JP2014173506A - Various energy conservation cycle combination engine - Google Patents

Abstract

PROBLEM TO BE SOLVED: To enable injection speed of substance 3E, vacuum and head drop to be manufactured with wisdom of mankind in view of the fact that the maximum energy on the earth that can be manufactured through gravitational acceleration and head drop in vacuum of large specific gravity substance.SOLUTION: A column pipe 12B of a gravitational electric power generation building 12 for manufacturing a head drop is also used as a large specific gravity substance lifting device 2F. Substance with large specific weight 3E is applied to generate electric power through a vertical full dynamic blade substance with large specific weight 3E gravitational turbine 11B for accelerating through gravitational acceleration in the lifting conservation injection vacuum at an uppermost part. This is more than 10 times of the existing pumping-up electric power generation under the same amount of water. Improved existing gas turbine is attained by making a stationary blade into a dynamic blade in double reverse rotating, super-heated steam 5H manufactured by a compressed air heat exchanger 2Y is applied to manufacture 20 times of heated steam in the existing boiler, various engines including all the dynamic blades for outputting 10 times rotation plus 10 times injection propulsion, automobiles run in 1/10 fuel cost, airplanes or ships run in ten times speed, the airplanes are driven by 1/50 ten thousands as expenditures for reaching space, and an operational profit rate in all applications for manufactured products such as one-day trip every where on the earth is remarkably No.1 class in the world eternally.

Description

The vertical turbine blade critical material gravity turbine 11B power generation of the present invention has practically used a difficult-to-manufacture all-blade counter-rotating engine whose state-of-the-art science and technology is far from the world, and has almost 100% exclusive monopoly production worldwide. Gravity-powered buildings aiming at eternal monopoly operation, water electrolysis prime, etc., because the energy that can be most easily regenerated on the earth is the gravitational acceleration in vacuum and the amount of power generation is proportional to the specific material velocity x head The height and strength of the 12+ specific material rising device 2F is the most important, the column tube 12B is used as the specific material rising device 2F, and the column of the steel frame 12A is made strong by increasing the tube diameter, such as 800 m or more. Rotating balance adjustment during ultra-high speed rotation is the most important process in the manufacturing process of vertical type moving blade ratio critical material gravity turbine 11B, which can make a powerful high-rise building. As a work, various bearings 12C are provided at both ends of the inner shaft device 60A and the outer shaft device 60B, the inner shaft device 60A and the outer shaft device 60B are separately assembled, and each of them is adjusted with an ultra-high speed rotation balance with a machine tool. After disassembling and making this assembly, unconventional inner shaft device 60A / cylindrical inner rotor blade group 60C and outer shaft device 60B / cylindrical outer rotor blade group 60D are double-reversed. The present invention relates to a technique for energy conservation and coalescence.

The vertical all-blade ratio critical material gravity turbine 11B power generation electric drive engine and electric product drive engine are the same as described above, and the most important process is the rotation balance adjustment processing at the time of ultra-high speed rotation. Various types of bearings 12C are provided at both ends of each device 60B, the inner shaft device 60A and the outer shaft device 60B are separately assembled, and each is disassembled after ultra-high speed rotation balance adjustment processing with a machine tool to form this assembly. Liquid oxygen producing machine 89A, simple multistage compressor 89B, simple gas engine 89C, simple air injection engine 89D, etc. By driving the injection engine 89E, a simple gas engine automobile 89F, a simple gas engine ship 89G, a simple gas engine airplane 89H, a simple air injection engine ship 89I, a simple injection engine flight Aircraft 89J, rotary wing airplane 89K, rotary wing jet airplane 89L, extra large Osprey 89M and large Osprey 89N are driven, and in the drive of ships, nitrogen, oxygen and CO2 are supplied to seawater as natural phenomenon acceleration 2a And seaweeds increase, fish and other human foods increase in the food chain, etc., and by plane and automobile drive, CO2 exhaust 1/10, fuel costs 1/10 and 1 / 500,000 costs aim to reach space, planes and ships The present invention relates to various energy conservation cycle coalescence engines and various energy conservation coalescence techniques aiming at 10 times speed and aiming for the world's most eternally sustainable operating profit rate.

  Since the pump input is proportional to the cube of the rotational speed of recent pumped-storage power generation, I agree with the adoption of a variable speed motor, but the experiments are conducted because the water speed of the existing pumped-storage power generation is Mach 1/7, Mach 1/5, etc. As a result, the water speed of the same water mass will increase to 10 times Mach 2 injection speed production of existing pumped-storage power generation x gravity acceleration 0 production in vacuum x 10 times drop production power generation = 100 times power generation quantity, Astronomical gravity production of Russia approaches the fallen meteorite speed Mach 50 of Russia, the same water mass approaches 100 times × 50/2 = 2500 times the existing pumped power generation amount, and astronomical that the power generation amount is proportional to the cube of the speed There is a background technology that produces a large amount of power generation, and Japan's fiscal deficit of 1,000 trillion yen has been reduced to 0 in a relatively short period of time due to the global warming prevention revolution, the economic growth strategy revolution, and the world's most eternal operating profit rate. Background that can be aimed at Surgery there is.

  The boiler of the existing thermal power generation produces superheated steam by atmospheric pressure fuel combustion and power generation by the 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 When fuel injection combustion is performed in 20 air, the combustion temperature greatly exceeds 13 times, and there is a background technology that makes the amount of superheated steam 5H production that exceeds 13 times that of existing boilers with the same amount of fuel required for experiments. Technological airplanes and marine gas turbines are equipped with alternating stationary blades and moving blades. In the compressor, compressed air is repeatedly dammed by the stationary blades, and the combustion gas is blocked by the stationary blades. Change the direction and repeat the change of direction, and have half of the stationary vanes with no work, alternately with the moving blades, and set the rotation output and jet propulsion output to 1/10 to 1/100, etc. 1/10 Therefore, airplanes and ships are aiming for 10 times speed, airplanes are in full space flight, the space arrival cost is 1 / 500,000, and the earth goes around 16 times a day. There is.

Japanese Patent No. 1607151, Patent No. 1609617, Patent No. 1645350, Patent No. 1924889, Patent No. 1912522, Patent No. 1959305, Patent No. 11986119, Patent No. 2646636, 1992 U.S. Pat. No. 5,133,305, 1993 U.S. Pat. US Pat. No. 5,429,078, 1997 US Pat. No. 5,701,864, PCT International Application No. PCT / JP97 / 01814, US Pat. No. 6,119,650, Chinese Patent No. 8818, EU British Patent No. 902175, PCT International Application No. PCT / JP97 / 02250 No. 6,263,664.

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 No. 2013-7975: January 21, 2013.

  In the existing pumped-storage power generation, the unit code violation of the work load kg weight m / second is obvious, such as using only the potential energy and generating less than the pumped power. And the improvement of compressors and turbines for gas turbines that drive airplanes and ships is provided with alternating stationary blades and moving blades. Then, there is a problem of improving the point that it is too unreasonable, such as damming the gas velocity with a stationary blade and repeating reverse injection and consuming most of the gas velocity with a stationary blade that does not work at all.

An existing stationary blade is a cylindrical outer moving blade group 60B and an existing moving blade is a cylindrical inner moving blade group 60A. A vertical total moving blade specific material gravity turbine 11B, a liquid oxygen production machine 89A, and a simple multistage compressor 89B, simple gas engine 89C, simple air injection engine 89D, simple injection engine 89E, and vehicles such as automobiles, ships, and airplanes are driven by rotational force and jet propulsion, and the airplane is near the existing highest flight altitude. More superheated steam rockets are injected, space arrival costs are about the same as existing fuel costs, and around the earth 16 times a day at the height of space flight, etc. Power generation, ships, airplanes, automobiles, etc., which are monopolized and secretly operated, improve the point of existing state-of-the-art science and technology, and make it the best in the world with outstanding profitability and the best in new employment. To prevent global warming.

Experimentation is necessary, but adding gravity acceleration + injection speed + head in the vacuum to the power generation part of the existing pumped-storage power generation has a great effect of making the power generation of the same pumping capacity 10 to 100 times the target of power generation, Vertical type moving blade ratio critical material gravity turbine 11B fuel cost 0 low cost power generation, heat heated by electric drive solar heater 21 to recover compression heat, heat production heat close to infinity at 0 fuel cost The effect that can be used is also great, and liquid nitrogen and liquid oxygen as by-products are also enormous, so liquid nitrogen has a great effect that can be used as various kinds of cold heat such as ice production. When liquid oxygen is used instead of air compression, it is compressed The work rate is set to 21/60000 volumetric compression work rate of air compression, simple gas engine 89C, simple air injection engine 89D, simple injection engine 89E, etc. are driven, and vehicles such as automobiles, ships and airplanes are driven. To rolling force driving and injection propulsion drive, great effect and which aim to 1/10 the fuel costs and 10 double speed, the effect of global warming prevention revolution.

Illustration of gravity power building 12 (Example 1) Explanatory drawing of vertical type moving blade ratio critical material gravity turbine 11B bearing 12C (Example 2) Explanatory drawing of the cylindrical blade group of the inner shaft device 60A and the outer shaft device 60B (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 simple air injection engine 89D (Example 8) Explanatory drawing of the simple injection engine 89E (Example 9) Illustration of simple gas locomotive 89F (Example 10) Explanatory drawing of simple gas engine ship 89G (Example 11) Explanatory drawing of the simple gas engine airplane 89H (Example 12) Explanatory drawing of the simple air injection engine ship 89I (Example 13) Explanatory drawing of simple injection engine airplane 89J (Example 14) Explanatory drawing of rotary wing airplane 89K (Example 15) Explanatory drawing of rotary wing jet airplane 89L (Example 16) Illustration of oversized Osprey 89M (Example 17) Illustration of Large Osprey 89N (Example 18)

  Since there is no example of a counter-rotating engine in the existing technology and the present invention is entirely related to the counter-rotating engine, the inner rotor blade group 60C and the outer cylinder rotor group 60D are separately assembled in the manufacturing process, Is equipped with various bearings and can be rotated and machined by machine tools in the same way as during operation, and each of them has a completely new machining technology, with the same amount of pumped water. Demonstrate the current state-of-the-art science and technology that is unreasonable by challenging the power generation capacity 10 to 100 times that of existing pumped-storage power generation, aiming at the prime of space flight with the same fuel amount, and planes and ships with the same fuel amount 10 times faster .

In the gravity power generation building 12 of FIG. 1, 1/7 to 1/5 of pumped water generation water speed sound speed is gravity acceleration + injection speed Mach 1 to 3 in a vacuum, and power is generated at a mercury 3E speed Mach 3 or more to generate the same mercury 3E. Aiming at 15 times or more of the mass pumped-storage power generation, the drop is aimed to increase the infinite production power generation in the gravity power generation building 12, and the water 3E of a specific material is injected at a high speed from the top of the gravity power generation building 12 to increase the degree of vacuum In the process of accelerating the acceleration of gravity in the middle, the cylinder outer rotor blade group 60D + cylindrical inner rotor blade group 60C is sprayed and each of them is double-reversed to drive a large number of vertical all blade water gravity turbines 11A one after another. The transport speed to the top of the specific material 3E or 2E by the specific material rising device 2F 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 as a specific material rising device 2F inside the column tube 12B. 3E is stored at the top, and is injected by Mach 1 to 3 with a specific material accelerator 6W, and acceleration of gravity acceleration while raising the degree of vacuum is made, and a vertical type moving blade specific material gravity turbine 11B power generation is produced. Energy conservation cycle coalescence engine power generation and coalescence method power generation.

The vertical all-blade ratio critical material gravity turbine 11B power generation shown in FIG. 2 has a power generation amount proportional to kg weight m / sec. The inner cylindrical blade group 60C and inner shaft device 60A and the outer cylindrical blade group 60D and outer shaft device 60B are respectively provided with optimum bearings 12C at both ends, and each is assembled and machined separately by a machine tool. Enables ultra-high-speed balance adjustment processing operation. After each processing is disassembled and precision assembling, etc., a set of vertical all-blade specific material gravity turbine 11B is manufactured by a completely new processing and assembly technology, gravity power building Ascend to 50-100 sets in accordance with the height of the 12 column pipes 12B, and store the mercury 3E etc. at the top by the column tube 12B and specific material rising device 2F. The substance mercury 3E The injection ratio critical substance 2E is mixed and injected at 2 etc., and the acceleration of gravity in the vacuum is accelerated while the degree of vacuum is higher than that of the existing steam turbine. In the process of linear acceleration of gravity acceleration, The outer blade group 60D is driven in reverse, and the specific critical material 3E speed is converted into electricity with the best theoretical theory. For example, the specific critical material 3E speed can be regenerated with the wisdom of humanity. There is a significant improvement in the existing state-of-the-art science and technology, such as the reproducibility of the 3E drop by 5-10 times with the wisdom of humanity. The power generation amount will be infinitely increased, and the world's best global warming prevention with the highest profit rate will be achieved.

  The most important configuration in the fitting assembly portion 9M of the cylindrical inner blade group 60C and inner shaft device 60A and the cylindrical outer blade group 60D and outer shaft device 60B in FIG. As precision machining, the structure and accuracy are such that the rotation balance does not change even after repeated disassembly and assembly many times, and the cylindrical inner blade group 60C and inner shaft device 60A and the outer cylindrical blade group 60D and outer shaft By inverting the device 60B, the cylindrical outer rotor blade group 60D is changed into the outer inlet blade 60e of the outer rotor blade 60d, the plurality of outer intermediate blades 60g of the outer rotor blade 60d, or the outer outlet blade 60k of the outer rotor blade 60d. In the manufacturing of 100 sets, the cylindrical inner blade group 60C is used as the inner inlet blade 60f of the inner rotor blade 60c, a plurality of inner intermediate blades 60h of the inner rotor blade 60c, and the inner outlet blade 60j of the inner rotor blade 60c. 100 production head 800m It is the most difficult, the greatest contribution in human history and ultra-precision manufacturing, such as minimizing the number of parts and almost all possible automatic production, etc. Although experimentation is necessary, the amount of power generation is increased infinitely at zero fuel cost, and the world's best prevention of global warming is achieved.

In the heat production of the solar heater 21 of FIG. 4, since air 20 ° C. becomes 160 ° C. with an adiabatic compression ratio 4, the fuel injection combustion heat exchange superheated steam 5H is produced by ultra high pressure compression such as 20 MPa, and the same fuel amount is produced. Of superheated steam 5H, the intake air temperature of the compressed air heat exchanger 2Y aiming at 10 to 100 times that of the existing boiler is maximized, and the vertical type moving blade ratio critical material gravity turbine 11B fuel cost 0 power generation extremely cheap electricity Drive to make the superheated steam 5H maximum production + liquid air 28a cooling by-product supply equipment 3D, and make the use of warm heat and prime use of cold heat, the solar heater 21 with buoyancy on the water surface or a circular railroad on the flat ground The solar heater 21 is provided with a rotation support portion 4f and a gear device 4d and a roller 4e as a floating device and a land device not shown in the drawing that maintain and rotate sunlight at right angles from east to west. , Cylindrical rotation 77G is a device that controls the vertical rotation of sunlight in the vertical direction by using buoyancy and circular rails, and controls the rotation of the west-west direction by using buoyancy and circular rails. A device that maximizes the air temperature in the 4H, collects sunlight with the largest amount of earth in a straight line by the rectangular long lens 2d, maximizes the temperature of the air 28a inside the air passage 28A equipped with the heat absorption tube 4H near the focal length, The temperature of the external air passage 28A air 28a also rises, and the entire lens material can be used as a rectangular long lens 2d extending linearly in the existing lens cross section, 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, a long long lens 2d is connected to a joint 80A + fastener 80B and the sealed upper part is set to a 4H external air passage 28A. Compressed by suction as a multistage heat pump 1G, simple multistage compressor 89B, liquid oxygen producing machine 89A, etc. as heat pump 1G, 800-1200 ° C multiple times, and recovered heat per compression by 1-multistage compressed air heat exchanger 2Y The liquid air 28a cold heat is stored in the liquid oxygen chamber 5K + the liquid nitrogen chamber 5L, and the 24-hot air steam 5H around 24 to 200 ° C. is divided and stored in the high-pressure high-temperature steam chamber 5N, and the liquid air cold heat + superheated steam heat is stored. The supply equipment 3D is used for various purposes, and the electric drive prime and the storage battery drive prime are made, and the various warm use primes and various cold use primes of the electric product are made.

  The liquid oxygen producing machine 89A in FIG. 5 uses a vertical all-blade ratio critical material gravity turbine 11B with a fuel cost of 0 power generation electric drive, compresses the air 28a heated by the solar heater 21 by ultra-high pressure, and performs compressed air heat exchange. Heat exchange is performed in the vessel 2Y, and the mass of the superheated steam 5H + liquid oxygen 5K cold + liquid nitrogen 5L is targeted for mass production, and the cylindrical inner blade group 60C and inner shaft device 60A and the cylindrical outer blade group 60D and outer shaft device 60B. Bearings 12C are provided at the optimum positions at both ends, and both ends can be held and precisely processed by machine tools after assembling separately, ultra-high speed rotation balance adjustment processing is enabled, and the inner shaft device 60A and inner compression blade 8q and inner output are provided. As a manufacturing balance adjustment process for the blade 8s, the outer shaft device 60B, the outer compression blade 8r, and the outer output blade 8t, the assembly of the inner shaft device 60A and the outer shaft device 60B can be performed at a very high speed. In the production of liquid oxygen 5K + liquid nitrogen 5L + superheated steam 5H, the compressed air heat exchanger 2Y is used, and the air 28a heated by the solar heater 21 in FIG. 4 is heat-exchanged by the long compressed air heat exchanger 2Y to produce the superheated steam 5H. + Mass production of low temperature ultra high pressure compressed air 28a by rectifying tower exhaust gas cooling, air 28a in the process of adiabatic linear expansion, the outer output blades 8t and the inner output blades 8s are double-reversed, and the major material ratio of the vertical blades Gravity turbine 11B Fuel cost 0 Power generation Extremely cheap Electricity As a drive with very little electricity, it is the prime use of isothermal heat that recovers methane injected into methane hydrate by mass production of superheated steam 5H, liquid oxygen 5K and liquid nitrogen 5L are for fuel combustion By using it for various engines equipped with ultrahigh pressure combustion parts such as 21/60000 and 79/60000, it is possible to drive various airplanes, ships, automobiles, etc. To high-speed jet propulsion drive, to liquid oxygen making machine 89A.

A simple multistage compressor 89B shown in FIG. 6 is connected to various engines to produce ultra-high pressure compressed air 28a. The cylindrical inner blade group 60C and inner shaft device 60A and the cylindrical outer blade group 60D and outer shaft device are used. The bearings 12C are provided at the optimum positions on both ends of each of the 60B, and both ends can be precisely processed by a machine tool after assembling separately, and ultra-high speed rotation balance adjustment processing is enabled, the inner shaft device 60A and the inner compression blade 8q, A plurality of outer shaft devices 60B and outer compression blades 8r are manufactured and balance-adjusted, and each is assembled into a super-high-speed double reversal of the inner shaft device 60A and the outer shaft device 60B. A simple multi-stage compressor 89 for producing high-pressure compressed air 28a at an optimum temperature by compressing the air 28a with ultra-high pressure and using the compressed air heat exchanger 2Y to produce heat exchange superheated steam 5H, such as twice compression or three times compression. Connected to various engines to drive a liquid oxygen production machine 89A, a simple gas engine 89C, a simple air injection engine 89D, a simple injection engine 89E, etc. A simple multi-stage compressor 89B including a micro ultra-high speed simple multi-stage compressor 89B is used for various rotational drives and ultra-high-speed jet propulsion drives.

The simple gas engine 89C in FIG. 7 uses the compressed air heat exchanger 2Y to produce superheated steam 5H as combustion heat exchange in an ultra-high pressure environment, and produces the same amount of superheated steam 5H around 13 to 20 times that of an existing boiler. The superheated steam 5H is used to expand and drive the entire rotor blade steam turbine 11 of the previous application to a vacuum, aiming for a power generation amount 20 times that of the existing thermal power generation, and the simple gas engine 89C rotates 10 times the existing gas turbine by all the rotor blades. As the output +10 times propulsion propulsion output, etc., the cylinder inner rotor blade group 60C and inner shaft device 60A and the cylindrical outer rotor blade group 60D and outer shaft device 60B are provided. It is possible to perform both-end holding precision machining with a machine tool later, ultra-high-speed rotation balance adjustment processing, inner shaft device 60A and inner compression blade 8q, inner output blade 8s, outer shaft device 60B and outer compression blade 8 As a manufacturing balance adjustment process of r and the outer output blade 8t, the superassembly of the inner shaft device 60A and the outer shaft device 60B is carried out by this assembly, and the superheated steam 5H is produced with the same fuel amount. Aiming to double, as superheated steam 5H production of compressed air heat exchanger 2Y, fuel injection combustion to superhigh pressure compressed air 28a + superheated steam 5H production Simple gas engine 89C drive, vertical type moving blade ratio critical material gravity turbine 11B power generation electric In the process of using the long compressed air heat exchanger 2Y with the inlet closed, including product driving, liquid oxygen 5H and liquid nitrogen 5L are injected from the oxygen nitrogen injection nozzle 6M, and fuel injection combustion is performed from the fuel injection nozzle 6X. In the mass production of superheated steam 5H combined with normal combustion, as the all blade blade turbine driven thermal power generation, etc., in the thermal power generation, the air 28 heated by the solar heater 21 in FIG. Compressed fuel injection combustion, heat exchange with the long compressed air heat exchanger 2Y, the theoretical air-fuel ratio combustion to 4 times the combustion amount of the existing gas turbine, super high pressure combustion to aim the production amount of superheated steam 5H 10 times that of the existing boiler For power generation, when liquid oxygen 5K or liquid nitrogen 5L is used for fuel combustion, the compression work rate is set to various engines equipped with ultra-high pressure combustion parts such as 21/60000 and 79/60000, and the same fuel amount is 10 times that of existing ones. A simple gas engine 89C is used for power generation, airplanes, ships, automobiles, etc., aiming for power generation, 10 times speed and 1/10 fuel cost, and various rotational driving and ultra-high speed injection propulsion driving.

The simple air injection engine 89D of FIG. 8 includes 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, and is assembled separately. It is possible to perform both-end holding precision machining with a machine tool later, ultra-high-speed rotational balance adjustment processing, inner shaft device 60A and inner compression blade 8q and inner output blade 8s, outer shaft device 60B and outer compression blade 8r and outer output. As the manufacturing balance adjustment process of the blade 8t, the main assembly makes the ultra-high-speed counter-rotating air compression of the inner shaft device 60A and the outer shaft device 60B, and the target amount is 10 times that of the existing boiler. As superheated steam 5H production of air heat exchanger 2Y, fuel injection combustion + superheated steam 5H production simple air injection engine 89D drive to ultrahigh pressure compressed air 28a, ultrahigh pressure compressed air 28a quality In the process of increasing fuel injection combustion, generating rotational output + superheated steam 5H into the production rocket outer box 77B, and in the process of aiming for 10 times speed by air suction injection, air suction injection is also performed from the outer periphery, and vertical full motion Including the blade ratio critical material gravity turbine 11B power generation electrical product drive, the inlet is closed in the process of using the long compressed air heat exchanger 2Y, liquid oxygen 5H and liquid nitrogen 5L are injected from the oxygen nitrogen injection nozzle 6M, Fuel injection combustion from the fuel injection nozzle 6X, mass production of superheated steam 5H combined with normal combustion, mass production of superheated steam 5H with the theoretical air-fuel ratio combustion even with normal combustion and four times the normal combustion amount, and liquid oxygen 5K And 5L of liquid nitrogen is used for fuel combustion, has a compression work rate of 21/60000 and 79/60000, etc., and has an ultra-high pressure combustion part, aiming for 10 times speed and 1/10 fuel cost, super high speed for ships etc. To injection propulsion drive, to simplify air injection engine 89D.

The simple injection engine 89E of FIG. 9 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, respectively, and is assembled separately. The machine tool enables both-end holding precision machining, ultra-high speed rotation balance adjustment machining, inner shaft device 60A, inner compression blade 8q, inner output blade 8s, outer shaft device 60B, outer compression blade 8r, and outer output blade. 8t production balance adjustment processing, this assembly will make the ultra-high speed counter-rotating air compression of the inner shaft device 60A and the outer shaft device 60B, the compressed air aiming 10 times the amount of superheated steam 5H production amount with the same fuel amount As superheated steam 5H production of heat exchanger 2Y, fuel injection combustion to superhigh pressure compressed air 28a + superheated steam 5H production Simple injection engine 89E drive, supermass high pressure compressed air 28a mass increase Rotating power generation + superheated steam 5H is injected into the rocket outer box 77B for injection injection combustion, and a large compression including a vertical full blade ratio material gravity turbine 11B power generation electric product drive In the process of using the air heat exchanger 2Y, the inlet is closed, liquid oxygen 5H or liquid nitrogen 5L is injected from the oxygen nitrogen injection nozzle 6M, fuel injection combustion is performed from the fuel injection nozzle 6X, and a large amount of superheated steam 5H combined with normal combustion As the production, the mass production of the combustion of the superheated steam 5H, which is four times the normal combustion ratio of the theoretical air-fuel ratio combustion in the normal combustion, and the liquid oxygen 5K and the liquid nitrogen 5L are used for fuel combustion, and the compression work rate is 21/60000. Use simple injection engine 89E with ultra-high pressure combustion part such as 79/60000, aiming for 10 times speed and 1/10 fuel cost, turning airplane or ship to rotational drive or ultra-high speed injection propulsion drive

The simple gas engine vehicle 89F in FIG. 10 is driven by the simple gas engine 89C, which is an improved invention of the existing micro gas turbine vehicle, and requires experimentation, but the amount of superheated steam 5H produced is 10 times that of the existing boiler, or the total moving blade + superheated steam 5H As a simple gas engine 89C power generation aiming at 10 times the output of the existing gas turbine as production and the same fuel amount as 10 times the existing thermal power generation, in the simple gas engine 89C, normal air compression fuel injection combustion and liquid oxygen liquid nitrogen Fuel injection combustion is performed in compression injection, superheated steam 5H is produced at 30MPa, respectively, and combustion gas 49 is sucked and injected at each, and the generator 1 is used as a 10 times rotational output of an existing micro gas turbine with the same fuel amount. Drive and store electricity in the storage battery 1A, rotate the storage battery driving wheel 4J to normal vehicle operation, and aim for 1/10 of the existing vehicle with a simple gas machine The automobile 89F, to the preeminent world of global warming prevention operating profit margin by bus or taxi.

The simple gas engine ship 89G shown in FIG. 11 needs to be tested as a simple gas engine 89C driven ship that is an improved invention of the existing gas turbine ship, but the amount of superheated steam 5H produced is 10 times that of the existing boiler, or the total moving blade + superheated steam. 5H production is a simple gas engine 89C with 10 times the rotational output of the existing gas turbine, and fuel injection combustion is performed in normal air compression fuel injection combustion and compression injection of liquid oxygen liquid nitrogen, respectively, and superheated steam 5H is produced at 30 MPa or more, respectively. High-speed injection, suction and injection of each combustion gas 49 and drive the simple gas engine 89C to drive the screw 7C, the exhaust gas is injected at ultra-high speed to generate propulsion force, air suction injection at the outer periphery, the same fuel amount existing As the gas turbine's 10 times rotation output + 10 times injection propulsion output, etc., the flat sea is made to be super high speed injection propulsion beyond the air flotation superheated steam flotation airplane and approach, and the same fuel By close to 10 times the degree of existing vessels, the operating profit margin of simple gas engine ship 89G to the preeminent world of global warming prevention.

The simple gas engine airplane 89H in FIG. 12 is a simple gas engine 89C driven airplane that is an improved invention of the existing turbo flop engine, and requires experimentation, but the amount of superheated steam 5H produced is 10 times that of the existing boiler, or the total moving blade + superheated steam 5H production is a simple gas engine 89C with 10 times rotational output or 10 times injection propulsion output of an existing gas turbine, and fuel injection combustion is performed for normal air compression fuel injection combustion and liquid oxygen liquid nitrogen compression injection, respectively, and superheated steam, respectively. 5H is manufactured at a high speed of 30 MPa, etc., each combustion gas 49 is sucked and injected, the simple gas engine 89C is driven by the driving propeller 7A, the exhaust is injected at a high speed to generate a propulsive force, and the same fuel amount Produces superheated steam 5H by normal air-compressed fuel-injection combustion when flying in the atmosphere as 10 times rotation output + 10 times injection propulsion output of an existing turbo flop engine The combustion gas 49 is compressed and injected with 30MPa superheated steam 5H and compressed and linearly expanded with a 30MPa superheated steam 5H. By making exhaust injection, the space arrival cost is 1 / 500,000, etc., and the space arrival cost is about the same as the existing airplane, making the operating profit rate of the simple gas engine airplane 89H the world's best global warming prevention.

The simple air-injection engine ship 89I in FIG. 13 is a modified air-injection engine 89D-driven ship that is an improved invention of the existing gas turbine ship, and requires experimentation, but the amount of superheated steam 5H produced is 10 times that of the existing boiler, As superheated steam 5H production, a simple air injection engine 89D with 10 times rotational output and 10 times injection propulsion output of an existing gas turbine is used, and fuel injection combustion is used for normal air compression fuel injection combustion and liquid oxygen liquid nitrogen compression injection, respectively. The superheated steam 5H is injected into the rocket outer box 77B at a manufacturing pressure of 30 MPa, etc., and the front air 28a is injected into the bottom of the suction ship, and the outer periphery is again propelled about 10 times as much as the existing gas turbine ship. After the simple air injection engine 89D is rotationally driven with the combustion gas 49, the air in front of the exhaust injection is sucked and injected, and the same fuel amount is injected 10 times that of the existing gas turbine ship. A simple air-injection engine ship 89I, aiming at over 10 times the speed of the existing ship with the same fuel amount by propelling over the flat sea with combustion gas 49 levitation + superheated steam 5H levitation plane over and close approach Is the world's best global warming prevention.

The simple injection engine airplane 89J in FIG. 14 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 10 times that of the existing boiler, or the total moving blade + superheated steam 5H As a manufacture, a simple injection engine 89E having a 10 times rotational output or 10 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, and superheated steam 5H Is injected into the outer rocket box 77B at 30MPa, etc., and the forward air 28a is propelled about 10 times as much as that of the existing suction jet, and the simple injection engine 89E is driven to rotate by the respective combustion gases 49 before the exhaust injection forward. Air is sucked and injected, with the same fuel amount as 10x injection propulsion output of existing jets, combustion gas 49 + superheated steam 5H super high speed injection propulsion, large During the flight, the superheated steam 5H is produced and stored in a normal air-compressed fuel injection combustion, and compression and fuel injection combustion of liquid oxygen liquid nitrogen fuel 30MPa and the like from the vicinity of the highest flight altitude is usually performed. By using the superheated steam 5H for 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, making the operating profit rate of the simple injection engine airplane 89J the best in the world Prevent global warming.

The rotary wing airplane 89K in FIG. 15 is a simple gas engine 89C driven airplane that is an improved invention of the existing helicopter and requires experimentation, but the production amount of superheated steam 5H is 10 times that of the existing boiler, or the production of all rotor blades + superheated steam 5H. A simple gas engine 89C with 10 times rotational output and 10 times injection propulsion output of an existing gas turbine is used to produce superheated steam 5H by fuel injection combustion in normal air compression fuel injection combustion and liquid oxygen liquid nitrogen compression injection, respectively. Super-high-speed injection at 30 MPa, etc., each combustion gas 49 is sucked and injected, the simple gas engine 89C is driven for linear expansion, its exhaust is injected at high speed to generate propulsion, and the same fuel amount of the existing helicopter 10 The rotary blade 7B is driven to rotate with the aim of doubling the rotation output. When flying in the atmosphere, the superheated steam 5H is produced and stored and increased by the normal air-compressed fuel injection combustion. Combustion compression and fuel injection combustion of liquid oxygen liquid nitrogen fuel 30MPa etc. from near, and the combustion gas 49 exhaust gas is suction injection linear expansion with 30MPa superheated steam 5H, simple gas engine 89C drive linear exhaust injection, space arrival cost By setting the cost to reach space to 1 / 500,000, the same as the existing airplane, the operating profit rate of the rotary wing airplane 89K will be the best global warming prevention in the world.

The rotor-blade jet airplane 89L in FIG. 16 is an airplane driven by a simple injection engine 89E, which is an improved invention of an existing helicopter, and requires experimentation, but the amount of superheated steam 5H produced is 10 times that of an existing boiler, or all rotor blades + superheated steam 5H are produced. As a simple injection engine 89E with 10 times rotational output or 10 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. Injected into the rocket outer box 77B at a production of 30 MPa, etc., the upper air 28a and the combustion gas 49 are propelled by about 10 times that of the existing jet jet, and the simple injection engine 89E is rotated by each combustion gas 49 to rotate. After driving the blades 7B, the air above the exhaust injection and the combustion gas 49 are sucked and injected, and the same fuel amount as the target of 10 times injection propulsion output of the combustion gas 4 + Superheated steam 5H super-high speed injection propulsion, when flying in the atmosphere, increase the production and storage of superheated steam 5H by normal air compression fuel injection combustion, compression of liquid oxygen liquid nitrogen fuel 30MPa etc. from the vicinity of the normal maximum flight altitude The fuel injection combustion is performed, and the combustion gas 49 is changed to suction injection linear expansion exhaust injection with 30 MPa superheated steam 5H, the space arrival cost is reduced to 1 / 500,000, etc., and the space arrival cost is reduced to the existing airplane fuel cost. Make the operating profit rate of the wing jet airplane 89L the world's best global warming prevention.

The oversized Osprey 89M in FIG. 17 is an airplane driven by the simple injection engine 89E of the improved invention of the existing Osprey and requires experimentation, but the production amount of superheated steam 5H is 10 times that of the existing boiler, A simple injection engine 89E with 10 times rotational output and 10 times injection propulsion output of an existing gas turbine is used to produce superheated steam 5H by performing fuel injection combustion in normal air compression fuel injection combustion and liquid oxygen liquid nitrogen compression injection, respectively. Is injected into the outer casing 77B of the rocket, and the upper air 28a and the combustion gas 49 are propelled about 10 times as much as the existing jets of suction injection, and the simple injection engine 89E is rotated by each combustion gas 49 linear injection, and the propeller After driving 7A, the air above the exhaust injection and the combustion gas 49 are sucked and injected, and the same fuel amount is burned as the target of 10 times the injection propulsion output of the existing jet 49+ superheated steam 5H super-high-speed injection propulsion, superheated steam 5H is produced and increased by normal air compressed fuel injection combustion when flying in the atmosphere, and usually compressed by liquid oxygen liquid nitrogen fuel 30MPa etc. from around the highest flight altitude By making the combustion gas 49 into a suction injection linear expansion exhaust injection with 30 MPa 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, The operating profit rate of the rotary wing jet airplane 89L will be the world's best global warming prevention.

The large Osprey 89N shown in FIG. 18 is a simple gas engine 89C driven airplane that is an improved invention of the existing Osprey, and requires experimentation, but the production amount of superheated steam 5H is 10 times that of the existing boiler, A simple gas engine 89C with 10 times rotational output or 10 times injection propulsion output of an existing gas turbine is used to produce superheated steam 5H by performing fuel injection combustion in normal air compression fuel injection combustion and liquid oxygen liquid nitrogen compression injection, respectively. Etc., each of the combustion gases 49 is sucked and injected, the simple gas engine 89C is driven for linear expansion, its exhaust is injected at a high speed to generate an injection propulsion output, and the same fuel amount of the existing helicopter 10 The propeller 7A is driven to rotate with the aim of double-rotation output. When flying in the atmosphere, the superheated steam 5H is produced and stored and increased by normal air-compressed fuel injection combustion. Combustion and fuel injection combustion of liquid oxygen liquid nitrogen fuel 30MPa and the like from around the row altitude, the combustion gas 49 exhaust is made into a suction injection linear expansion with 30MPa superheated steam 5H, a simple gas engine 89C drive linear exhaust injection is made, By setting the arrival cost to 1 / 500,000 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.

Since there is no improvement in the existing pumped-storage power generation for a long time, water injection speed Mach 3 etc. added + gravity acceleration added in vacuum + drop infinite additional power generation, vertical type moving blade specific material gravity turbine 11B power generation, existing pumped water In comparison with power generation, in the power generation part of pumped-storage power generation, gravity acceleration + head in vacuum is added to the water jet speed Mach 3 etc. of the water jet processing machine, and the power generation part also has a work load kg weight m / sec. × In proportion to the drop, there is a possibility that the amount of power generation with zero fuel cost will increase indefinitely, such as 10 to 100 times. There is a possibility to prevent global warming in the world.

Boilers for existing thermal power generation have not been improved for a long time, and the air temperature after adiabatic compression at 20 ° C has increased to 82 ° C at a compression ratio of 2 and 160 ° C at a compression ratio of 4. If there is little, the production amount of superheated steam 5H in the compressed air heat exchanger 2Y of the present invention, such as fuel injection combustion 20MPa, may increase 10 to 20 times, and the world's thermal power generation All boilers generate electricity as a compressed air heat exchanger 2Y, with simple gas engine 89C power generation, total replacement of thermal power generation in the world to the same fuel amount 10 to 20 times, and the world's highest profit rate There is a possibility of prevention.

In addition to the production of superheated steam 5H, the existing gas turbine is equipped with half of the stationary blades and moving blades alternately, and the compressor uses the stationary blades to dam the compressed air and repeatedly changes the direction, and the turbine generates combustion gas. Since the vane expansion is repeated without changing the direction of damming with the stationary blade, the rotation output and the jet propulsion output are set to 1/10 to 1/100, etc., so that the stationary blade is the cylindrical outer blade group 60D and the inner cylindrical blade group 60C. With a simple gas engine 89C, a simple air injection engine 89D, a simple injection engine 89E, etc., which are double-reversed, the rotational output and the injection propulsion output are brought close to 100 times in the manufacture of the compressed air heat exchanger 2Y superheated steam 5H In addition, a vertical all-blade ratio critical material gravity turbine 11B power generation electric product drive is added to use solar heater 21 superheated steam 5H thermal production by-product liquid oxygen 5K + liquid nitrogen 5L, air volume There is a possibility of driving the simple gas engine 89C, the simple air injection engine 89D and the simple injection engine 89E with a reduction work rate of 21/60000 + 79/60000 volumetric compression work rate, and in the automobile, CO2 exhaust and fuel costs may be brought close to 1/10. There is a possibility that ships may approach the speed of 10 times with the same fuel cost, airplanes will reach the space cost of 1 / 500,000, etc., as a prime use of space to take a day trip anywhere on earth to prevent global warming, etc. There is also the possibility of making a major revolution in the use of hot and cold heat.

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 is air temperature and compressed multiple times with heat pump (various air compressors) 2C 1K: Liquid fuel control valve, 1L: Fuel heating pipe, 1Q: On-off valve, 1Y: Multistage combustion chamber, 1b: Fuel (liquid fuel + liquefiable gas) 2X2Y2Z Fuel) 1b: Fuel pipe (provided so that the fuel injection temperature becomes the optimum temperature) 1c: Liquid fuel, 1d: Mercury, 1g: Gravity accelerating unit, 1h: Horizontal shaft (outer shaft device and inner 2) Sunlight heater (collects sunlight in a straight line with a long lens and heats the high-temperature portion forming intake air) 2a: Speeds up the natural phenomenon (change in air is almost zero) When the leftovers move to a nearby river, a huge amount of microorganisms that approaches zero overnight will be used to increase food for humans. Equipment that increases the supply of nutrients such as nitrogen, oxygen, and CO2 and increases foods such as fish and kombu. 2a: Speeds up natural phenomena (in ships, the supply of nutrients such as nitrogen, oxygen, and CO2 into the sea makes it possible to digest microorganisms. Phytoplankton, seaweed, etc. aiming for tens of thousands of forests, increasing food for fish such as fish and kombu by increasing the food chain, etc. 2b: Low water resistance (by injecting air, combustion gas, superheated steam, etc. at the bottom of the ship at high speed) Minimize water resistance ) 2c: heat insulating material, 2d: long lens (convex lens cross-section extended into a straight line, a plurality of uses aiming at the shortest focal length lens width) 2e: water surface, 2g: specific material acceleration direction, 2A: heat-resistant material, 2B : Heat absorbing material, 2C: 1 to multi-stage compression heat recovery device (heat energy is air temperature, heat recovery is performed multiple times with a heat pump multiple times with a compression heat exchanger, and the remainder is divided and stored as warm 50 + liquid cold 28a) 2E : Specific material (including alloy, platinum sphere, gold sphere, tungsten alloy powder sintered sphere, silver sphere, copper sphere, tin sphere, lead sphere, zinc sphere, aluminum sphere, indium, cadmium, gallium, thallium, bismuth, etc. Substance) 2E: Specific critical substance (Since the manufacturing method reduces 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 pulverization air cooling water cooling) 2E: Specific critical substance (Siri Covered 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 substance elevating device (gravity energy is increased and stored) 2H: Cold seawater mixer, 2X: Air heat exchanger 2Y: Compressed air heat exchanger (liquid air cold heat + 2Z: Specific heat exchanger (used for temperature control of liquid metal below 500 degrees) 3a: Water repellent plating, 3i: Simple multistage compressor, 3s: Simple compressor, 3u: Turbine, 3A: Water repellent coating, 3B: Water pressure reciprocating engine, 3D: Electricity + liquid air cold heat + superheated steam heat supply equipment (cooling + heat production with gravity power generation electricity, supplying liquid oxygen and liquid nitrogen Car, ship and flight Methane is injected into the methane hydrate supplied with overheated steam or superheated steam, etc. Recovery of methane, etc. Electricity + cold heat + warm use intensive 3E: Specific critical substances (specific critical liquid substances such as mercury and water at room temperature) 3E: Specific critical substances ( 3F: oxygen pressure reciprocating engine, 3G: theoretical combustion gear engine, 3H: reciprocating piston, 3J: theoretical combustion reciprocating engine, 3K: external gear 3L: multistage combustion chamber 3M: Steam pressure reciprocating engine, 3N: Steam pressure gear engine 3P: Theoretical expansion engine (the gas volume is the inversely proportional to the pressure, the best engine + oxygen hydrogen increase combustion aim) 3Q: Theoretical expansion engine (Best by Boyle's law) 3R: Theoretical gas turbine (theoretical best gas turbine whose gas volume is inversely proportional to the pressure) 3S: Theoretical steam turbine (the gas volume is pressure) 3T: Theoretical gas compressor (Theoretical best gas compressor whose gas volume is inversely proportional to the pressure) 3U: Theoretical turbine, 3V: Pump engine (Use existing pumps in the engine) 3X: Compressor engine (uses various existing compressors in the engine) 3Y: Counter-reversal engine (engine whose gas volume is inversely proportional to pressure) 3Z: Oxygen pressure gear engine, 3a: Water repellent plating, 3b: Water repellent Coating, 4F: Combustion gas reciprocating engine, 4H: Heat absorption tube (The long lens 2d collects sunlight into the heat absorption tube in a straight line, and the air temperature inside the tube is heated to the maximum to increase the outside air temperature) 4J: Battery drive wheel, 4K: Theoretical expansion engine vehicle, 4Q: Theoretical combustion chamber (theoretical air-fuel ratio combustion in the superheated steam production, the combustion chamber aiming at 20 times pressure superheated steam injection, etc.), 4W: Theoretical compression 4Y: Theoretical combustion chamber (combustion chamber for high-temperature pyrolysis electrolysis combustion of water by steam in steam) 0Z: Combustion gas gear engine, 4X: Turbine blade cross section (increase cross-sectional area and 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 suction Air path, 5d: Combustion flow inner wall, 5e: Ultra high pressure oxygen, 5h: Rectification tower exhaust gas, 5h: Rectification tower exhaust pipe, 5A: Supply valve, 5B: Cooling fin, 5C: Exhaust chamber, 5D: Exhaust valve 5E: Air supply chamber, 5F: Oxygen heating tube, 5G: Steam heating tube, 5G: High pressure high temperature water heating tube, 5H: Superheated steam, 5H: High pressure high temperature superheated steam tube, 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, 6C: Combustion gas water vapor nozzle, 6E: Specific critical material injection Nozzle, 6F: Water injection nozzle, 6G: Stator blade, 6H: Drain pipe, 6L: Oxygen injection nozzle, 6M: Oxygen nitrogen injection nozzle, 6W: Specific critical material accelerator (Liquid specific material 3E pressure and specific gravity difference 6X: Fuel injection nozzle, 6X: After burner (combustion of the fuel injection cold heat 28a and the combustion flow 6Y into the suction air flow, and the increase in the amount of fuel combustion increases the universe. 6Y: Combustion gas injection nozzle (cooling 28a combustion flow) 6Z: Superheated steam injection nozzle, 7A: Propeller, 7B: Rotary blade, 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: Rotary wing injection airplane, 7P: Extra large osprey, 7Q: Large osprey, 8a: Turbine wing (cycle number and specific gravity) Large material properties Turbine blades with angle, curve and rotational radius double reversal according to work speed and peripheral speed 8c: Turbine blades (inner and outer rotor blade groups are fitted to the inner and outer shaft device cylinders respectively) 8d: upper expansion blade group, 8e: lower expansion blade group, 8f: assembly turbine blade group, 8g: upper compression blade group, h: Lower compression blade group, 8j: Assembly compression blade group, 8k: Inner compression blade, 8m: Outer compression blade, 8n: Inner output blade, 8p: Outer output blade, 8q: Inner compression blade (rotational speed and peripheral speed) 8r: Outer compression blade (compression blade with angle, curve and rotation radius doubly reversed according to rotational speed and peripheral speed) 8s: Inner output blade (An output blade with an angle, a curve, and a rotational radius double reversal according to the rotational speed and peripheral speed) 8t: Outer output blade (an output blade with an angle, a curve, and a rotational radius double according to the rotational speed and the peripheral speed) 8B: Horizontal all-blade hydrogravity turbine, 8C: Horizontal all-blade specific material gravity turbine, 8D: Horizontal all-blade water gravity turbine, 8E: Horizontal all-blade material gravity turbine, 8V: All-type turbine Rotor Water Gravity Turbine, 8W Bin, 8X: Vertical all blade hydrogravity turbine, 8Y: Vertical all blade specific material gravity turbine, 9: Wear resistant annular assembly 9b: Upper attractive lower repulsion magnet 9A: Cylindrical ring assembly (wear resistant cylindrical ring assembly blade group turbine blade (8a) 6 types 6 types for reverse rotation, simple structure and few parts 9A: Cylindrical ring assembly (outer inlet blade 60e + outer intermediate blade 60g + outer outlet blade 60k is fitted to form outer rotor blade 60d, inner inlet blade 60f + inner 9B: Repulsive permanent magnet, 9C: Suction permanent magnet, 9D: Compressed air part, 9E: Vacuum part, 9M: Fitting assembly part, Intermediate blade 60h + Inner outlet blade 60j 9Q: Vertical parallel plate (preserves blast air 10: hull, 10A: cabin, 10b: cockpit, 10c: control room, 10d: cabin, 10e: cargo compartment, 11: full-blade steam turbine, 11A: vertical full motion Blade Water Gravity Turbine, 11B: Vertical Type Whole Blade Ratio Material Gravity Turbine, 11C: Horizontal Type Whole Blade Water Gravity Turbine, 11D: Gas Cooling Chamber, 11E: Horizontal Type Whole Blade Ratio Material Gravity Turbine, 12: Gravity Power generation building, 12A: Steel frame, 12B: Column tube, 12C: Bearing, 12D: Square flange, 16B: Vertical shaft, 21: Solar heater (mainly used with the intake air path provided in the heat absorption tube 4H) 24) Combustion gas control valve, 24A: Compressed air control valve, 24B: Liquid oxygen control valve, 24C: Liquid nitrogen control valve, 24D: Oxygen control valve, 24E: Nitrogen control valve, 25: Superheated steam control valve, 25 : Fuel control valve, 25c: Fuel pipe, 28a: Air, 28a: Cold heat (compressed air 28a is compressed with a heat pump and compressed air is heated to 50 warm heat + compressed air 28a cold containing liquid oxygen and liquid nitrogen) 28b: Calorific value of compressed air, 28A: Intake air passage, 28B: Air passage inlet, 38: Rotation guide, 38a: Flight trunk, 38b: Flight wing, 38c: Flight tail, 38d: Vertical wing, 38e: Wing leading edge 38H: Air suction jet ship (with 79S79T79Y79Z) 38C: Water suction jet ship (with 79U79X) 38H: Theoretical screw ship, 38J: Theoretical jet ship, 38T: Theoretical jet airplane, 38U: theoretical propeller airplane, 39A: solar thermal gravity airplane, 39B: solar thermal gravity rotating airplane, 39C: solar thermal gravity helicopter , 39D: screw ship, 39G: solar thermal gravity ship, 39H: oxygen coalescence screw ship, 39J: oxygen coalescence injection ship, 39K: oxygen coalescence screw injection ship, 39L: oxygen coalescence jet airplane, 39M: oxygen coalescence propeller airplane, 39N: oxygen coalescence propeller jet plane, 39P: oxygen coalescence rotorcraft, 39Q: oxygen coalescence screw ship, 39R: oxygen coalescence jet ship, 39S: oxygen coalescence screw jet ship, 39T: oxygen coalescence jet airplane, 39U: oxygen coalescence propeller Airplane, 40A: Rudder, 49: Combustion gas, 50: Superheated steam, 50: Superheated steam chamber, 50: Heat (compressed air 28a with a heat pump and divided into 50 heat of compressed air calorie heat + compressed air 28a cold) 50A: Water vapor, 50a: Superheated steam injection pipe, 51: Empty Extractor 51: Combined extractor (extractor for joining) 51A: Air extraction chamber 52a: Hot water 52a: Deep sea water 52b: Hot water 52d: Hot (change from 50) 52e: Cold (28a) 55B: Transmission, 60: Cylindrical blade group, 60A: Inner shaft device (equipment with turbine blades) 60B: Outer shaft device (equipment with turbine blades) 60C: Cylindrical inner blade group (wear-resistant cylindrical annular assembly) 60D: Cylindrical outer rotor blade group (Wear resistant cylindrical annular assembly including fixed rotor blade group facilitates easy assembly) 60E: Outlet fixed outside Blade (inlet blade for annular assembly fixing outer rotor blade group) 60F: inlet fixed inner blade (inlet blade for annular assembly fixing inner rotor blade group) 60G: outer annular blade (intermediate blade for annular assembly of outer rotor blade group) 60H: Inner ring Blade (intermediate blade for annular assembly of inner blade group) 60J: Outlet fixed outer blade (exit blade for annular assembly fixing outer blade group) 60K: Outlet fixed inner blade (exit blade for annular assembly fixing of inner blade group) ) 60c: inner blade, 60d: outer blade, 60e: outer inlet blade, 60f: inner inlet blade, 60g: outer intermediate blade, 60h: inner intermediate blade, 60j: inner outlet blade, 60k: outer outlet blade, 76 : Gear device (including magnetic frictional power transmission device) 77B: Rocket outer box, 77C: Counter-rotating machine outer box, 77F: Injection section outer box, 77G: Cylindrical rotating section, 77a: Turbine outer box, 77b: Compressor Outer box, 80: Bearing (including magnetic bearing + air bearing) 80a: Thrust bearing (including magnetic bearing + air bearing) 80A: Joint, 80B: Fastener, 80Y: Liquid air suction water jet (high pressure high temperature combustion chamber 5M high pressure High temperature steam room 5N Received and injected and burned multiple times at 5M and heated and injected 5N multiple times from the inner and outer peripheries, sucked and injected by air suction and injected) 80Z: Liquid air suction water jet (high pressure and high temperature) Combustion chamber 5M Receives high-pressure high-temperature steam chamber 5N, and injects and burns fuel 5M multiple times and heats and injects 5N multiple times from the inner and outer peripheries. 84: Counter-rotating magnetic friction device (device that rotates the inner rotor blade group and the outer rotor blade group at the same speed in the opposite direction) 84Y: Counter-rotating Gear device (device that double-reverses with existing technology) 85: Double-reverse magnetic device (magnet-utilized gear height is slight to non-contact and reciprocally rotates with a horizontal shaft 1h gear) 85Y: Double-reverse gear device (existing (Reverse rotation by 1h gear on the horizontal axis) 8p: Liquid oxygen production machine, 88q: Simple gas engine, 88r: Simple air injection engine, 88s: Simple injection engine, 88A: Oxygen combined air injection unit (rocket combined with jet combustion + steam injection, etc.) 88B: Oxygen Combined air injection unit (ultra-high pressure rocket combustion + jet combustion + superheated steam injection suction) 88C: theoretical air injection unit, 88M: theoretical water injection unit, 88K: oxygen combined water injection unit (rocket combustion + jet combustion + water vapor injection, etc. 88L: oxygen combined water injection unit (super high pressure rocket combustion + jet combustion + superheated steam injection suction) 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 vehicle, 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, 95a: combustion gas reservoir, 95b: compressed air reservoir, 95c: Superheated steam reservoir, 103: Cold heat recovery device,

Claims (153)

  Various energy storage cycle coalescence engine and coalescence method as part of vertical type moving blade specific material gravity turbine (11B) specific material riser (2F) and gravity power generation building (12).   Various types of energy storage cycle coalescence engine and coalescence method using a vertical all-blade ratio critical material gravity turbine (11B) specific material riser (2F) and a column tube (12B) of a gravity power generation building (12).   Various energy storage cycle coalescence engine and coalescence method as pillars of vertical material moving blade ratio critical material gravity turbine (11B) specific material lift device (2F) and gravity power generation building (12).   Various energy storage cycle coalescence engine and coalescence method as the core of vertical type moving blade specific material gravity turbine (11B) specific material riser (2F) and gravity power generation building (12).   Various types of energy storage cycle coalescing engines having a rectangular pipe (12B) and a square flange (12D) of a vertical type moving blade ratio critical material gravity turbine (11B) specific material rising device (2F) and gravity power generation building (12), and Merge method.   Vertical type rotor blade specific material gravity turbine (11B) specific material riser (2F) and gravity power generation building (12) column tube (12B) square flange (12D) is fixed to steel frame (12A) as square Various energy storage cycle coalescence engines and coalescence methods.   Vertical type blade blade critical material gravity turbine (11B) specific material riser (2F) and gravity power generation building (12) column tube (12B) square flange (12D) is square and bolted to steel frame (12A) Various energy storage cycle coalescence engines and coalescence methods.   Vertical type moving blade ratio critical material gravity turbine (11B) ratio critical material riser (2F) and gravity power generation building (12) column tube (12B) square flange (12D) squared and fixed to steel frame (12A) top and bottom Various energy storage cycle coalescence engines and coalescence methods.   Vertical type moving blade specific material gravity turbine (11B) specific material riser (2F) / gravity power generation building (12) column tube (12B) square flange (12D) square and steel frame (12A) up and down bolt Various tightened energy conservation cycle coalescence engines and coalescence methods.   Vertical type moving blade specific material gravity turbine (11B) specific material riser (2F) and gravity power generation building (12) column tube (12B) square flange (12D) square steel frame (12A) upper and lower bolts Various energy storage cycle coalescence engines and coalescence methods that increase the number of floors by tightening.   Vertical type moving blade specific material gravity turbine (11B) specific material riser (2F) and gravity power generation building (12) column tube (12B) square flange (12D) square steel frame (12A) upper and lower bolts Various energy conservation cycle coalescing engines and coalescence methods with floors of 10 or more.   Vertical type moving blade specific material gravity turbine (11B) specific material riser (2F) and gravity power generation building (12) column tube (12B) square flange (12D) square steel frame (12A) upper and lower bolts Various energy conservation cycle coalescence engines and coalescence methods with floors of 200 floors or less.   Vertical type moving blade specific material gravity turbine (11B) specific material riser (2F) and gravity power generation building (12) column tube (12B) square flange (12D) square steel frame (12A) upper and lower bolts Various energy conservation cycle coalescence engines and coalescence methods with floors of 150 floors or less.   Vertical type moving blade specific material gravity turbine (11B) specific material riser (2F) and gravity power generation building (12) column tube (12B) square flange (12D) square steel frame (12A) upper and lower bolts Various energy conservation cycle coalescence engines and coalescence methods with floors of 100 floors or less.   Vertical type moving blade specific material gravity turbine (11B) specific material riser (2F) and gravity power generation building (12) column tube (12B) square flange (12D) square steel frame (12A) upper and lower bolts Various energy conservation cycle coalescence engines and coalescence methods with floors below 80 floors.   Vertical type moving blade specific material gravity turbine (11B) specific material riser (2F) and gravity power generation building (12) column tube (12B) square flange (12D) square steel frame (12A) upper and lower bolts Various energy conservation cycle coalescence engines and coalescence methods with floors of 60 floors or less.   Various energy conservation cycle coalescence engines and coalescence that use the significant material (3E) ascended and stored at the top in the vertical type moving blade specific material gravity turbine (11B) specific material riser (2F) and column pipe (12B) Method.   Vertical all-blade specific material gravity turbine (11B) specific material riser (2F) and column pipe (12B) with specific material (3E) rise to the top and preservation ratio material injection (6W) Various energy storage cycle coalescence engine and coalescence method.   Vertical type moving blade ratio critical material gravity turbine (11B) ratio critical material riser (2F) and column pipe (12B) raise specific material (3E) to the top Conservation ratio critical material accelerator (6W) Mach 3 Various energy storage cycle coalescence engines and coalescence methods to be injected as described above.   Vertical type moving blade ratio critical material gravity turbine (11B) ratio critical material riser (2F) and column pipe (12B) raise specific material (3E) to the top Conservation ratio critical material accelerator (6W) Mach 3 Various energy storage cycle coalescence engines and coalescence methods to be injected below.   Vertical material blade specific material gravity turbine (11B) specific material riser (2F) and column tube (12B) with specific material (3E) raised to the top Preservation ratio material material accelerator (6W) Mach 1 Various energy storage cycle coalescence engines and coalescence methods to be injected as described above.   Vertical material blade specific material gravity turbine (11B) specific material riser (2F) and column tube (12B) with specific material (3E) raised to the top Preservation ratio material material accelerator (6W) Mach 1 Various energy storage cycle coalescence engines and coalescence methods to be injected below.   Vertical all-blade specific material gravity turbine (11B) specific material riser (2F) and column pipe (12B) with specific material (3E) rise to the top and preservation ratio material injection (6W) Various energy storage cycle coalescence engine and coalescence method for acceleration of gravitational acceleration in vacuum.   Vertical type moving blade ratio critical material gravity turbine (11B) ratio critical material riser (2F) and column pipe (12B) raise specific material (3E) to the top Conservation ratio critical material accelerator (6W) Mach 3 Various energy storage cycle coalescence engines and coalescence methods for accelerating gravitational acceleration in a jet vacuum.   Vertical type moving blade ratio critical material gravity turbine (11B) ratio critical material riser (2F) and column pipe (12B) raise specific material (3E) to the top Conservation ratio critical material accelerator (6W) Mach 3 Various energy storage cycle coalescence engines and coalescence methods for accelerating gravitational acceleration in a jet vacuum below.   Vertical material blade specific material gravity turbine (11B) specific material riser (2F) and column tube (12B) with specific material (3E) raised to the top Preservation ratio material material accelerator (6W) Mach 1 Various energy storage cycle coalescence engines and coalescence methods for accelerating gravitational acceleration in a jet vacuum.   Vertical material blade specific material gravity turbine (11B) specific material riser (2F) and column tube (12B) with specific material (3E) raised to the top Preservation ratio material material accelerator (6W) Mach 1 Various energy storage cycle coalescence engines and coalescence methods for accelerating gravitational acceleration in a jet vacuum below.   Vertical all-blade specific material gravity turbine (11B) specific material riser (2F) and column pipe (12B) with specific material (3E) rise to the top and preservation ratio material injection (6W) Various energy storage cycle coalescence engine and coalescence method for injecting into gravity acceleration acceleration cylinder outer rotor blade group (60D) and cylinder inner rotor blade group (60C) in vacuum.   Vertical type moving blade ratio critical material gravity turbine (11B) ratio critical material riser (2F) and column pipe (12B) raise specific material (3E) to the top Conservation ratio critical material accelerator (6W) Mach 3 As described above, various energy storage cycle coalescence engines and coalescence methods for injecting into the gravity acceleration acceleration cylinder outer rotor blade group (60D) and cylinder inner rotor blade group (60C) in jet vacuum.   Vertical type moving blade ratio critical material gravity turbine (11B) ratio critical material riser (2F) and column pipe (12B) raise specific material (3E) to the top Conservation ratio critical material accelerator (6W) Mach 3 Various energy storage cycle coalescence engines and coalescence methods for injecting into a gravity acceleration acceleration cylinder outer rotor blade group (60D) and cylinder inner rotor blade group (60C) in jet vacuum in the following.   Vertical material blade specific material gravity turbine (11B) specific material riser (2F) and column tube (12B) with specific material (3E) raised to the top Preservation ratio material material accelerator (6W) Mach 1 As described above, various energy storage cycle coalescence engines and coalescence methods for injecting into the gravity acceleration acceleration cylinder outer rotor blade group (60D) and cylinder inner rotor blade group (60C) in jet vacuum.   Vertical material blade specific material gravity turbine (11B) specific material riser (2F) and column tube (12B) with specific material (3E) raised to the top Preservation ratio material material accelerator (6W) Mach 1 Various energy storage cycle coalescence engines and coalescence methods for injecting into a gravity acceleration acceleration cylinder outer rotor blade group (60D) and cylinder inner rotor blade group (60C) in jet vacuum in the following.   Vertical all-blade specific material gravity turbine (11B) specific material riser (2F) and column pipe (12B) with specific material (3E) rise to the top and preservation ratio material injection (6W) Various energy storage cycle coalescing engines and coalescence methods in which each of the jets is driven in a counter-rotating manner into a vacuum outer gravity blade group (60D) and a cylinder inner blade group (60C) in vacuum   Vertical type moving blade ratio critical material gravity turbine (11B) ratio critical material riser (2F) and column pipe (12B) raise specific material (3E) to the top Conservation ratio critical material accelerator (6W) Mach 3 As described above, various energy storage cycle coalescence engines and coalescence methods for driving the jets to reversely rotate in the jet vacuum gravity acceleration accelerating cylinder outer rotor blade group (60D) and cylinder inner rotor blade group (60C).   Vertical type moving blade ratio critical material gravity turbine (11B) ratio critical material riser (2F) and column pipe (12B) raise specific material (3E) to the top Conservation ratio critical material accelerator (6W) Mach 3 In the following, various energy storage cycle coalescence engines and coalescence methods in which each of the jets is driven in a counter-rotating manner into the gravity vacuum acceleration cylinder outer rotor blade group (60D) and cylinder inner rotor blade group (60C) in jet vacuum.   Vertical material blade specific material gravity turbine (11B) specific material riser (2F) and column tube (12B) with specific material (3E) raised to the top Preservation ratio material material accelerator (6W) Mach 1 As described above, various energy storage cycle coalescence engines and coalescence methods for driving the jets to reversely rotate in the jet vacuum gravity acceleration accelerating cylinder outer rotor blade group (60D) and cylinder inner rotor blade group (60C).   Vertical material blade specific material gravity turbine (11B) specific material riser (2F) and column tube (12B) with specific material (3E) raised to the top Preservation ratio material material accelerator (6W) Mach 1 In the following, various energy storage cycle coalescence engines and coalescence methods in which each of the jets is driven in a counter-rotating manner into the gravity vacuum acceleration cylinder outer rotor blade group (60D) and cylinder inner rotor blade group (60C) in jet vacuum.   Vertical all-blade specific material gravity turbine (11B) specific material riser (2F) and column pipe (12B) with specific material (3E) rise to the top and preservation ratio material injection (6W) Various energy storage cycle coalescence engines and coalescence methods for generating electric power by inverting and injecting each of the jets into a vacuum outer gravity blade group (60D) and a cylinder inner blade group (60C) in vacuum.   Vertical type moving blade ratio critical material gravity turbine (11B) ratio critical material riser (2F) and column pipe (12B) raise specific material (3E) to the top Conservation ratio critical material accelerator (6W) Mach 3 As described above, various energy storage cycle coalescence engines and coalescence methods for generating electric power by inverting and driving the respective jets in the jet vacuum gravity acceleration accelerating cylinder outer rotor blade group (60D) and cylinder inner rotor blade group (60C).   Vertical type moving blade ratio critical material gravity turbine (11B) ratio critical material riser (2F) and column pipe (12B) raise specific material (3E) to the top Conservation ratio critical material accelerator (6W) Mach 3 Various energy storage cycle coalescence engines and coalescence methods for generating electric power by inverting and injecting each of the jets into the outer vacuum blade group (60D) and the inner cylinder blade group (60C) in the gravity acceleration acceleration cylinder in the jet vacuum.   Vertical material blade specific material gravity turbine (11B) specific material riser (2F) and column tube (12B) with specific material (3E) raised to the top Preservation ratio material material accelerator (6W) Mach 1 As described above, various energy storage cycle coalescence engines and coalescence methods for generating electric power by inverting and driving the respective jets in the jet vacuum gravity acceleration accelerating cylinder outer rotor blade group (60D) and cylinder inner rotor blade group (60C).   Vertical material blade specific material gravity turbine (11B) specific material riser (2F) and column tube (12B) with specific material (3E) raised to the top Preservation ratio material material accelerator (6W) Mach 1 Various energy storage cycle coalescence engines and coalescence methods for generating electric power by inverting and injecting each of the jets into the outer vacuum blade group (60D) and the inner cylinder blade group (60C) in the gravity acceleration acceleration cylinder in the jet vacuum.   Bearings at both ends of the vertical all blade ratio material gravity turbine (11B) outer shaft device (60B) and cylindrical outer blade group (60D) and inner shaft device (60A) and cylinder inner blade group (60C) ( 12C) Various energy storage cycle coalescence engines and coalescence methods provided.   Bearings at both ends of the vertical all blade ratio material gravity turbine (11B) outer shaft device (60B) and cylindrical outer blade group (60D) and inner shaft device (60A) and cylinder inner blade group (60C) ( 12C) Various energy storage cycle merging engines and merging methods that enable both-end support processing with a temporary assembly machine tool.   Bearings at both ends of the vertical all blade ratio material gravity turbine (11B) outer shaft device (60B) and cylindrical outer blade group (60D) and inner shaft device (60A) and cylinder inner blade group (60C) ( 12C) Various energy storage cycle merging engines and merging methods in which both ends are supported and ultra-high-speed balance adjustment processing is separately performed by temporary assembly machine tools.   Bearings at both ends of the vertical all blade ratio material gravity turbine (11B) outer shaft device (60B) and cylindrical outer blade group (60D) and inner shaft device (60A) and cylinder inner blade group (60C) ( 12C) Various energy storage cycle merging engines and merging methods for performing ultra-high-speed balance adjustment ultra-precision machining with both ends supported by a temporary assembly machine tool.   Bearings at both ends of the vertical all blade ratio material gravity turbine (11B) outer shaft device (60B) and cylindrical outer blade group (60D) and inner shaft device (60A) and cylinder inner blade group (60C) ( 12C) Various energy storage cycle merging engines and merging methods to be assembled after ultra-high-speed balance adjustment and ultra-precision machining on both ends separately by temporary assembly machine tools.   Spider-type all blade ratio critical material gravity turbine (11B) generator-driven liquid oxygen production machine (89A) outer shaft device (60B) and outer compression blade (8r) and inner shaft device (60A) and inner compression blade (8q) ) Various energy storage cycle coalescence engines and coalescence methods equipped with bearings (12C) at both ends.   Spider-type all blade ratio critical material gravity turbine (11B) generator-driven liquid oxygen production machine (89A) outer shaft device (60B) and outer compression blade (8r) and inner shaft device (60A) and inner compression blade (8q) ) Various energy storage cycle merging engines and merging methods each having bearings (12C) at both ends and separately supporting both ends with a temporary assembly machine tool.   Spider-type all blade ratio critical material gravity turbine (11B) generator-driven liquid oxygen production machine (89A) outer shaft device (60B) and outer compression blade (8r) and inner shaft device (60A) and inner compression blade (8q) ) Various energy storage cycle merging engines and merging methods, in which bearings (12C) are provided at both ends, and both ends are supported by a temporary assembly machine tool, and both ends are supported and ultra-high-speed balance adjustment is performed.   Spider-type all blade ratio critical material gravity turbine (11B) generator-driven liquid oxygen production machine (89A) outer shaft device (60B) and outer compression blade (8r) and inner shaft device (60A) and inner compression blade (8q) ) Various energy storage cycle merging engines and merging methods in which bearings (12C) are provided at both ends, respectively, and both ends are supported and ultra-high-speed balance adjustment ultra-precision machining is performed with a temporary assembly machine tool.   Spider-type all blade ratio critical material gravity turbine (11B) generator-driven liquid oxygen production machine (89A) outer shaft device (60B) and outer compression blade (8r) and inner shaft device (60A) and inner compression blade (8q) ) Bearings (12C) at both ends, and each energy storage cycle coalescence engine and coalescence method to be assembled after ultra-high-speed balance adjustment ultra-precision machining with both ends supported by a temporary assembly machine tool.   Vertical type moving blade ratio critical material gravity turbine (11B) Electric power driven liquid oxygen production machine (89A) Outer shaft device (60B) and outer output blade (8t) and Inner shaft device (60A) and inner output blade (8s) ) Various energy storage cycle coalescence engines and coalescence methods equipped with bearings (12C) at both ends.   Vertical type moving blade ratio critical material gravity turbine (11B) Electric power driven liquid oxygen production machine (89A) Outer shaft device (60B) and outer output blade (8t) and Inner shaft device (60A) and inner output blade (8s) ) Various energy storage cycle merging engines and merging methods each having bearings (12C) at both ends and separately supporting both ends with a temporary assembly machine tool.   Vertical type moving blade ratio critical material gravity turbine (11B) Electric power driven liquid oxygen production machine (89A) Outer shaft device (60B) and outer output blade (8t) and Inner shaft device (60A) and inner output blade (8s) ) Various energy storage cycle merging engines and merging methods, in which bearings (12C) are provided at both ends, and both ends are supported by a temporary assembly machine tool, and both ends are supported and ultra-high-speed balance adjustment is performed.   Vertical type moving blade ratio critical material gravity turbine (11B) Electric power driven liquid oxygen production machine (89A) Outer shaft device (60B) and outer output blade (8t) and Inner shaft device (60A) and inner output blade (8s) ) Various energy storage cycle merging engines and merging methods in which bearings (12C) are provided at both ends, respectively, and both ends are supported and ultra-high-speed balance adjustment ultra-precision machining is performed with a temporary assembly machine tool.   Vertical type moving blade ratio critical material gravity turbine (11B) Electric power driven liquid oxygen production machine (89A) Outer shaft device (60B) and outer output blade (8t) and Inner shaft device (60A) and inner output blade (8s) ) Bearings (12C) at both ends, and each energy storage cycle coalescence engine and coalescence method to be assembled after ultra-high-speed balance adjustment ultra-precision machining with both ends supported by a temporary assembly machine tool.   A simple multi-stage compressor (89B), outer shaft device (60B) and outer compressor blade (8r) and inner shaft device (60A) and inner compressor blade (8q), which are connected and driven, are fitted with bearings (12C) at both ends. Various energy storage cycle coalescing engine and coalescence method capable of containing all blade ratio material gravity turbine (11B) 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. Various types of energy storage cycle coalescence engine and coalescence method capable of containing a vertical-type all-blade specific material gravity turbine (11B) generator electric product drive 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 types of energy storage cycle coalescence engine and coalescence method capable of containing a vertical type moving blade ratio critical material gravity turbine (11B) power generation electric product driven at both ends with a temporary assembly machine tool and adjusted at ultra high speed.   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. Both types of energy storage cycle coalescence engine and coalescence method capable of being driven by a vertical type blade blade critical material gravity turbine (11B) power generation electrical product to be processed at both ends with a temporary assembly machine tool, ultra-high speed balance adjustment and ultra-precision machining.   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. Supporting both ends with a temporary assembly machine tool Ultra-high-speed balance adjustment Super-precision machining to make the final assembly of a blade-type all-blade ratio critical material Gravity turbine (11B) Various energy storage cycle coalescence engine and coalescence method that can be driven .   Vertical type moving blade ratio critical material gravity turbine (11B) Simple gas engine (89C) including power generation electric product drive Outer shaft device (60B) and outer compressor blade (8r) and inner shaft device (60A) and inner compressor blade (8q) Various energy storage cycle coalescence engines and coalescence methods provided with bearings (12C) at both ends.   Vertical type moving blade ratio critical material gravity turbine (11B) Simple gas engine (89C) including power generation electric product drive Outer shaft device (60B) and outer compressor blade (8r) and inner shaft device (60A) and inner compressor blade (8q) Various energy storage cycle merging engines and merging methods in which bearings (12C) are provided at both ends and both ends are separately supported by a temporary assembly machine tool.   Vertical type moving blade ratio critical material gravity turbine (11B) Simple gas engine (89C) including power generation electric product drive Outer shaft device (60B) and outer compressor blade (8r) and inner shaft device (60A) and inner compressor blade (8q) Various energy storage cycle merging engines and merging methods in which bearings (12C) are provided at both ends, and the both ends are supported and ultra-high-speed balance adjustment processing is separately performed by a temporary assembly machine tool.   Vertical type moving blade ratio critical material gravity turbine (11B) Simple gas engine (89C) including power generation electric product drive Outer shaft device (60B) and outer compressor blade (8r) and inner shaft device (60A) and inner compressor blade (8q) Various energy storage cycle merging engines and merging methods in which bearings (12C) are provided at both ends, and both ends are supported and ultra-high-speed balance adjustment ultra-precision machining is performed separately by a temporary assembly machine tool.   Vertical type moving blade ratio critical material gravity turbine (11B) Simple gas engine (89C) including power generation electric product drive Outer shaft device (60B) and outer compressor blade (8r) and inner shaft device (60A) and inner compressor blade (8q) Various energy storage cycle merging engines and merging methods in which bearings (12C) are provided at both ends, and each assembly is separately assembled by temporary assembly machine tools after both ends are supported and ultra-high speed balance adjustment is performed after ultra-precision machining.   Vertical all blade ratio material gravity turbine (11B) Simple gas engine (89C) including power generation electrical product drive Outer shaft device (60B) and outer output blade (8t) and inner shaft device (60A) and inner output blade (8s) Various energy storage cycle coalescence engines and coalescence methods equipped with bearings (12C) at both ends.   Vertical all blade ratio material gravity turbine (11B) Simple gas engine (89C) including power generation electrical product drive Outer shaft device (60B) and outer output blade (8t) and inner shaft device (60A) and inner output blade (8s) Various energy storage cycle coalescence engines and coalescence methods that have bearings (12C) at both ends and can be supported at both ends by a temporary assembly machine tool.   Vertical all blade ratio material gravity turbine (11B) Simple gas engine (89C) including power generation electrical product drive Outer shaft device (60B) and outer output blade (8t) and inner shaft device (60A) and inner output blade (8s) Various energy storage cycle merging engines and merging methods in which bearings (12C) are provided at both ends, and both ends are supported and ultra-high-speed balance adjustment processing is separately performed by a temporary assembly machine tool.   Vertical all blade ratio material gravity turbine (11B) Simple gas engine (89C) including power generation electrical product drive Outer shaft device (60B) and outer output blade (8t) and inner shaft device (60A) and inner output blade (8s) Various energy storage cycle merging engines and merging methods in which bearings (12C) are provided at both ends, and both ends are supported and ultra-high-speed balance adjustment ultra-precision machining is performed separately by a temporary assembly machine tool.   Vertical all blade ratio material gravity turbine (11B) Simple gas engine (89C) including power generation electrical product drive Outer shaft device (60B) and outer output blade (8t) and inner shaft device (60A) and inner output blade (8s) Bearings (12C) provided at both ends, and various energy storage cycle combining engines and combining methods to be assembled after ultra-high-speed balance adjustment and ultra-precision processing with both ends supported by a temporary assembly machine tool.   Vertical all blade ratio material gravity turbine (11B) Simple air injection engine (89D) including power generation electrical product drive Outer shaft device (60B) and outer compressor blade (8r) and inner shaft device (60A) and inner compression Various energy storage cycle coalescence engines and coalescence methods having bearings (12C) at both ends of each blade (8q).   Vertical all blade ratio material gravity turbine (11B) Simple air injection engine (89D) including power generation electrical product drive Outer shaft device (60B) and outer compressor blade (8r) and inner shaft device (60A) and inner compression Bearings (12C) are provided at both ends of each of the blades (8q), and various energy storage cycle combining engines and combining methods that enable both-end support processing with a temporary assembly machine tool.   Vertical all blade ratio material gravity turbine (11B) Simple air injection engine (89D) including power generation electrical product drive Outer shaft device (60B) and outer compressor blade (8r) and inner shaft device (60A) and inner compression Various energy storage cycle merging engines and merging methods in which bearings (12C) are provided at both ends of each of the blades (8q), and both ends are supported and ultra-high-speed balance adjustment processing is performed by a temporary assembly machine tool.   Vertical all blade ratio material gravity turbine (11B) Simple air injection engine (89D) including power generation electrical product drive Outer shaft device (60B) and outer compressor blade (8r) and inner shaft device (60A) and inner compression Various energy storage cycle merging engines and merging methods that have bearings (12C) at both ends of each of the blades (8q), respectively, and perform ultra-high-speed balance adjustment ultra-precision machining at both ends with a temporary assembly machine tool.   Vertical all blade ratio material gravity turbine (11B) Simple air injection engine (89D) including power generation electrical product drive Outer shaft device (60B) and outer compressor blade (8r) and inner shaft device (60A) and inner compression Bearings (12C) are provided at both ends of each blade (8q), 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.   Vertical all-blade ratio critical material gravity turbine (11B) simple air injection engine (89D) including power generation electrical product drive outer shaft device (60B) and outer output blade (8t) and inner shaft device (60A) and inner output Various energy storage cycle coalescence engines and coalescence methods equipped with bearings (12C) at both ends of each blade (8s).   Vertical all-blade ratio critical material gravity turbine (11B) simple air injection engine (89D) including power generation electrical product drive outer shaft device (60B) and outer output blade (8t) and inner shaft device (60A) and inner output Bearings (12C) are provided at both ends of each of the blades (8s), and various energy storage cycle combining engines and combining methods that enable both ends to be supported by a temporary assembly machine tool.   Vertical all-blade ratio critical material gravity turbine (11B) simple air injection engine (89D) including power generation electrical product drive outer shaft device (60B) and outer output blade (8t) and inner shaft device (60A) and inner output Various energy storage cycle merging engines and merging methods in which bearings (12C) are provided at both ends of each of the blades (8s), respectively, and both ends are supported by a temporary assembly machine tool and ultra-high speed balance adjustment processing is performed.   Vertical all-blade ratio critical material gravity turbine (11B) simple air injection engine (89D) including power generation electrical product drive outer shaft device (60B) and outer output blade (8t) and inner shaft device (60A) and inner output Bearings (12C) are provided at both ends of each blade (8s), and various energy storage cycle merging engines and merging methods are used to perform ultra-high-speed balance adjustment ultra-precision machining with both ends supported by temporary assembly machine tools.   Vertical all-blade ratio critical material gravity turbine (11B) simple air injection engine (89D) including power generation electrical product drive outer shaft device (60B) and outer output blade (8t) and inner shaft device (60A) and inner output Bearings (12C) are provided at both ends of each wing (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 ultrahigh-speed balance adjustment is performed after ultraprecision machining.   Vertical type moving blade ratio critical material gravity turbine (11B) Simple injection engine (89E) including outer power unit (60B) and outer compressor unit (8r) and inner shaft unit (60A) and inner unit compressor (8q) Various energy storage cycle coalescence engines and coalescence methods provided with bearings (12C) at both ends.   Vertical type moving blade ratio critical material gravity turbine (11B) Simple injection engine (89E) including outer power unit (60B) and outer compressor unit (8r) and inner shaft unit (60A) and inner unit compressor (8q) Various energy storage cycle merging engines and merging methods in which bearings (12C) are provided at both ends and both ends are separately supported by a temporary assembly machine tool.   Vertical type moving blade ratio critical material gravity turbine (11B) Simple injection engine (89E) including outer power unit (60B) and outer compressor unit (8r) and inner shaft unit (60A) and inner unit compressor (8q) Various energy storage cycle merging engines and merging methods in which bearings (12C) are provided at both ends, and the both ends are supported and ultra-high-speed balance adjustment processing is separately performed by a temporary assembly machine tool.   Vertical type moving blade ratio critical material gravity turbine (11B) Simple injection engine (89E) including outer power unit (60B) and outer compressor unit (8r) and inner shaft unit (60A) and inner unit compressor (8q) Various energy storage cycle merging engines and merging methods in which bearings (12C) are provided at both ends, and both ends are supported and ultra-high-speed balance adjustment ultra-precision machining is performed separately by a temporary assembly machine tool.   Vertical type moving blade ratio critical material gravity turbine (11B) Simple injection engine (89E) including outer power unit (60B) and outer compressor unit (8r) and inner shaft unit (60A) and inner unit compressor (8q) Various energy storage cycle merging engines and merging methods in which bearings (12C) are provided at both ends, and each assembly is separately assembled by temporary assembly machine tools after both ends are supported and ultra-high speed balance adjustment is performed after ultra-precision machining.   Vertical type moving blade ratio critical material gravity turbine (11B) Simple injection engine (89E) including power generation electric product drive Outer shaft device (60B) and outer output blade (8t) and inner shaft device (60A) and inner output blade (8s) Various energy storage cycle coalescence engines and coalescence methods equipped with bearings (12C) at both ends.   Vertical type moving blade ratio critical material gravity turbine (11B) Simple injection engine (89E) including power generation electric product drive Outer shaft device (60B) and outer output blade (8t) and inner shaft device (60A) and inner output blade (8s) Various energy storage cycle coalescence engines and coalescence methods that have bearings (12C) at both ends and can be supported at both ends by a temporary assembly machine tool.   Vertical type moving blade ratio critical material gravity turbine (11B) Simple injection engine (89E) including power generation electric product drive Outer shaft device (60B) and outer output blade (8t) and inner shaft device (60A) and inner output blade (8s) Various energy storage cycle merging engines and merging methods in which bearings (12C) are provided at both ends, and both ends are supported and ultra-high-speed balance adjustment processing is separately performed by a temporary assembly machine tool.   Vertical type moving blade ratio critical material gravity turbine (11B) Simple injection engine (89E) including power generation electric product drive Outer shaft device (60B) and outer output blade (8t) and inner shaft device (60A) and inner output blade (8s) Various energy storage cycle merging engines and merging methods in which bearings (12C) are provided at both ends, and both ends are supported and ultra-high-speed balance adjustment ultra-precision machining is performed separately by a temporary assembly machine tool.   Vertical type moving blade ratio critical material gravity turbine (11B) Simple injection engine (89E) including power generation electric product drive Outer shaft device (60B) and outer output blade (8t) and inner shaft device (60A) and inner output blade (8s) Bearings (12C) provided at both ends, and various energy storage cycle combining engines and combining methods to be assembled after ultra-high-speed balance adjustment and ultra-precision processing with both ends supported by a temporary assembly machine tool.   A simple gas engine (89C), which completely abolishes existing stationary blades and double-rotating blades, is equipped with a compressed air heat exchanger (2Y) and produces the same amount of superheated steam (5H) as the same fuel amount as that of existing boilers. Various energy storage cycle coalescing engines and coalescence methods that can be driven and contained in a vertical-type all-blade ratio critical material gravity turbine (11B) power generation electric product that makes the rotational output and injection propulsion output more than double that of the 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) to produce superheated steam (5H) with the same fuel amount as the existing boiler 4 Various energy storage cycle coalescence engines and coalescence methods that can be driven and contained in a vertical type moving blade ratio critical material gravity turbine (11B) power generation electric product that makes the rotational output and injection propulsion output more than four times that of the 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 engine and coalescence method capable of containing a vertical type moving blade ratio critical material gravity turbine (11B) power generation electric product to make the rotation output and injection propulsion output more than 8 times that of the 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) to produce superheated steam (5H) with the same fuel amount as the existing boiler 4 Various energy storage cycle coalescence engine and coalescence method capable of containing a vertical type moving blade ratio critical material gravity turbine (11B) power generation electric product to make the rotational output more than twice that of the 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 engine and coalescence method capable of containing a vertical type moving blade ratio critical material gravity turbine (11B) power generation electric product driving that makes the rotational output more than 16 times that of the 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) to produce superheated steam (5H) with the same fuel amount as the existing boiler 4 The energy output cycle coalescence engine that can be driven by the vertical type moving blade ratio critical material gravity turbine (11B) power generation electric product to make it a simple gas engine motor vehicle (89F) whose rotational output is more than 8 times that of the existing gas turbine 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. The energy output cycle coalescence engine that can be driven by the vertical type moving blade ratio critical material gravity turbine (11B) power generation electrical product to make the rotation output more than 16 times that of the existing gas turbine 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) to produce superheated steam (5H) with the same fuel amount as the existing boiler 4 Various energy storage cycle coalescence engine and coalescence method capable of driving and driving the vertical type moving blade ratio critical material gravity turbine (11B) power generation electric product to make automobiles more than double the rotation output to 8 times or more 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 capable of driving and driving the vertical type moving blade ratio critical material gravity turbine (11B) power generation electric product, which makes the rotation output more than 16 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) to produce superheated steam (5H) with the same fuel amount as the existing boiler 4 Various energy storage cycle coalescence engine and coalescence method capable of containing a vertical type moving blade ratio critical material gravity turbine (11B) power generation electrical product to make vehicles more than twice as many as the rotational output 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 engines and coalescence methods capable of containing a vertical type moving blade ratio critical material gravity turbine (11B) power generation electric product to make the rotation output more than 16 times that of a vehicle having a rotational output of 16 times or more.   A simple gas engine (89C), which completely abolishes existing stationary blades and double-rotating blades, is equipped with a compressed air heat exchanger (2Y) and produces the same amount of superheated steam (5H) as the same fuel amount as that of existing boilers. Rotating output and injection propulsion output to make a simple gas engine ship (89G) more than twice as large as the existing gas turbine Storage cycle coalescence engine 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) to produce superheated steam (5H) with the same fuel amount as the existing boiler 4 Rotating output and injection propulsion output to make a simple gas engine ship (89G) more than 4 times that of the existing gas turbine Storage cycle coalescence engine 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. Rotating output and injection propulsion output to make a simple gas engine ship (89G) more than 8 times that of the existing gas turbine Storage cycle coalescence engine and coalescence method.   A simple gas engine (89C), which completely abolishes existing stationary blades and double-rotating blades, is equipped with a compressed air heat exchanger (2Y) and produces the same amount of superheated steam (5H) as the same fuel amount as that of existing boilers. Rotating output and injection propulsion output to make a simple gas engine airplane (89H) more than twice that of an existing gas turbine Storage cycle coalescence engine 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) to produce superheated steam (5H) with the same fuel amount as the existing boiler 4 Rotating output and injection propulsion output to make a simple gas engine airplane (89H) more than 4 times that of an existing gas turbine Storage cycle coalescence engine 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. Rotating output and injection propulsion output to make a simple gas engine airplane (89H) more than 8 times that of an existing gas turbine Storage cycle coalescence engine and coalescence method.   A simple gas engine (89C), which completely abolishes existing stationary blades and double-rotating blades, is equipped with a compressed air heat exchanger (2Y) and produces the same amount of superheated steam (5H) as the same fuel amount as that of existing boilers. More than twice the rotational output and injection propulsion output to make the rotor blade airplane (89K) more than twice that of the existing gas turbine. Cycle coalescence engine 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) to produce superheated steam (5H) with the same fuel amount as the existing boiler 4 Rotating power and injection propulsion power to make the rotor blade airplane (89K) more than 4 times that of the existing gas turbine. Cycle coalescence engine 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. Rotating output and injection propulsion output to make rotor blade airplane (89K) more than 8 times that of existing gas turbines. Vertical type moving blade specific material gravity turbine (11B) Power generation Electric product drive can contain various energy storage Cycle coalescence engine and coalescence method.   A simple gas engine (89C), which completely abolishes existing stationary blades and double-rotating blades, is equipped with a compressed air heat exchanger (2Y) and produces the same amount of superheated steam (5H) as the same fuel amount as that of existing boilers. Rotating output and propulsion propulsion output to a large Osprey (89N) that is more than twice that of existing gas turbines. 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) to produce superheated steam (5H) with the same fuel amount as the existing boiler 4 Rotating output and injection propulsion output to make large osprey (89N) more than 4 times that of existing gas turbines 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 large Osprey (89N) more than 8 times that of the existing gas turbine Merger engine and merger method.   A simple injection engine (89E), which completely abolishes existing stator blades and has double rotating blades, is equipped with a compressed air heat exchanger (2Y) and produces the same amount of superheated steam (5H) with the same fuel amount of existing boilers. Rotating output and injection propulsion output more than double that of a simple air-injection engine ship (89I) that is more than twice that of an existing gas turbine. Energy conservation cycle coalescence engine and coalescence method.   A simple injection engine (89E) that completely abolishes existing stator blades and has double rotating blades, is equipped with a compressed air heat exchanger (2Y), and produces the same amount of superheated steam (5H) as the same fuel amount of existing boilers. Rotating output and propulsion propulsion output is more than 4 times that of existing gas turbine, making it a simple air injection engine ship (89I). Energy conservation 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) more than 8 times that of an existing gas turbine Energy conservation cycle coalescence engine and coalescence method.   A simple injection engine (89E), which completely abolishes existing stator blades and has double rotating blades, is equipped with a compressed air heat exchanger (2Y) and produces the same amount of superheated steam (5H) with the same fuel amount of existing boilers. Rotating output and injection propulsion output to make a simple injection engine airplane (89J) more than twice that of an existing gas turbine Storage cycle coalescence engine and coalescence method.   A simple injection engine (89E) that completely abolishes existing stator blades and has double rotating blades, is equipped with a compressed air heat exchanger (2Y), and produces the same amount of superheated steam (5H) as the same fuel amount of existing boilers. Rotating output and injection propulsion output to make a simple injection engine airplane (89J) more than 4 times that of existing gas turbines Storage 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 to make a simple injection engine airplane (89J) more than 8 times that of existing gas turbines Storage cycle coalescence engine and coalescence method.   A simple injection engine (89E), which completely abolishes existing stator blades and has double rotating blades, is equipped with a compressed air heat exchanger (2Y) and produces the same amount of superheated steam (5H) with the same fuel amount of existing boilers. Rotating blades and injection propulsion powers that are more than double that of a rotary blade injection airplane (89L) that is twice or more that of an existing gas turbine. Storage cycle coalescence engine and coalescence method.   A simple injection engine (89E) that completely abolishes existing stator blades and has double rotating blades, is equipped with a compressed air heat exchanger (2Y), and produces the same amount of superheated steam (5H) as the same fuel amount of existing boilers. Rotating blades and injection propulsion powers that make the rotor blade injection plane (89L) more than 4 times that of existing gas turbines Storage 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 blades and injection propulsion power to make rotor blade injection plane (89L) more than 8 times that of the existing gas turbine Storage cycle coalescence engine and coalescence method.   A simple injection engine (89E), which completely abolishes existing stator blades and has double rotating blades, is equipped with a compressed air heat exchanger (2Y) and produces the same amount of superheated steam (5H) with the same fuel amount of existing boilers. Rotating output and injection propulsion output is oversized Osprey (89M) more than twice that of existing gas turbine Merger engine and merger method.   A simple injection engine (89E) that completely abolishes existing stator blades and has double rotating blades, is equipped with a compressed air heat exchanger (2Y), and produces the same amount of superheated steam (5H) as the same fuel amount of existing boilers. Rotating output and propulsion propulsion output over 4 times that of existing gas turbines with oversized Osprey (89M) 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 are oversized Osprey (89M) more than 8 times that of existing gas turbines Merger engine and merger 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 twice the rotational output and injection propulsion output to make the simple air-injection engine ship (89I) more than twice the existing gas turbine can be driven by the vertical full blade ratio material gravity turbine (11B) power generation electric product drive Various energy storage cycle coalescence engines and coalescence methods.   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 4 times the rotational output and injection propulsion output is a simple air injection engine ship (89I) that is 4 times more than the existing gas turbine. Various energy storage cycle coalescence engines and coalescence methods.   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 rotary output and injection propulsion output is 8 times more than the existing gas turbine simple air injection engine ship (89I). Various energy storage cycle coalescence engines and coalescence methods.   A simple gas engine (89C), which completely abolishes existing stationary blades and double-rotating blades, is equipped with a compressed air heat exchanger (2Y) and produces the same amount of superheated steam (5H) as the same fuel amount as that of existing boilers. It is possible to include a vertical type full blade ratio gravity material gravity turbine (11B) power generation electric product drive that drives the whole rotor blade steam turbine (11) as much as twice or more (89C) and makes the rotational output more than twice that of the existing gas turbine. Various energy storage cycle coalescence engines and coalescence methods.   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) to produce superheated steam (5H) with the same fuel amount as the existing boiler 4 It is possible to include a vertical type full blade ratio gravity material gravity turbine (11B) power generation electric product drive that drives the whole rotor blade steam turbine (11) as much as twice or more (89C) and the rotational output is four times that of the existing gas turbine. Various energy storage cycle coalescence engines and coalescence methods.   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. It is possible to include a vertical type full blade ratio gravity material gravity turbine (11B) power generation electric product drive that drives the whole blade steam turbine (11) as much as twice or more (89C) and the rotational output is eight times that of the existing gas turbine. Various energy storage cycle coalescence engines and coalescence methods.   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) to produce superheated steam (5H) with the same fuel amount as the existing boiler 4 It is possible to include a vertical type full blade ratio gravity material gravity turbine (11B) power generation electric product drive that drives the whole blade steam turbine (11) as much as twice or more (89C) and the rotational output is eight times that of the existing gas turbine. Various energy storage cycle coalescence engines and coalescence methods.   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. It is possible to include a vertical type full blade ratio gravity material gravity turbine (11B) power generation electric product drive that drives the whole rotor blade steam turbine (11) to more than double (89C) and the rotational output is 16 times that of the existing gas turbine. Various energy storage cycle coalescence engines and coalescence methods.   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) to produce superheated steam (5H) with the same fuel amount as the existing boiler 4 Double-type full-blade specific material gravity turbine (11B) that drives all-blade steam turbines (11) to generate electric power (89C) and makes the rotational output more than eight times that of existing gas turbines. ) Various energy storage cycle coalescing engines and coalescence methods that can be driven by power generation products   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. The vertical blade-type steam turbine (11) is driven to generate power (89C), and the rotary output becomes a simple gas engine vehicle (89F) that is 16 times or more that of the existing gas turbine. ) Various energy storage cycle coalescing engines and coalescence methods that can be driven by power generation products.   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) to produce superheated steam (5H) with the same fuel amount as the existing boiler 4 Double-type all-blade specific material gravity turbine (11B) power generation electric product that drives all-blade steam turbine (11) to more than double the power generation (89C) and makes the rotation output more than eight times that of existing gas turbines Various energy storage cycle coalescence engines and coalescence methods that can be driven and contained.   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. A vertical all-blade specific material gravity turbine (11B) power generation electrical product that drives the power generation of the whole blade steam turbine (11) at a speed of 89 times or more and makes the rotation output 16 times or more that of the existing gas turbine. Various energy storage cycle coalescence engines and coalescence methods that can be driven and contained.   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) to produce superheated steam (5H) with the same fuel amount as the existing boiler 4 Double-type full-blade specific material gravity turbine (11B) power generation electric product that drives all-blade steam turbine (11) to generate power more than twice (89C) and makes the rotation output more than eight times that of existing gas turbines Various energy storage cycle coalescence engines and coalescence methods that can be driven and contained.   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. Double-type full-blade specific material gravity turbine (11B) power generation electrical product that drives all-blade steam turbines (11) to generate more than double the power (89C) and makes the rotational output more than 16 times that of existing gas turbines Various energy storage cycle coalescence engines and coalescence methods that can be driven and contained.   A simple gas engine (89C), which completely abolishes existing stationary blades and double-rotating blades, is equipped with a compressed air heat exchanger (2Y) and produces the same amount of superheated steam (5H) as the same fuel amount as that of existing boilers. Double-type all-blade ratio critical material that drives all-blade steam turbines (11) to generate power (89C) more than double, and makes the rotational output and injection propulsion output more than double that of existing gas turbines (89G) Gravity turbine (11B) various energy storage cycle coalescing engine and coalescence method capable of containing power generation 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) to produce superheated steam (5H) with the same fuel amount as the existing boiler 4 Double-type all-blade blade critical material that drives all-blade steam turbines (11) to generate power (89C), and makes the rotational output and injection propulsion output more than four times that of existing gas turbines (89G) Gravity turbine (11B) various energy storage cycle coalescing engine and coalescence method capable of containing power generation 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. Double-type all-blade ratio critical material that drives all-blade steam turbines (11) to generate power (89C), and makes the rotational output and injection propulsion output more than eight times that of existing gas turbines (89G) Gravity turbine (11B) various energy storage cycle coalescing engine and coalescence method capable of containing power generation electric product drive.   A simple gas engine (89C), which completely abolishes existing stationary blades and double-rotating blades, is equipped with a compressed air heat exchanger (2Y) and produces the same amount of superheated steam (5H) as the same fuel amount as that of existing boilers. Double-type all-blade ratio critical substance that drives and generates power for all blade steam turbines (11) at least twice, and makes the rotation output and injection propulsion output more than twice that of existing gas turbines as a simple gas engine airplane (89H) Gravity turbine (11B) various energy storage cycle coalescing engine and coalescence method capable of containing power generation 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) to produce superheated steam (5H) with the same fuel amount as the existing boiler 4 Double-type all-blade ratio critical material that drives all-blade steam turbine (11) to generate power (89C), and makes the rotational output and injection propulsion output more than four times that of existing gas turbines (89H) Gravity turbine (11B) various energy storage cycle coalescing engine and coalescence method capable of containing power generation 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. Double-type all-blade ratio critical substance that drives and generates power for all rotor blade steam turbines (11C) and makes the output of rotation and injection propulsion more than eight times that of existing gas turbines (89H) Gravity turbine (11B) various energy storage cycle coalescing engine and coalescence method capable of containing power generation electric product drive.   A simple gas engine (89C), which completely abolishes existing stationary blades and double-rotating blades, is equipped with a compressed air heat exchanger (2Y) and produces the same amount of superheated steam (5H) as the same fuel amount as that of existing boilers. Rotating blade turbine (11) is driven to generate power (89C), and the rotary power and injection propulsion power is more than twice that of the existing gas turbine. Various energy storage cycle coalescence engine and coalescence method capable of containing turbine (11B) power generation 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) to produce superheated steam (5H) with the same fuel amount as the existing boiler 4 Rotating all-blade steam turbine (11) to generate power (89C) to make rotary output and injection propulsion output more than four times that of existing gas turbines (89K) Various energy storage cycle coalescence engine and coalescence method capable of containing turbine (11B) power generation 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. Rotating blade steam turbine (11) is driven to generate power (89C), and the rotary power and injection propulsion power is more than 8 times that of the existing gas turbine. Various energy storage cycle coalescence engine and coalescence method capable of containing turbine (11B) power generation electric product drive.   A simple gas engine (89C), which completely abolishes existing stationary blades and double-rotating blades, is equipped with a compressed air heat exchanger (2Y) and produces the same amount of superheated steam (5H) as the same fuel amount as that of existing boilers. Double-type full-blade ratio gravity material gravity turbine that drives all-blade steam turbine (11) to generate power (89C) and makes large output Osplay (89N) more than double the existing gas turbine (11B) Various energy storage cycle coalescing engines and coalescence methods that can be driven and contained in a power generation electric product.   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) to produce superheated steam (5H) with the same fuel amount as the existing boiler 4 Double-type full-blade ratio critical material gravity turbine that drives all-blade steam turbines (11) to generate power (89C) and produces large-scale ospreys (89N) that is more than four times that of existing gas turbines. (11B) Various energy storage cycle coalescing engines and coalescence methods that can be driven and contained in a power generation electric product.   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. Double-type full-blade specific gravity gravity turbine that drives all-blade steam turbine (11) to generate power (89C), and makes large-scale osprey (89N) more than 8 times that of existing gas turbines. (11B) Various energy storage cycle coalescing engines and coalescence methods that can be driven and contained in a power generation electric product.

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