrical inner blade group (60C) Various energy storage cycle coalescence engine and coalescence method capable of containing an object drive. The superheated steam (5H) manufactured by the simple gas engine (89P) is raised by the superheated steam pipe (5H) to the top of the vertical all blade steam turbine (11F) to release the on-off valve (1Q), and the superheated steam (5H) Horizontal full-rotor blade water gravity turbine (11C) power generation electricity that reduces the impulse liquefied steam volume in the process of double reversal drive by sucking and jetting the spray water to make the cylindrical outer blade group (60D) + cylindrical inner blade group (60C) Various energy storage cycle coalescence engines and coalescence methods capable of containing product drive. The superheated steam (5H) manufactured by the simple gas engine (89P) is raised by the superheated steam pipe (5H) to the top of the vertical all blade steam turbine (11F) to release the on-off valve (1Q), and the superheated steam (5H) Horizontal full-blade hydrogravity turbine (11C) generator electric manufacturing that reduces the volume of impulse liquefied steam in the process of double reversal drive by sucking low-temperature water jet and cylindrical outer rotor blade group (60D) + cylindrical inner rotor blade group (60C) Various energy storage cycle coalescence engine and coalescence method capable of containing an object drive. The superheated steam (5H) manufactured by the simple gas engine (89P) is raised by the superheated steam pipe (5H) to the top of the vertical all blade steam turbine (11F) to release the on-off valve (1Q), and the superheated steam (5H) Horizontal type full-blade water gravity turbine (11C) power generation that reduces the impulse liquefied steam volume in the process of double reversal drive by sucking and jetting low temperature water injected into the cylinder outer blade group (60D) + cylinder inner blade group (60C) Various energy storage cycle coalescing engines and coalescence methods that can contain electrical product drives. The superheated steam (5H) manufactured by the simple gas engine (89P) is raised by the superheated steam pipe (5H) to the top of the vertical all blade steam turbine (11F) to release the on-off valve (1Q), and the superheated steam (5H) Horizontal type full-blade water gravity turbine (11C) power generation electricity that sucks high-temperature jet water and reduces the volume of impulse liquefied steam in the process of double reversal drive of the outer cylinder group (60D) and the inner cylinder group (60C) Various energy storage cycle coalescence engines and coalescence methods capable of containing product drive. The superheated steam (5H) manufactured by the simple gas engine (89P) is raised by the superheated steam pipe (5H) to the top of the vertical all blade steam turbine (11F) to release the on-off valve (1Q), and the superheated steam (5H) Horizontal all-blade water gravity turbine (11C) power generation that reduces the impulse liquefied steam volume in the process of double inversion drive by sucking and injecting high-temperature water injected into the cylinder outer blade group (60D) + cylinder inner blade group (60C) Various energy storage cycle coalescing engines and coalescence methods that can contain electrical product drives. The superheated steam (5H) manufactured by the simple gas engine (89P) is raised by the superheated steam pipe (5H) to the top of the vertical all blade steam turbine (11F) to release the on-off valve (1Q), and the superheated steam (5H) Horizontal type full-blade water gravity that reduces the volume of impulse liquefied steam in the process of double reversal drive by accelerating gravity acceleration in vacuum by sucking and jetting high-temperature water in the process of double reversal drive of cylinder outer blade group (60D) + cylinder inner blade group (60C) Various energy storage cycle coalescence engine and coalescence method capable of containing turbine (11C) power generation electrical product drive. The superheated steam (5H) manufactured by the simple gas engine (89P) is raised by the superheated steam pipe (5H) to the top of the vertical all blade steam turbine (11F) to release the on-off valve (1Q), and the superheated steam (5H) Horizontal full blade hydrogravity turbine that reduces the volume of impulse liquefied steam in the process of double reversal drive by accelerating the acceleration of gravity in suction vacuum and accelerating the cylinder outer blade group (60D) + cylinder inner blade group (60C) 11C) Various energy storage cycle coalescing engines and coalescence methods that can contain power generation electrical product drives. The superheated steam (5H) manufactured by the simple gas engine (89P) is raised by the superheated steam pipe (5H) to the top of the vertical all blade steam turbine (11F) to release the on-off valve (1Q), and the superheated steam (5H) Horizontal full blade hydrogravity turbine that reduces the volume of impulse liquefied steam in the process of double reversal drive by accelerating gravitational acceleration in vacuum by sucking and spraying water into the cylinder outer blade group (60D) + cylinder inner blade group (60C) (11C) Various energy storage cycle coalescence engines and coalescence methods that can contain power generation product drives. The superheated steam (5H) manufactured by the simple gas engine (89P) is raised by the superheated steam pipe (5H) to the top of the vertical all blade steam turbine (11F) to release the on-off valve (1Q), and the superheated steam (5H) Horizontal full blade hydrogravity turbine that reduces the volume of impulse liquefied steam in the process of double reversal drive by accelerating gravitational acceleration in jet low-temperature water suction vacuum and rotating cylinder outer blade group (60D) + cylinder inner blade group (60C) 11C) Various energy storage cycle coalescence engines and coalescence methods that can contain power generation electrical product drives. The superheated steam (5H) manufactured by the simple gas engine (89P) is raised by the superheated steam pipe (5H) to the top of the vertical all blade steam turbine (11F) to release the on-off valve (1Q), and the superheated steam (5H) Horizontal full blade water gravity that reduces the volume of impulse liquefied steam in the process of double reversal drive by accelerating gravitational acceleration in vacuum by sucking and spraying jet low temperature water in the process of double reversal drive of cylinder outer blade group (60D) + cylinder inner blade group (60C) Various energy storage cycle coalescence engine and coalescence method capable of containing turbine (11C) power generation electrical product drive. The superheated steam (5H) manufactured by the simple gas engine (89P) is raised by the superheated steam pipe (5H) to the top of the vertical all blade steam turbine (11F) to release the on-off valve (1Q), and the superheated steam (5H) Vertical-rotary blade water gravity that reduces the volume of impulse liquefied steam in the process of double reversal drive by accelerating the acceleration of gravity in vacuum by sucking high-temperature water jet and rotating the outer blade group (60D) + inner cylinder blade group (60C) Various energy storage cycle coalescence engine and coalescence method capable of containing turbine (11A) power generation electrical product drive.

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