JP2014231768A - Various energy reservation cycle combined engine - Google Patents

Abstract

PROBLEM TO BE SOLVED: To attain solutions overcoming defaults found in the existing jet engines or gas turbines that half of the stationary blades having no power and half of the rotary blades are alternatively arranged to reserve compressed air or combustion gas to cause their speed or output to approach to a value of 0.SOLUTION: In order to eliminate too incoherent defaults found in the existing most-advanced scientific technologies, 10 times-speed compression and expansion are attained through super-speed double inversion linear compression and linear expansion of compression blades 8q, compression blades 8r, output blades 8s and output blades 8t for use in cooling and compression of compressed air with water-cooled compression blades of a double inversion engine 12G and the like having full rotary blades; super-heated steam 5H is manufactured by a compression air heat exchanger 2Y with fuel injection, combustion and heat exchanging operation with a compression ratio being about 100; 130 times super-heated steam 5H of the existing fire power generation boiler with the same amount of fuel is manufactured; 1000 times injection propulsion output of the existing jet engine with the same amount of fuel or rotary output is attained; in an automobile driving or ship driving or airplane driving, the case of the airplanes is rocket injection with super-heated steam from near the existing highest altitude and expenditure of the existing rocket reaching the space is its 1/5,00,000.

Description

Car drive, ship drive and airplane drive by various counter-rotating engines of the present invention have put into practical use an all-rotor counter-rotating engine that has no experimentation or is difficult to manufacture with the latest science and technology, and the pumping pump input of pumped storage power generation is the rotational speed Is calculated to be proportional to the square of the combustion gas velocity and superheated steam velocity, and the rotation output and injection propulsion output that challenge the infinite increase in speed are calculated. By using the air temperature of 20 ° C to 260 ° C, which is 13 times the compression ratio of 8, the air 28a is compressed into a compressed air heat exchanger 2Y that performs heat exchange by compressing the super-high-speed all-rotating blade counter-rotating water cooling blade. Aiming at a compression ratio of 80 to 100, the amount of superheated steam 5H produced is the same fuel amount as 130 times the existing boiler, and the inner compression blade 8q and the outer compression blade 8r are each provided with a water pipe 5G, and the compressed air 28a is cooled with water 52a. 52b, compressed air The superheated steam pipe 5H of the exchanger 2Y is supplied with super high pressure such as 30MPa to produce superheated steam 5H, aiming to produce 30MP superheated steam 5H, which is 130 times the same amount of fuel as the existing boiler. Etc., with the target of injection propulsion output and rotational output 1000 times that of the existing gas turbine, and equipped with various bearings 12C at both ends, and the inner shaft device 60A and the inner output blade 8s are separately provided. The assembly is made into a processing assembly, and both ends are held by machine tools. After the ultra-high speed rotation balance adjustment processing, the assembly is disassembled and assembled, and the unprecedented inner shaft device 60A and inner compression blade 8q, and outer shaft device 60B and outer compression blade 8r. Challenge the speed limit of ultra high speed counter-rotating linear compression, facilitate the compression ratio 80-100, supply to compressed air heat exchanger 2Y, fuel injection combustion and superheated steam Heat recovery is performed at 5H, and by means of counter-rotating linear compression and counter-rotating linear expansion, it is necessary to experiment with the same amount of fuel at 1000 times rotation output and injection propulsion output of the existing gas turbine. Compressor 12N connection, counter-rotating injection engine 12E, counter-rotating air injection engine 12F, counter-rotating automobile 11B, counter-rotating ship 11C, counter-rotating airplane 11E, counter-rotating injection ship 11F, counter-rotating jet airplane 11G, rotary wing airplane 11I, rotary wing jet airplane 11J, Osprey extra large 11M, Osprey large 11N, CO2 exhaust 1/100, fuel cost 1/100, 1 / 500,000 expense space arrival planes and ships aiming at 10 times speed, etc. Each of the energy conservation cycle coalescence engines and various energy conservation aiming at the world's most eternally sustainable operating profit rate It is related with the technique of the union method.

  In the existing pumped-storage power generation, since the pumping input becomes an input proportional to the cube of the rotation speed, a variable speed motor is used, so the rotation output and the injection propulsion output are the combustion gas 49 speed and the superheated steam 5H speed 2 It is necessary to experiment whether it is proportional to the power. Since the water speed of the existing pumped-storage power generation of the existing state-of-the-art science and technology that is too lazy is Mach 1/7, Mach 1/5, etc., superheated steam is injected at approximately the same pressure as the space shuttle combustion chamber pressure of 22-25 MPa, steam The existing thermal power generation technology that drives the turbine, the superheated steam injection speed is calculated to be close to the space shuttle injection speed Mach 30 or the earth escape speed Mach 32, etc. in the static vane linear expansion, and the overheating speed becomes very easy. Steam 5H injection speed Mach 32 or higher There is no engine that can be driven most efficiently other than the full-blade counter-rotating engine, the counter-rotating counter-rotating engine 12G, the counter-rotating injection engine 12E, and the counter-rotating engine. Air injection engine 12F, etc., aiming for rotational output and injection propulsion output 1000 times that of the existing gas turbine, airplanes and ships aiming for 10 times the speed, and airplanes aim for space flight prime. Reaching the budget deficit of 1,000 trillion yen in Japan in a relatively short period of time due to the economic growth strategy revolution and the world's most eternal revolution, with an operating profit rate of 1 / 500,000 and 16 rounds of the earth per day There is background technology that can be aimed at.

  The boiler of existing thermal power generation produces superheated steam by fuel injection combustion at atmospheric pressure and generates electricity with a steam turbine. The temperature rise of adiabatic compression is increased to 260 ° C, which is 13 times the air temperature 20 ° C and the compression ratio 8 Therefore, the compression ratio is increased as the production of the counter rotating engine 12G compressed air heat exchanger 2Y superheated steam 5H infinitely increased by the most efficient air compression by all rotor blades counter rotating ultra high speed compression, and the compression ratio rises as much as possible. When the compressed air heat exchanger 2Y is aimed at a compression ratio of 80 to 100, which is 10 times 8 and the fuel injection combustion heat exchange superheated steam 5H production experiment, the heat exchange superheated steam is most efficiently produced in the process of increasing the combustion temperature 130 times. 5H production, the same amount of fuel that is important for experimentation There is a possibility of background technology that produces about 5 times the amount of superheated steam 5H of existing boilers, steam turbine power generation of existing thermal power generation alternates between stationary blades and moving blades 2 each It is equipped with front and rear, steam speed is 0, and the stationary blade with rotational output 0 is rotated 20 times before and after 90 degrees direction change injection, and the steam speed is close to 1/30. As the rotor blade counter-rotating engine, the counter-rotating engine 12G, counter-rotating injection engine 12E, counter-rotating air injection engine 12F, etc. with the increase in the production amount of superheated steam 5H and the increase of the injection speed as the core, the same fuel amount already exists. Japan aims to revolutionize global warming, revolutionize economic growth strategy, and achieve the world's most eternal goal of operating profitability, with the aim of revolutionizing revolution and injection propulsion output by two times that of a gas turbine. There is a background technology that can aim to reduce the fiscal deficit of 1,000 trillion yen to 0 in a relatively short period of time.

Aircraft and marine gas turbines with the latest state-of-the-art technology are equipped with alternating stationary blades and moving blades. Air compressors use compressed air to dam the compressed air repeatedly with the stationary blades, and the turbines generate combustion gas. The stationary blades are dammed by 90 degrees and repeat the change of direction, and half of the stationary blades with no work are alternately provided with the moving blades. Since the ship speed is 1/10, etc., it is an air compressor with an extremely high speed that is at least twice the relative speed of the existing rotor blades with ultra-high-speed full rotor blades, and water pipes are used for the inner compressor blades 8q and the outer compressor blades 8r. 5G, the compressed air volume is reduced by cooling the water 52a to reduce the volume of the compressed air or heating the water 52a for superheated steam production. Fuel injection combustion heat exchange, compressed air Exchanger 2Y superheated steam 5H production, heat exchange aiming to raise combustion temperature 130 times, same fuel quantity 130 times superheated steam 5H production quantity of existing boiler, all rotor blades double reversal engine 12G, counter-rotating injection engine 12E, counter-rotating air injection engine 12F, etc., aiming for a revolution of 1000 times with revolution output and injection propulsion output twice that of existing gas turbines, and planes and ships aiming for 10 times speed Aiming for a cosmic flight, the cost of reaching the universe is 1 / 500,000 and the Earth goes 16 times a day. There is a background technology that can be aimed at zeroing in a relatively short period of time.

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: From January 21, 2013, the filing date of Japanese Patent Application No. 2013-8946: 10 items until April 22, 2013 There is an application.

  The existing pumped-storage power generation uses a variable speed motor because the pumping input is proportional to the cube of the rotational speed, so various counter-rotating engines are assumed that the rotational output is proportional to the square of the combustion gas speed. There is a problem to increase the superheated steam 5H speed as much as possible, and the boiler of existing thermal power generation produces superheated steam by atmospheric pressure fuel combustion and power generation by steam turbine drive, but the temperature rise of adiabatic compression is air temperature 20 ° C Is 13 times 260 ° C. with a compression ratio of 8, so that various counter-rotating engines that inject and burn fuel in air with a compression ratio of 80 to 100 will have the same fuel amount as 130 times the amount of superheated steam 5H produced by existing boilers. It is necessary to experiment, and the existing state-of-the-art science and technology airplanes and marine gas turbines are equipped with alternating stationary blades and moving blades. In the bin, the combustion gas is dammed with the stationary blades and rotated 90 degrees repeatedly. The stationary blades with no work are provided in half with the moving blades, and the combustion gas injection speed is set to around 1/10. Since the output and injection propulsion output are 1/100 etc., and the airplane speed and ship speed are 1/10 etc. including the superheated steam production 1/130 etc., the airplane is targeted for 1000 times rotation output and injection propulsion output. And the ship is aiming for 10 times speed, the airplane is in full space flight, the space arrival cost is 1 / 500,000, and the Earth makes 16 laps per day. There is a problem of preventing global warming.

Superheated steam production with compressed air heat exchanger 2Y in various counter-rotating engines, which has a compression ratio that greatly exceeds the existing technology by ultra-high speed counter-rotating all blades, is ultra-high-speed counter rotating and water cooling of the compressor blades. Inner compressor blades 8q + as counter-rotating injection engine 12E, counter-rotating engine 12G and counter-rotating air injection engine 12F aiming at 130 times superheated steam production of existing boilers by ultra-high pressure compression and 10 times combustion gas injection speed The outer compression blade 8r is cooled with water 52a to form a low-temperature compressed air 28a, and the total moving blade ultra-high speed double reversal + superheated steam production amount = 1000 times rotation output and injection propulsion output aiming at a compression ratio of 80 to 100, etc. Then, the fuel is injected and combusted in the compressed air heat exchanger 2Y, and heat is exchanged in the process where the combustion temperature approaches 130 times, and the superheated steam 5H such as 34 MPa is produced most efficiently, and the same fuel amount is 130 times that of the existing thermal power generation boiler. Aiming at production of hot steam 5H, superheated steam 5H + combustion gas 49 is injected according to various applications, and the counter-rotating injection engine 12E, counter-rotating engine 12G and counter-rotating air injection engine 12F are driven, and the experimental results The fuel cost of various vehicles such as automobiles will be a major revolution with 1/100 to 1/2 fuel cost, airplanes and ships aim for 10 times speed, and the airplane will reach a space use cost of 1 / 500,000, and the imitation can be improved Recognizing that the implementation of the invention is obsolete, as a top-secret manufacturing top-secret operation of all inventions that continue to be 100% monopolistic on a global scale, we will prevent global warming forever in the world with an outstanding operating profit rate.

Challenges to produce 130 times the same amount of superheated steam as existing boilers, ultrahigh-pressure counter-rotating + compression blades with water 52a cooling and ultra-high pressure compression, resulting in 1000 times the rotational output and injection propulsion output of existing jets and gas turbines The target effect is large, and the revolution output and injection propulsion output of the same fuel amount is more than twice the existing, and it has the great effect of making the vehicle revolution, ship revolution and airplane revolution, and space utilization by rocket injection of superheated steam 5H The effect that the prime is aimed at is also great, the effect that can be aimed at 100% monopoly manufacturing monopoly operation worldwide is also great, it has the great effect of increasing the employment profit rate in the world and infinite increase in employment, and the effect of preventing global warming is also great.

Explanatory drawing of counter-rotating engine 12G (Example 1) Explanatory drawing of the two-stage compressor 12N (Example 2) Explanatory drawing of counter-rotating injection engine 12E (Example 3) Explanatory drawing of counter-rotating air injection engine 12F (Example 4) Explanatory drawing of contra-rotating automobile 11B (Example 5) Explanatory drawing of counter-rotating ship 11C (Example 6) Explanatory drawing of the contra-rotating jet ship 11F (Example 7) Illustration of contra-rotating airplane 11E (Example 8) Explanatory drawing of the contra-rotating jet airplane 11G (Example 9) Explanatory drawing of the rotary wing airplane 11I (Example 10) Explanatory drawing of the rotary wing jet airplane 11J (Example 11) Illustration of Osprey Extra Large 11M (Example 12) Illustration of Osprey Large 11N (Example 13)

Since there is no precedent for a fully rotating blade counter-rotating engine to generate existing rotational output and injection propulsion output, the entire invention is related to a fully rotating blade counter-rotating engine. Each blade group 60D is provisionally assembled separately, and each end is equipped with various bearings 12C so that it can be rotated and machined by machine tools in the same way as during operation. The most important result is the experimental results centered on a completely new processing technology, and there is no trace of using adiabatic compression air temperature of 20 ° C to 260 ° C, which is 13 times the compression ratio of 8, for superheated steam production. Therefore, the increase in the amount of superheated steam 5H is the most important, and the compressor of various counter-rotating engines whose experimental results are important, aiming to increase the compression air temperature by 130 times by the ultra-high-speed full rotor blade counter-rotating compression. Water for superheated steam production 2a-cooled air-cooled compression using compressed air blades to increase the amount of superheated steam 5H, and to achieve the highest heat exchange that requires an experiment of fuel injection combustion in the compressed air heat exchanger 2Y with a compression ratio of 80 to 100, Aiming to produce 130 times the amount of superheated steam 5H with the same fuel amount as the existing boiler, aiming to produce the superheated steam 5H 130 times the production amount + injection speed 8 times the rotational speed of the existing gas turbine 64 times the same fuel amount Of counter-rotating engine 12G, counter-rotating injection engine 12E and counter-rotating air injection engine 12F, aiming at 1000 times the rotational output and injection propulsion output of As a major revolution, the company will make full-automated mass production of top-secret production vehicles, ships, and airplanes, aiming for the best in the world and an infinite increase in employment.

The contra-rotating engine 12G in FIG. 1 includes an inner shaft device 60A / inner compression blade 8q + outer shaft device 60B / outer compression blade 8r, and an inner shaft device 60A / inner output blade 8s + outer shaft device 60B / outer output blade 8t. Bearings 12C are provided at both ends, and each is separately temporarily assembled into an annular inner output 8s screw assembly fixing or a fitting assembly fixing, and both ends are held by a machine tool. As the counter rotating engine 12G to be assembled, the inner shaft blade 60A + the outer shaft device 60B is counter-rotated by the counter-rotating magnetic device 85 or the counter-rotating gear device 85Y to cool a large number of water 52a. The air 28a sucked from the inlet outer box nozzle 6G is heated by the 8q + outer compression blade 8r to heat the water 52a for production of the linearly cooled compressed superheated steam 5H, and the ultra-high speed counter-rotating linearly cooled compression 2 Compressor 12N connected linear cooling compression, water injection cooling linear compression water cooling from the inner shaft device 60A or outer shaft device 60B can be selected, supplied to the compressed air heat exchanger 2Y at a compression ratio of 80 to 100, etc. After the injection combustion superheated steam pipe 5H and the heat exchange superheated steam 5H are manufactured, the combustion gas 49 is turned to the counter-rotating engine 12G output blade injection drive, and the target amount of superheated steam 5H is 130 times that of the existing thermal power boiler with the same fuel amount. Superheated steam 5H such as 34MPa is injected from superheated steam pipe 5H, combustion gas 49 such as 10MPa is sucked and injected, and the outer output blade 8t and the inner output blade 8s are driven by ultra-high speed counter-rotation, so that the same fuel amount is present. The revolution of the gas turbine will be a major revolution, and the counter-rotating engine 12G will be targeted for 1000 times rotation output.

The two-stage compressor 12N of FIG. 2 includes bearings 12C at both ends of the inner shaft device 60A and inner compression blade 8q + outer shaft device 60B and outer compression blade 8r, and separately attaches and fixes the annular inner compression blade 8q to each other. The two-stage compressor 12N is used as a two-stage compressor 12N which is temporarily assembled in a fitting assembly and fixed to hold both ends with a machine tool and is used for ultra-high speed rotation balance adjustment processing, etc. 85Y causes the inner shaft device 60A and the outer shaft device 60B to be double-reversely driven, and the air 28a sucked from the inlet outer box nozzle 6G is linearly cooled and compressed by the inner compression blades 8q and the outer compression blades 8r cooled by a large number of water 52a. The two-stage compressor 12N ultra-high speed counter-rotating linear cooling compression or connected linear cooling compression is selected, and water jet cooling linear cooling compression cooling water cooling from the inner shaft device 60A or the outer shaft device 60B is selected. As a function, it is supplied to the compressed air heat exchanger 2Y at a compression ratio of 40 to 100 or more, and after producing the fuel injection combustion superheated steam pipe 5H and the heat exchange superheated steam 5H, the counter-rotating engine 12G output blade injection drive of the combustion gas 49 The same fuel amount is connected to the counter-rotating engine 12G, counter-rotating injection engine 12E, counter-rotating air injection engine 12F, etc. as the connected drive aiming at the production amount of superheated steam 5H 130 times that of the existing thermal power boiler, A two-stage compressor 12N used for various applications as a staged air compressor.

The contra-rotating injection engine 12E of FIG. 3 includes an inner shaft device 60A and inner compression blade 8q + outer shaft device 60B and outer compression blade 8r, and an inner shaft device 60A and inner output blade 8s + outer shaft device 60B and outer output blade 8t. Bearings 12C are provided at both ends, each of which is separately assembled into an annular inner output 8s screw assembly fixing or a fitting assembly fixing, etc., and both ends are held by a machine tool. As the counter-rotating injection engine 12E to be assembled in this way, the counter-rotating magnetic device 85 to the counter-rotating gear device 85Y causes the inner shaft device 60A + the outer shaft device 60B to be counter-rotated so that a large number of water 52a is cooled. The air 28a sucked from the inlet outer box nozzle 6G is linearly cooled and compressed by the compression blades 8q and the outer compression blades 8r, and the ultra-high speed counter-rotating linear cooling compression or the two-stage compressor 12N connection linear cooling is performed. Compressed, water injection cooling linear cooling from the inner shaft device 60A or outer shaft device 60B can be selected, compressed water cooling is supplied to the compressed air heat exchanger 2Y at a compression ratio of 80 to 100, etc., and fuel injection combustion overheating After the heat exchange of the steam 5H production, the combustion gas 49 is turned into the counter-rotating injection engine 12E output blade injection drive, the same fuel amount is set to 130 times the superheated steam 5H production amount of the existing thermal power generation boiler, and the superheated steam 5H injection target such as 34 MPa is aimed. As a result, the air 28a is injected and sucked into the rocket outer box 77B, and the combustion gas 49 is sucked and injected by the 8 times superheated steam 5H injection of the existing jet engine. Aiming for high output that requires experimentation, aiming for 1000 times the injection propulsion output of the existing jet engine with the same fuel amount, including 130 times the amount of superheated steam 5H production To double inversion injection engine 12E.

The contra-rotating air injection engine 12F in FIG. 4 includes an inner shaft device 60A and inner compression blade 8q + outer shaft device 60B and outer compression blade 8r, and an inner shaft device 60A and inner output blade 8s + outer shaft device 60B and outer output blade 8t. Bearings 12C are provided at both ends, respectively, and each is separately temporarily assembled into an annular inner output 8s screw assembly fixing or a fitting assembly fixing, and both ends are held by a machine tool, and an ultra-high speed rotation balance adjustment process, etc. As the counter-rotating air injection engine 12F to be assembled as a good balance adjustment, the counter-rotating magnetic device 85 to the counter-rotating gear device 85Y causes the inner shaft device 60A + the outer shaft device 60B to be counter-rotated to drive a large number of water. As the inner compression blades 8q + outer compression blades 8r cooled by 52a, the air 28a sucked from the inlet outer box nozzle 6G is linearly cooled and compressed, and an ultra-high speed counter-rotating linear cooling compressor or a two-stage compressor is used. It is possible to select water jet cooling linear cooling compression water cooling from the inner shaft device 60A or the outer shaft device 60B, and supply to the compressed air heat exchanger 2Y at a compression ratio of 80 to 100, such as 10 MPa. Then, after the fuel injection combustion superheated steam pipe 5H and the heat exchange superheated steam 5H are manufactured, the combustion gas 49 is turned into the counter-rotating air injection engine 12F output blade injection drive, and the superheated steam 5H of 130 times the same fuel amount as the existing thermal power generation boiler is manufactured. As a target, the air 28a is sucked and injected from the inner and outer circumferences of the rocket outer box 77B in the process of injection propulsion by injecting it into the rocket outer box 77B, and combusted by the 8H pressure superheated steam 5H injection of the existing jet engine Gas 49 is sucked and injected, and ships are propelled and propelled, including the amount of superheated steam 5H produced 130 times, and the same fuel amount 1000 times as many as existing jet engines. It aimed at, to double inverted air injection engine 12F of the large output aim necessary experiment.

In the contra-rotating automobile 11B drive of FIG. 5, if the input of the pumped-storage power generation pump is proportional to the cube of the rotational speed, the temperature rise of the adiabatic compression is 260 ° C., the air temperature 20 ° C. is 13 times the compression ratio 8 Utilizing to the limit, aiming at a compression pressure of 10 MPa or more by ultra-high-speed full rotor blade counter-rotating water cooling compression, fuel injection combustion heat exchange in the compressed air heat exchanger 2Y, mass production of superheated steam 5H such as 34 MPa, 34MPa overheating Steam 5H is injected and 10MPa combustion gas 49 is sucked and injected to drive the outer output 8t + inner output blade 8s, and the same fuel amount as a counter-rotating engine 12G driven by the existing micro gas turbine 1000 times rotation output, The reversing engine 12G drives the generator 1 to store in the storage battery 1A to drive the storage battery driving wheel 4J and drive the counter-reversing vehicle 11B. The life is aimed at 1000 times rotation output, and as a strategy for various strategies based on the experimental results, the counter-reversing vehicle 11B is operated in the process of operation by bus, taxi or the like, for example, as a small power plant when operation is stopped.

In the contra-rotating ship 11C drive of FIG. 6, when the pumping power generation pumping pump input is proportional to the cube of the rotational speed, the temperature rise of the adiabatic compression is 260 ° C., which is 13 times the air temperature 20 ° C. Utilizing to the limit, aiming at a compression pressure of 10 MPa or more by ultra-high-speed full rotor blade counter-rotating water cooling compression, fuel injection combustion heat exchange in the compressed air heat exchanger 2Y, mass production of superheated steam 5H such as 34 MPa, 34MPa overheating Inverting engine 12G driven by injecting steam 5H and sucking and injecting 10MPa combustion gas 49, driving outer output 8t + inner output blade 8s, approaching 1000 times rotation output and injection propulsion output of existing gas turbine with same fuel amount As an experiment, the screw 7C is driven with the rotational output of the counter rotating engine 12G and the propulsion is propelled with the exhaust injection output, and the counter rotating ship 11C is propelled with propulsion + screw 7C. In addition, the revolution output and injection propulsion output of the same fuel amount are doubled, and the revolution is 1000 times that of the existing gas turbine, and various strategies based on the experimental results are operated with a target of 1000 km per hour, for example. Reversing ship 11C.

In the contra-rotating jet ship 11F drive of FIG. 7, when the pumped pump power generation pump input is proportional to the cube of the rotational speed, the temperature rise of the adiabatic compression becomes 260 ° C., the air temperature 20 ° C. is 13 times the compression ratio 8 Is used to the limit, with the aim of a compression pressure of 10 MPa or more by ultra-high-speed full-rotary blade counter-rotating water cooling compression, fuel injection combustion heat exchange is performed in the compressed air heat exchanger 2Y, and mass production of superheated steam 5H such as 34 MPa is carried out. 34MP superheated steam 5H is injected into the outer box 77B, the air 28a ahead of the outer periphery of the rocket outer box 77B is sucked and injected, and the exhaust of 10MPa combustion gas 49 is sucked and injected through the inner periphery of the rocket outer box 77B to output outside. 8t + rotational output increase drive of the inner output blade 8s, the same fuel amount as 1000x injection propulsion output of the existing jet engine, the counter-rotating air injection engine 12F drive, In the experiment of the gas propulsion engine 12F injection propulsion output and the propulsion of the counter-inversion injection ship 11F injection propulsion output of the same fuel amount is twice as large as the existing jet engine, and a 1000 times target injection propulsion output For example, a counter-rotating jet ship 11F operated with a target of 1000 km / h is used as a plan for various strategies based on the experimental results.

In the contra-rotating airplane 11E drive of FIG. 8, if the input of the pumped-storage power generation pump is proportional to the cube of the rotational speed, the temperature rise of the adiabatic compression will increase to 260 ° C, which is 13 times the air temperature 20 ° C. Utilizing to the limit, aiming at a compression pressure of 10 MPa or more by ultra-high-speed full rotor blade counter-rotating water cooling compression, fuel injection combustion heat exchange in the compressed air heat exchanger 2Y, mass production of superheated steam 5H such as 34 MPa, 34MPa overheating Steam 5H is injected and 10MPa combustion gas 49 is sucked and injected, and the outer output 8t + inner output blade 8s is driven at ultra high speed counter rotation, aiming at 1000 times rotation output and injection propulsion output of the existing gas turbine with the same fuel amount. As the double reversing engine 12G driving, the propeller 7A is driven by the rotational output of the counter rotating engine 12G and is propelled by the jet propulsion output, and is propelled by the counter rotating airplane 11E and propeller 7A. In the experiment, the revolution output of the same fuel amount and the injection propulsion output are twice as large as the existing gas turbine, and the experiment aimed at 1000 times, for example, the maximum injection amount of superheated steam 5H rocket injection from the current highest flight altitude The flight speed in the vicinity of the vacuum is Mach 32, and the counter-reversing airplane 11E is aimed at the space flight cost 1 / 500,000 aiming at the prime of space flight.

In the contra-rotating jet airplane 11G drive of FIG. 9, when the input of the pumped-storage power pump is proportional to the cube of the rotational speed, the temperature rise of adiabatic compression becomes 260 ° C., which is 13 times the air temperature 20 ° C. and the compression ratio 8 Is used to the limit, with the aim of a compression pressure of 10 MPa or more by ultra-high-speed full-rotary blade counter-rotating water cooling compression, fuel injection combustion heat exchange is performed in the compressed air heat exchanger 2Y, and mass production of superheated steam 5H such as 34 MPa is carried out. 34MP superheated steam 5H is injected into the outer box 77B, the air 28a ahead is sucked and injected, and 10MPa combustion gas 49 exhaust is sucked and injected from the inner periphery of the rocket outer box 77B, and the outer output 8t + inner output blade 8s rotation output is increased. To drive the counter-rotating jet engine 11E, aiming to drive the counter-rotating injection engine 12E with the same fuel amount as 1000 times the propulsion output of the existing jet engine. As an experiment, the same fuel amount injection propulsion output is doubled, and the revolution is set as the maximum injection amount of superheated steam 5H rocket injection from the current highest flight altitude as an experiment aiming for a revolution of 1000 times that of the existing jet engine, and the flight speed near the vacuum is Mach 32 is aiming for the escape speed of the earth, aiming at the prime of space flight, and making it a contra-rotating jet airplane 11G aiming at a space arrival cost of 1 / 500,000.

In the rotary wing airplane 11I drive of FIG. 10, if the input of the pumped-storage pump is proportional to the cube of the rotational speed, the temperature rise of the adiabatic compression is limited to the air temperature 20 ° C becomes 260 ° C, 13 times the compression ratio 8 , Aiming at a compression pressure of 10 MPa or more by super-high-speed all-rotary blade counter-rotating water cooling compression, fuel injection combustion heat exchange in the compressed air heat exchanger 2Y, mass production of superheated steam 5H such as 34 MPa, 34 MPa superheated steam 5H is injected and 10MPa combustion gas 49 is sucked and injected, outer output 8t + inner output blade 8s ultra-high speed double reversal, and exhaust propulsion is performed by exhaust, 1000 times rotation output and injection propulsion output of the same gas amount existing gas turbine As the counter-rotating engine 12G driving, the rotor blade 7B is driven with the rotating output of the counter-rotating engine 12G, and the exhaust propelling is performed for the propulsion, and the rotor blade 11I injection propulsion + rotating blade is performed. 7B propulsion experiment, the revolution output of the same fuel amount and injection propulsion output is twice as large as the existing gas turbine, and the experiment aiming for 1000 times the revolution, and superheated steam 5H rocket injection maximum injection from the current highest flight altitude In terms of quantity, the rotary wing airplane 11I is aimed at a space flight prime aiming at the earth escape speed of Mach 32 and a space arrival cost of 1 / 500,000.

In the rotary wing jet airplane 11J drive of FIG. 11, if the input of the pumped-storage pump is proportional to the cube of the rotational speed, the temperature rise of adiabatic compression will be 260 ° C, which is 13 times the air temperature 20 ° C. Utilizing to the limit, aiming at a compression pressure of 10MPa or more by ultra-high-speed full rotor blade counter-rotating water cooling compression, fuel injection combustion heat exchange with compressed air heat exchanger 2Y, mass production of superheated steam 5H such as 34MPa, outside the rocket 34MP superheated steam 5H is injected into the box 77B, the air 28a ahead is sucked and injected, and 10MPa combustion gas 49 exhaust is sucked and injected from the inner periphery of the rocket outer box 77B, and the rotational output of the outer output 8t + inner output blade 8s is increased. As a counter-rotating injection engine 12E drive, aiming at 1000 times the injection propulsion output of the existing jet engine with the same fuel amount, injecting with the counter-rotating injection engine 12E injection propulsion output In the experiment of propulsion and counter-inversion jet airplane 11J injection propulsion, the same fuel amount injection propulsion output is twice that of the existing jet engine, and the experiment aiming for a revolution of 1000 times, superheated steam from the current highest flight altitude As the 5H rocket injection maximum injection amount, the flight speed near the vacuum is set to the earth escape speed of Mach 32, and the space flight prime is targeted.

The Osprey extra large 11M drive in FIG. 12 is the limit of the adiabatic compression temperature rise to 260 ° C, which is 13 times the compression ratio of 8 ° C, as the pump input of the pumped pump is proportional to the cube of the rotational speed. Utilizing ultra high-speed full rotor blades with counter-inverted water cooling compression, aiming at a compression pressure of 10 MPa or more, fuel injection combustion heat exchange with the compressed air heat exchanger 2Y, mass production of superheated steam 5H such as 34 MPa, 34 MPa superheated steam 5H 10MPa combustion gas 49 is sucked and injected, and the outer output 8t + inner output blade 8s are injected and propelled by ultra-high speed counter-rotating drive exhaust, aiming at the same fuel amount 1000 times rotation output and injection propulsion output of the existing gas turbine. As a counter-rotating engine 12G drive, the propeller 7A is driven by the counter-rotating engine 12G rotation output to make the propulsion propulsion by the injection propulsion output, and the Osprey extra large 11M injection propulsion + professional In the experiment for propeller 7A propulsion, the revolution output of the same fuel amount and the injection propulsion output are twice as large as the existing gas turbine, and the experiment aimed at 1000 times revolution, the superheated steam 5H rocket injection maximum injection amount from the highest flight altitude The flight speed in the vicinity of the vacuum is set to an Osprey extra large 11M aiming at a space arrival cost of 1 / 500,000 aiming for the space flight prime aiming at the earth escape speed of Mach 32.

The Osprey large-scale 11N drive in FIG. 13 reaches the limit of the temperature rise of adiabatic compression when the input of the pumped-storage pump is proportional to the cube of the rotational speed, and the air temperature 20 ° C becomes 260 ° C, 13 times the compression ratio 8 Utilizing ultra high speed full rotor blades with counter-inverted water cooling compression, aiming at a compression pressure of 10 MPa or more, fuel injection combustion heat exchange with compressed air heat exchanger 2Y, mass production of superheated steam 5H such as 34 MPa, rocket outer box 77B 34MP superheated steam 5H is injected into the air 28a in front of the suction, 10MPa combustion gas 49 exhaust is sucked and injected from the inner periphery of the rocket outer box 77B, and the outer output 8t + inner output blade 8s is driven to increase the rotational output. Osprey large 11N injection with the same fuel amount as the counter-rotating injection engine 12E injection propulsion + propeller 7A drive, aiming at 1000 times the injection propulsion output of the existing jet engine In the experiment to make a propulsion, the fuel injection propulsion output of the same fuel amount is twice that of the existing jet engine, the revolution is 1000 times, and the superheated steam 5H rocket injection maximum injection amount from the highest flight altitude is near the vacuum The Osprey large size 11N aiming at a space arrival cost of 1 / 500,000, aiming for the space flight prime aiming at the flight speed of Mach 32.

Since the existing state-of-the-art science and technology is too unreasonable, the estimated power generation amount is enormous, and experiments are necessary. As the counter-rotating engine 12G, counter-rotating injection engine 2E and counter-rotating air injection engine 12F, airplanes There is a possibility of driving secret ships and vehicles, and approaching the 1000 times rotation output and injection propulsion output of an existing gas turbine of the same fuel amount, etc., and performing top secret manufacturing and top secret operation.

0: Various energy storage cycle coalesced engine (various heat energy is compressed and recovered by heat pump as air temperature, divided into air 28a cold heat + superheated steam 50 heat, and gravitational energy is accelerated and accelerated by gravitational acceleration in vacuum 1) Generator, 1c: Liquid fuel, 1e: Factory power generation, 1f: Horizontal shaft bearing 0 approach (horizontal shaft bearing + thrust bearing + electromagnet bearing load 0) 1h: Horizontal axis (axis that alternates the rotation direction of the outer shaft device and the inner shaft device) 1A: Storage battery, 1D: Fuel injection pump, 1H: In-house power generation, 1K: Liquid fuel control valve, 1L: High-pressure fuel heating pipe , 1M: Osprey extra large, 1N: Osprey large size, 2A: heat-resistant material, 2C: 1 to multi-stage compression heat recovery device (thermal energy is air temperature and multiple times with heat pump Heat recovered multiple times with a heat exchanger and the remainder is divided and stored as hot 50 + liquid cold 28a 2Y: compressed air heat exchanger (high-pressure air 28a cold + superheated steam 50 hot) 2b: little water resistance (air on the bottom of the ship) 2c: Insulating material, 2d: Long lens (Convex lens cross section is a straight extension rectangle, multiple lenses are used to aim at the shortest focal length lens width) 3d : Combined turbine, 3e: Two-stage compressor, 3s: Simple compressor, 3u: Turbine, 3E: Specific critical substances (specific critical substances that are liquid at room temperature such as mercury and water) 3E: Specific critical substances (500 of low melting point alloy) 3Q: Theoretical expansion engine (best target by Boyle's law) 3R: Theoretical gas turbine, 3S: Theoretical steam turbine, 3T: Theoretical gas compressor, 3U: Theoretical tank Bin, 4H: Heat absorption tube (The long lens 2d linearly collects sunlight into the heat absorption tube and heats the air temperature inside the tube to the maximum to increase the outside air temperature.) 4J: Battery drive wheel, 4L: Theory Expansion engine vehicle, 4M: Theoretical turbine vehicle, 4Q: Theoretical combustion chamber (combustion chamber aiming at the 20% pressure superheated steam injection, etc., and the conventional air-fuel ratio combustion in the superheated steam production), 4T: Axial flow double reversal Compressor, 4V: Axial flow counter-rotating turbine, 4d: Gear device, 4e: Roller, 4f: Rotation support, 5: Air injection nozzle, 5b: Compressed air passage, 5G: Steam heating pipe, 5G: Water pipe, 5H : Superheated steam, 5H: Superheated steam pipe, 5J: Compressed air superheated pipe, 5M: High pressure high temperature combustion chamber, 5Q: High pressure high temperature water control valve, 5S: Compressed air heating pipe, 5V: Compressed air control valve, 5Z: Water pump , 6 Final compression blade, 6A: Superheated steam rocket nozzle (injection nozzle capable of reverse injection depending on application) 6B: Compressed air injection nozzle, 6F: Water injection nozzle, 6G: Outer box nozzle, 6H: Drain pipe, 6W: Acceleration of specific material Machine, 6X: fuel injection nozzle, 6Y: combustion gas injection nozzle, 6Z: superheated steam injection nozzle, 7A: propeller, 7B: rotating blade, 7C: screw, 8a: turbine blade, 8d: upper expansion blade group, 8e: lower Side expansion blade group, 8f: Assembly turbine blade group, 8g: Upper compression blade group, 8h: Lower compression blade group, 8j: Assembly compression blade group, 8k: Inner compression blade (equipped with both-side center support inner shaft device) 8m: Outer compression blades (both center support outer shaft devices included), 8n: Inner output blade (both center support inner shaft devices included), 8p: Outer output blades (both center support outer shaft devices included) 8q: Inner Compressor blade (compressed blade with angle, curve and rotational radius tuned according to rotational speed and peripheral speed) 8r: Outer compressed blade (angle, curve and rotational radius tuned according to rotational speed and peripheral speed) Compression blade), 8s: inner output blade (angle and curve according to rotational speed and circumferential speed, output blade with rotational radius double inverted), 8t: outer output blade (angle and curve according to rotational speed and circumferential speed) 9B: Electromagnet permanent magnet, 9C: Electromagnet permanent magnet, 9D: Pneumatic part, 9E: Pneumatic part, 9M: Fitting assembly part, 9Q: Vertical parallel plate, 9b: Top suction Lower repulsion magnet, 9c: Suction magnet, 9d: Repulsion magnet, 11: Full bucket steam turbine, 11B: Counter rotating vehicle, 11C: Counter rotating vessel, 11D: Condenser, 11E: Counter rotating aircraft, 11F : Contra-rotating jet ship, 11 : Contra-rotating jet airplane, 11I: rotary wing airplane, 11J: rotary wing jet airplane, 11M: extra large Osprey, 11N: large Osprey, 12: gravity power generation building, 12A: steel frame, 12B: column tube, 12C: bearing, 12D: Square flange, 12E: Counter-rotating injection engine, 12F: Counter-rotating air injection engine, 12G: Counter-rotating engine, 12N: Two-stage compressor, 21: Solar heater (intake air path through heat absorption tube) 24A: compressed air control valve, 25: superheated steam control valve, 25b: high pressure fuel control valve, 25c: fuel pipe, 28A: intake air passage, 28a: air, 28b: intake air Road, 29a: super high pressure air, 38H: theoretical screw ship, 38J: theoretical injection ship, 38T: theoretical injection airplane, 38U: theoretical propeller airplane 49: combustion gas, 50: superheated steam, 50: superheated steam chamber, 50A: high-pressure high-temperature water, 50a: superheated steam injection pipe, 52a: water, 52b: high-temperature water, 60A: inner shaft device, 60B: outer shaft device , 60G: outer annular blade, 60H: inner annular blade, 77A: gas turbine outer box, 77B: rocket outer box, 77C: counter-rotating machine outer box, 77G: cylindrical rotating part, 77a: turbine outer box, 77b: compression Outer box, 80: Bearing (Bearing load as close to 0 as possible using magnetic force + air pressure) 80A: Joint, 80B: Fastener, 80a: Thrust bearing (Bearing load as much as possible using magnetic force + air pressure) 85: Counter-rotating magnetic device (magnet-utilized gear height is slight to non-contact and rotating in the opposite direction with the horizontal shaft 1h gear) 85Y: Counter-rotating gear device (horizontal shaft 1h gear) More to mutually reverse rotation) 88B: steam combined air injection unit, 88C: the theoretical air injection unit, 88L: steam combined water injection unit, 88M: Theoretical water injection unit, 89A: Liquid oxygen production unit

Claims (574)

  Various energy storage cycle merging engines and merging methods as a counter-rotating water-cooled blade compression counter-rotating engine (12G) having bearings (12C) at both ends and enabling temporary assembly processing.   Various energy storage cycle merging engines and merging methods as a two-stage compressor (12N) of counter-rotating water-cooled blade compression equipped with bearings (12C) at both ends and enabling temporary assembly processing.   Various energy storage cycle merging engines and merging methods as a counter-rotating water-cooled blade-compressed counter-rotating injection engine (12E) having bearings (12C) at both ends and enabling temporary assembly processing.   Various energy storage cycle merging engines and merging methods as a counter-rotating water-cooled blade compression counter-rotating air injection engine (12F) equipped with bearings (12C) at both ends to enable temporary assembly processing.   Bearings (12C) at both ends to enable temporary assembly processing Various energy conservation cycle coalescing engines with a counter-rotating engine (12G) having a compression part as a two-stage compressor (12N) for counter-rotating water cooling blade compression And coalescing method.   Combined with various energy storage cycles with a counter-rotating injection engine (12E) having bearings (12C) at both ends to enable temporary assembly processing, and the compression part is a two-stage compressor (12N) of counter-rotating water cooling blade compression Organization and coalescence method.   Various energy storage cycles with a counter-rotating air injection engine (12F) with bearings (12C) at both ends and a compression section that is a two-stage compressor (12N) for counter-rotating water cooling blade compression that enables temporary assembly. Merger engine and merger method.   Various energy storage cycle coalescence engine and coalescence method as a counter-rotating automobile (11B) equipped with a counter-rotating water cooling blade compression counter-rotating engine (12G) equipped with bearings (12C) at both ends and enabling temporary assembly processing .   Various energy storage cycle coalescence engines and coalescence methods including a counter rotating water cooled blade compression counter rotating engine (12G) and counter rotating ship (11C) equipped with bearings (12C) at both ends and enabling temporary assembly processing .   Various energy storage cycle coalescence engine and coalescence method as a counter-rotating aircraft (11E) equipped with a counter rotating water cooling blade compression counter rotating engine (12G) equipped with bearings (12C) at both ends and enabling temporary assembly processing .   Various energy storage cycle coalescence engines and coalescence methods comprising a counter rotating engine (12G) with a counter rotating water cooled blade compression equipped with bearings (12C) at both ends and enabling temporary assembly processing, and a rotor blade airplane (11I).   Various energy storage cycle merging engines and merging methods such as a counter rotating water-cooled blade compression counter rotating engine (12G) equipped with bearings (12C) at both ends and an Osprey extra large (11M).   Various energy storage cycle coalescence engines including a counter-rotating water-cooled blade compression counter-rotating injection engine (12E) and counter-rotating injection ship (11F) equipped with bearings (12C) at both ends and enabling temporary assembly processing; Merge method.   Various energy storage cycle coalescing engines including a counter rotating water cooled blade compression counter rotating injection engine (12E) and counter rotating injection airplane (11G) equipped with bearings (12C) at both ends and enabling temporary assembly processing; Merge method.   Various energy storage cycle coalescence engines and coalescence with a counter rotating water injection vane compression engine (12E) equipped with bearings (12C) at both ends and enabling temporary assembly processing, and a rotary blade injection airplane (11J) Method.   Various energy storage cycle coalescence engines and coalescence methods including a counter rotating water-cooled blade compression contra-rotating injection engine (12E) equipped with bearings (12C) at both ends and an Osprey large size (11N).   Various energy storage cycle coalescence engines equipped with counter-rotating water-cooled blade compression counter-rotating air injection engine (12F) and counter-rotating injection ship (11F) equipped with bearings (12C) at both ends to enable temporary assembly processing And coalescing method.   A counter rotating engine (12G) of a counter rotating water cooling blade compressed with a bearing (12C) at both ends and enabling temporary assembly processing (12G), an outer compressing blade (8r) of cooling water (52a), an inner compressing blade (8q), and Various energy storage cycle coalescence engines and coalescence methods.   A counter rotating engine (12G) of a counter rotating water cooling blade (12a) that is provided with bearings (12C) at both ends to enable provisional assembly processing, and a water (52a) cooling outer compression blade (8r) and an inner compressing blade (8q). Various energy storage cycle coalescence engines and coalescence methods.   Bearings (12C) are provided at both ends, enabling temporary assembly processing. Outer compression of counter-rotating engine (12G) water (52a) cooling with compression section as two-stage compressor (12N) of counter-rotating water cooling blade compression Various energy storage cycle coalescing engines and coalescence methods as wings (8r) inner compression wings (8q).   Bearings (12C) are provided at both ends, enabling temporary assembly processing. Outer compression of counter-rotating engine (12G) water (52a) cooling with compression section as two-stage compressor (12N) of counter-rotating water cooling blade compression Various energy storage cycle coalescing engine and coalescence method for the blade (8r) inner compression blade (8q).   Provided with bearings (12C) at both ends to enable provisional assembly processing. A counter rotating engine (12G) having a compression section made of a two-stage compressor (12N) for counter rotating water cooling blade compression. Counter rotating vehicle (11B) Various energy storage cycle coalescence engines and coalescence methods.   Provided with bearings (12C) at both ends to enable temporary assembly processing. Provided with a counter-rotating engine (12G) having a compression section of a two-stage compressor (12N) for counter-rotating water cooling blade compression. Counter-rotating ship (11C) Various energy storage cycle coalescence engines and coalescence methods.   Provided with bearings (12C) at both ends to enable provisional assembly processing. Compressed part is a two-stage compressor (12N) with a counter-rotating water cooling blade compression. A counter-rotating airplane (11E) is equipped with a counter-rotating engine (12G). Various energy storage cycle coalescence engines and coalescence methods.   A rotary wing airplane (11I) equipped with a counter rotating engine (12G) having bearings (12C) at both ends and capable of temporary assembly processing and having a compression section as a two stage compressor (12N) of a counter rotating water cooled blade compression; Various energy storage cycle coalescence engines and coalescence methods.   Provided with bearings (12C) at both ends to enable provisional assembly processing The compression section is a double-reversed engine (12G) with a double-stage water-cooled blade compression two-stage compressor (12N) and an Osprey extra large (11M) Various energy storage cycle coalescence engines and coalescence methods.   Provided with bearings (12C) at both ends to enable temporary assembly processing. A counter-rotating jet ship (12E) having a counter-rotating water-cooled blade compression two-stage compressor (12N). 11F) various energy storage cycle coalescence engines and coalescence methods.   Provided with bearings (12C) at both ends to enable temporary assembly processing. A counter-rotating jet airplane (12E) having a counter-rotating water-cooled blade compression two-stage compressor (12N) having a counter-rotating jet engine (12E) 11G) various energy storage cycle coalescence engines and coalescence methods.   Provided with bearings (12C) at both ends to enable temporary assembly processing. Rotating blade injection airplane (11J) equipped with counter rotating injection engine (12E) having a compression section made of a two-stage compressor (12N) of counter rotating water cooling blade compression. ) Various energy storage cycle coalescence engines and coalescence methods.   Osprey large size (11N) equipped with a counter-rotating injection engine (12E) having a bearing (12C) at both ends to enable temporary assembly processing and having a compression part as a two-stage compressor (12N) for counter-rotating water cooling blade compression; Various energy storage cycle coalescence engines and coalescence methods.   A counter-rotating jet ship equipped with a counter-rotating air injection engine (12F) having bearings (12C) at both ends and capable of provisional assembly processing, and the compression part being a two-stage compressor (12N) of counter-rotating water cooling blade compression (11F) Various energy storage cycle coalescence engines and coalescence methods.   A counter-rotating water cooling blade compression counter rotating engine (12G) water (52a) cooling outer compression blade (8r) inner compression blade (8q) cooling provided with bearings (12C) at both ends to enable temporary assembly processing. Various energy storage cycle coalescence engines and coalescence methods as wings.   A counter-rotating water cooling blade compression counter rotating engine (12G) water (52a) cooling outer compression blade (8r) inner compression blade (8q) cooling provided with bearings (12C) at both ends to enable temporary assembly processing. Various energy storage cycle coalescence engines and coalescence methods as compression blades.   Bearings (12C) are provided at both ends, enabling temporary assembly processing. Outer compression of counter-rotating engine (12G) water (52a) cooling with compression section as two-stage compressor (12N) of counter-rotating water cooling blade compression Various energy storage cycle coalescing engine and coalescence method using a blade (8r) inner compression blade (8q) cooling blade.   Bearings (12C) are provided at both ends, enabling temporary assembly processing. Outer compression of counter-rotating engine (12G) water (52a) cooling with compression section as two-stage compressor (12N) of counter-rotating water cooling blade compression Various energy storage cycle coalescing engine and coalescence method as a blade (8r) inner compression blade (8q) cooled compression blade.   Combined with various energy storage cycles as a counter rotating engine (12G) for counter rotating water cooling blade compression equipped with bearings (12C) at both ends and enabling temporary assembly processing by annular inner compression blade (8q) screw assembly fixing etc. Organization and coalescence method.   Combined with various energy storage cycles as a two-stage compressor (12N) of counter-rotating water-cooled blades equipped with bearings (12C) at both ends and enabling temporary assembly by annular inner compression blades (8q) screw assembly fixing etc. Organization and coalescence method.   Various energy storage cycles as a counter-rotating water-cooled-blade-compressed counter-rotating injection engine (12E) equipped with bearings (12C) at both ends and temporarily assembled by an annular inner compressor blade (8q) screw assembly and fixing. Merger engine and merger method.   Various types of energy storage as a counter-rotating water-cooled-blade-compressed counter-rotating air injection engine (12F) equipped with bearings (12C) at both ends and enabling temporary assembly by annular inner compression blade (8q) screw assembly and fixing. Cycle coalescence engine and coalescence method.   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner compression blade (8q) screw etc. Various energy storage cycle coalescence engine and coalescence method as an engine (12G).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner compression blade (8q) screw etc. Various energy storage cycle coalescence engines and coalescence methods as an injection engine (12E).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner compression blade (8q) screw etc. Various energy storage cycle coalescence engine and coalescence method as an air injection engine (12F).   Double reversing water (52a) cooling reversing blade compression reversing engine (12G) equipped with bearings (12C) at both ends and enabling temporary assembly by annular inner compression blade (8q) screw assembly fixing, etc. Various energy storage cycle coalescence engine and coalescence method as a reversing automobile (11B).   Double reversing water (52a) cooling reversing blade compression reversing engine (12G) equipped with bearings (12C) at both ends and enabling temporary assembly by annular inner compression blade (8q) screw assembly fixing, etc. Various energy conservation cycle coalescence engine and coalescence method as an inverted ship (11C).   Double reversing water (52a) cooling reversing blade compression reversing engine (12G) equipped with bearings (12C) at both ends and enabling temporary assembly by annular inner compression blade (8q) screw assembly fixing, etc. Various energy conservation cycle coalescence engine and coalescence method as a reversal airplane (11E).   A rotor (12G) with counter rotating water (52a) for cooling and compression blade compression, which has bearings (12C) at both ends and can be temporarily assembled by an annular inner compressor blade (8q) screw assembly and fixing. Various energy storage cycle coalescence engine and coalescence method as an airplane (11I).   Bearings (12C) at both ends and an annular inner compression blade (8q) screw assembly assembly fixed, etc. allows counter assembly water (52a) Cooling compression blade compression counter rotation engine (12G) Osprey extra large (11M) Various energy storage cycle coalescence engines and coalescence methods.   Two reversing water (52a) cooled reversible compression blade compression reversal injection engine (12E) equipped with bearings (12C) at both ends and temporarily assembled by annular inner compression blade (8q) screw assembly and fixing, etc. Various energy conservation cycle coalescence engine and coalescence method as a heavy reversal jet ship (11F).   Two reversing water (52a) cooled reversible compression blade compression reversal injection engine (12E) equipped with bearings (12C) at both ends and temporarily assembled by annular inner compression blade (8q) screw assembly and fixing, etc. Various energy storage cycle coalescence engine and coalescence method as a heavy inversion jet airplane (11G).   A counter rotating water (52a) with a counter rotating injection engine (12E) equipped with bearings (12C) at both ends and enabling temporary assembly by an annular inner compressor blade (8q) screw assembly fixing, etc. Various energy conservation cycle coalescence engine and coalescence method as a wing jet airplane (11J).   Osprey equipped with a counter rotating water (52a) cooling compressor blade compression counter rotating injection engine (12E) equipped with bearings (12C) at both ends and temporarily assembled by an annular inner compressor blade (8q) screw assembly and fixing. Various energy conservation cycle coalescence engines and coalescence methods of large size (11N).   Provided with bearings (12C) at both ends and a counter-rotating water (52a) with a counter-rotating air injection engine (12F) for cooling / compressing compressor blades, which can be temporarily assembled by an annular inner compressor blade (8q) screw assembly and fixing. Various energy conservation cycle coalescence engine and coalescence method as a counter-rotating jet ship (11F).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner compression blade (8q) screw etc. Various energy storage cycle coalescence engine and coalescence method as an engine (12G) equipped counter-rotating automobile (11B).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner compression blade (8q) screw etc. Various energy storage cycle coalescing engine and coalescence method as an engine (12G) equipped counter-reversing ship (11C).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner compression blade (8q) screw etc. Various energy storage cycle coalescence engine and coalescence method as an engine (12G) equipped contra-rotating airplane (11E).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner compression blade (8q) screw etc. Various energy storage cycle coalescing engine and coalescence method as engine (12G) equipped rotor blade airplane (11I).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner compression blade (8q) screw etc. Various energy storage cycle coalescing engine and coalescence method as an engine (12G) equipped Osprey extra large (11M).   A counter-rotating jet comprising a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that can be temporarily assembled by an annular inner compressor blade (8q) screw assembly and fixing. Various energy storage cycle coalescing engine and coalescence method as an engine (12E) equipped counter-rotating jet ship (11F).   A counter-rotating jet comprising a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that can be temporarily assembled by an annular inner compressor blade (8q) screw assembly and fixing. Various energy storage cycle coalescing engine and coalescence method as engine (12E) equipped counter-rotating jet airplane (11G).   A counter-rotating jet comprising a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that can be temporarily assembled by an annular inner compressor blade (8q) screw assembly and fixing. Various energy storage cycle coalescing engine and coalescence method as engine (12E) equipped rotor blade jet airplane (11J).   A counter-rotating jet comprising a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that can be temporarily assembled by an annular inner compressor blade (8q) screw assembly and fixing. Various energy storage cycle coalescing engine and coalescence method with engine (12E) equipped osprey large (11N).   Double reversal air having bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversal water cooling blades of the compression section so that temporary assembly can be performed by assembling and fixing the annular inner compression blade (8q) screw. Various energy storage cycle coalescing engines and coalescence methods, including an injection engine (12F) and a counter-rotating jet ship (11F).   Various types of counter-rotating engine (12G) for counter rotating water (52a) cooling compression blade compression equipped with bearings (12C) at both ends and enabling temporary assembly by annular outer compression blade (8r) screw assembly and fixing. Energy conservation cycle coalescence engine and coalescence method.   Various types of counter-rotating water (52a) cooling compression blade compression two-stage compressor (12N) equipped with bearings (12C) at both ends and capable of temporary assembly by annular outer compression blade (8r) screw assembly and fixing Energy conservation cycle coalescence engine and coalescence method.   The counter-rotating water (52a) is a counter-rotating injection engine (12E) for cooling compression blade compression that has bearings (12C) at both ends and can be temporarily assembled by an annular outer compression blade (8r) screw assembly and fixing. Various energy storage cycle coalescence engines and coalescence methods.   A counter-rotating water (52a) counter-rotating air jet engine (12F) for compressing a cooling compressor blade, which has bearings (12C) at both ends and can be temporarily assembled by an annular outer compressor blade (8r) screw assembly fixing, etc. Various energy storage cycle coalescence engines and coalescence methods.   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be done by screwing and fixing the annular outer compression blade (8r) Various energy storage cycle coalescence engine and coalescence method as an engine (12G).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be done by screwing and fixing the annular outer compression blade (8r) Various energy storage cycle coalescence engines and coalescence methods as an injection engine (12E).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be done by screwing and fixing the annular outer compression blade (8r) Various energy storage cycle coalescence engine and coalescence method as an air injection engine (12F).   Double reversing water (52a) cooling reversing compression blade reversing engine (12G) equipped with bearings (12C) at both ends and temporarily assembled by annular outer compression blade (8r) screw assembly fixing etc. Various energy storage cycle coalescence engine and coalescence method as a reversing automobile (11B).   Double reversing water (52a) cooling reversing compression blade reversing engine (12G) equipped with bearings (12C) at both ends and temporarily assembled by annular outer compression blade (8r) screw assembly fixing etc. Various energy conservation cycle coalescence engine and coalescence method as an inverted ship (11C).   Double reversing water (52a) cooling reversing compression blade reversing engine (12G) equipped with bearings (12C) at both ends and temporarily assembled by annular outer compression blade (8r) screw assembly fixing etc. Various energy conservation cycle coalescence engine and coalescence method as a reversal airplane (11E).   A rotor (12G) having a counter rotating engine (12G) for compressing and compressing compressed air that has bearings (12C) at both ends and is capable of temporary assembly by an annular outer compressor blade (8r) screw assembly and fixing. Various energy storage cycle coalescence engine and coalescence method as an airplane (11I).   Bearings (12C) at both ends and an annular outer compression blade (8r) screw assembly and fixing, enabling counter assembly processing (52a) Cooling compression blade compression counter rotation engine (12G) Osprey extra large (11M) Various energy storage cycle coalescence engines and coalescence methods.   A counter rotating water (52a) with a bearing (12C) at both ends and an annular outer compression blade (8r) screw assembly fixing and the like enabling temporary assembly processing. Various energy conservation cycle coalescence engine and coalescence method as a heavy reversal jet ship (11F).   A counter rotating water (52a) with a bearing (12C) at both ends and an annular outer compression blade (8r) screw assembly fixing and the like enabling temporary assembly processing. Various energy storage cycle coalescence engine and coalescence method as a heavy inversion jet airplane (11G).   A counter rotating water (52a) with a rotating reversing injection engine (12E) equipped with bearings (12C) at both ends and temporarily assembled by an annular outer compression vane (8r) screw assembly fixing, etc. Various energy conservation cycle coalescence engine and coalescence method as a wing jet airplane (11J).   Osprey equipped with counter rotating water (52a) cooling compressor blade compression counter rotating injection engine (12E) equipped with bearings (12C) at both ends and temporarily assembled by annular outer compression blade (8r) screw assembly fixing etc. Various energy conservation cycle coalescence engines and coalescence methods of large size (11N).   Provided with bearings (12C) at both ends and a counter-rotating water (52a) cooling-compressing-blade compression counter-rotating air injection engine (12F) which can be temporarily assembled by an annular outer compressor blade (8r) screw assembly and fixing. Various energy conservation cycle coalescence engine and coalescence method as a counter-rotating jet ship (11F).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be done by screwing and fixing the annular outer compression blade (8r) Various energy storage cycle coalescence engine and coalescence method as an engine (12G) equipped counter-rotating automobile (11B).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be done by screwing and fixing the annular outer compression blade (8r) Various energy storage cycle coalescing engine and coalescence method as an engine (12G) equipped counter-reversing ship (11C).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be done by screwing and fixing the annular outer compression blade (8r) Various energy storage cycle coalescence engine and coalescence method as an engine (12G) equipped contra-rotating airplane (11E).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be done by screwing and fixing the annular outer compression blade (8r) Various energy storage cycle coalescing engine and coalescence method as engine (12G) equipped rotor blade airplane (11I).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be done by screwing and fixing the annular outer compression blade (8r) Various energy storage cycle coalescing engine and coalescence method as an engine (12G) equipped Osprey extra large (11M).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be done by screwing and fixing the annular outer compression blade (8r) Various energy conservation cycle coalescing engines and coalescence methods, including an injection engine (12E) and a counter-rotating jet ship (11F).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be done by screwing and fixing the annular outer compression blade (8r) Various energy storage cycle coalescing engines and coalescence methods, including an injection engine (12E) and a counter-rotating jet airplane (11G).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be done by screwing and fixing the annular outer compression blade (8r) Various energy conservation cycle coalescing engines and coalescence methods, including an injection engine (12E) equipped with a rotor blade jet airplane (11J).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be done by screwing and fixing the annular outer compression blade (8r) Various energy storage cycle coalescing engine and coalescence method with injection engine (12E) and large osprey (11N).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be done by screwing and fixing the annular outer compression blade (8r) Various energy conservation cycle coalescing engines and coalescence methods, which are air injection engines (12F) and counter-rotating jets (11F).   Various types of counter-rotating engine (12G) with counter-rotating water (52a) cooling compression blade compression equipped with bearings (12C) at both ends and enabling temporary assembly by annular outer output blade (8t) screw assembly fixing etc. Energy conservation cycle coalescence engine and coalescence method.   Various types of counter-rotating water (52a) cooling compressor blade compression two-stage compressor (12N) equipped with bearings (12C) at both ends and capable of temporary assembly processing by annular outer output blade (8t) screw assembly and fixing Energy conservation cycle coalescence engine and coalescence method.   The counter-rotating water (52a) is a counter-rotating injection engine (12E) for compressing compressed air compressors that has bearings (12C) at both ends and can be temporarily assembled by fixing the annular outer output blade (8t) with screws. Various energy storage cycle coalescence engines and coalescence methods.   A counter-rotating water (52a) cooling-compressed-blade-compressed counter-rotating air injection engine (12F) having bearings (12C) at both ends and enabling temporary assembly by annular outer output blade (8t) screw assembly fixing, etc. Various energy storage cycle coalescence engines and coalescence methods.   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be performed by screwing and fixing the annular outer output blade (8t). Various energy storage cycle coalescence engine and coalescence method as an engine (12G).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be performed by screwing and fixing the annular outer output blade (8t). Various energy storage cycle coalescence engines and coalescence methods as an injection engine (12E).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be performed by screwing and fixing the annular outer output blade (8t). Various energy storage cycle coalescence engine and coalescence method as an air injection engine (12F).   Double reversing water (52a) cooling reversing blade compression reversing engine (12G) equipped with bearings (12C) at both ends and temporarily assembled by annular outer output blade (8t) screw assembly fixing etc. Various energy storage cycle coalescence engine and coalescence method as a reversing automobile (11B).   Double reversing water (52a) cooling reversing blade compression reversing engine (12G) equipped with bearings (12C) at both ends and temporarily assembled by annular outer output blade (8t) screw assembly fixing etc. Various energy conservation cycle coalescence engine and coalescence method as an inverted ship (11C).   Double reversing water (52a) cooling reversing blade compression reversing engine (12G) equipped with bearings (12C) at both ends and temporarily assembled by annular outer output blade (8t) screw assembly fixing etc. Various energy conservation cycle coalescence engine and coalescence method as a reversal airplane (11E).   Rotor blades equipped with counter rotating water (52a) cooling compression blade compression counter rotating engine (12G) with bearings (12C) squeezed at both ends to allow temporary assembly by annular outer output blade (8t) screw assembly fixing, etc. Various energy storage cycle coalescence engine and coalescence method as an airplane (11I).   Bearings (12C) at both ends, annular outer output blade (8t), counter-rotating water (52a) with cooling / compressing blade compression counter-rotating engine (12G), enabling temporary assembly by screw assembly fixing Osprey extra large (11M) Various energy storage cycle coalescence engines and coalescence methods.   Two reversing water (52a) cooled reversible compression blade compression reversal injection engine (12E) equipped with bearings (12C) at both ends and temporarily assembled by an annular outer output blade (8t) screw assembly fixing, etc. Various energy conservation cycle coalescence engine and coalescence method as a heavy reversal jet ship (11F).   Two reversing water (52a) cooled reversible compression blade compression reversal injection engine (12E) equipped with bearings (12C) at both ends and temporarily assembled by an annular outer output blade (8t) screw assembly fixing, etc. Various energy storage cycle coalescence engine and coalescence method as a heavy inversion jet airplane (11G).   A counter rotating water (52a) with a counter rotating injection engine (12E) for cooling and compression blade compression, which has bearings (12C) at both ends and can be temporarily assembled by an annular outer output blade (8t) screw assembly and fixing. Various energy conservation cycle coalescence engine and coalescence method as a wing jet airplane (11J).   Osprey with counter-rotating water (52a) cooling compression blade compression counter-rotating injection engine (12E) equipped with bearings (12C) at both ends and enabling temporary assembly by annular outer output blade (8t) screw assembly and fixing Various energy conservation cycle coalescence engines and coalescence methods of large size (11N).   Provided with bearings (12C) at both ends and a counter-rotating water (52a) cooling-compressing-blade compression counter-rotating air injection engine (12F) that can be temporarily assembled by an annular outer output blade (8t) screw assembly and fixing. Various energy conservation cycle coalescence engine and coalescence method as a counter-rotating jet ship (11F).   Counter-rotating water (52a) with a bearing (12C) at both ends and enabling temporary assembly by an annular outer output blade (8t) screw assembly fixing, etc. Counter-rotating engine (12G) water (52a) for cooling compression blade compression ) Various energy storage cycle coalescing engines and coalescence methods that are cooling outer compressor blades (8r) and inner compressor blades (8q).   Counter-rotating water (52a) with a bearing (12C) at both ends and enabling temporary assembly by an annular outer output blade (8t) screw assembly fixing, etc. Counter-rotating engine (12G) water (52a) for cooling compression blade compression ) Various energy storage cycle coalescing engine and coalescence method with cooling outer compression blade (8r) inner compression blade (8q).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be performed by screwing and fixing the annular outer output blade (8t). Engine (12G) Water (52a) Cooling outer compressor blade (8r) Inner compressor blade (8q) as various energy storage cycle coalescing engine and coalescence method.   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be performed by screwing and fixing the annular outer output blade (8t). Engine (12G) Water (52a) Cooling outer compressor blade (8r) Inner compressor blade (8q) Various energy storage cycle coalescing engine and coalescence method.   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be performed by screwing and fixing the annular outer output blade (8t). Various energy storage cycle coalescence engine and coalescence method as an engine (12G) equipped counter-rotating automobile (11B).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be performed by screwing and fixing the annular outer output blade (8t). Various energy storage cycle coalescing engine and coalescence method as an engine (12G) equipped counter-reversing ship (11C).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be performed by screwing and fixing the annular outer output blade (8t). Various energy storage cycle coalescence engine and coalescence method as an engine (12G) equipped contra-rotating airplane (11E).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be performed by screwing and fixing the annular outer output blade (8t). Various energy storage cycle coalescing engine and coalescence method as engine (12G) equipped rotor blade airplane (11I).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be performed by screwing and fixing the annular outer output blade (8t). Various energy storage cycle coalescing engine and coalescence method as an engine (12G) equipped Osprey extra large (11M).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be performed by screwing and fixing the annular outer output blade (8t). Various energy conservation cycle coalescing engines and coalescence methods, including an injection engine (12E) and a counter-rotating jet ship (11F).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be performed by screwing and fixing the annular outer output blade (8t). Various energy storage cycle coalescing engines and coalescence methods, including an injection engine (12E) and a counter-rotating jet airplane (11G).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be performed by screwing and fixing the annular outer output blade (8t). Various energy conservation cycle coalescing engines and coalescence methods, including an injection engine (12E) equipped with a rotor blade jet airplane (11J).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be performed by screwing and fixing the annular outer output blade (8t). Various energy storage cycle coalescing engine and coalescence method with injection engine (12E) and large osprey (11N).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be performed by screwing and fixing the annular outer output blade (8t). Various energy conservation cycle coalescing engines and coalescence methods, which are air injection engines (12F) and counter-rotating jets (11F).   Counter-rotating water (52a) with a bearing (12C) at both ends and enabling temporary assembly by an annular outer output blade (8t) screw assembly fixing, etc. Counter-rotating engine (12G) water (52a) for cooling compression blade compression ) Cooling outer compression blade (8r) Inner compression blade (8q) Various energy storage cycle coalescence engine and coalescence method.   Counter-rotating water (52a) with a bearing (12C) at both ends and enabling temporary assembly by an annular outer output blade (8t) screw assembly fixing, etc. Counter-rotating engine (12G) water (52a) for cooling compression blade compression ) Cooling outer compression blade (8r) Inner compression blade (8q) Various energy storage cycle coalescence engine and coalescence method as cooling compression blade.   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be performed by screwing and fixing the annular outer output blade (8t). Engine (12G) Water (52a) Cooling outer compression blades (8r) Inner compression blades (8q) Cooling blades Various energy storage cycle coalescence engines and coalescence methods.   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly can be performed by screwing and fixing the annular outer output blade (8t). Engine (12G) Water (52a) Cooling outer compression blade (8r) Inner compression blade (8q) Cooling compression blade Various energy storage cycle coalescence engine and coalescence method.   Various types of counter-rotating engine (12G) with counter-rotating water (52a) cooling compression blade compression equipped with bearings (12C) at both ends and capable of temporary assembly by annular inner output vane (8s) screw assembly fixing etc. Energy conservation cycle coalescence engine and coalescence method.   Various types of counter-rotating water (52a) cooling compression blade compression two-stage compressor (12N) equipped with bearings (12C) at both ends and capable of temporary assembly by annular inner output blade (8s) screw assembly fixing etc. Energy conservation cycle coalescence engine and coalescence method.   The counter-rotating water (52a) is a counter-rotating injection engine (12E) for compression of compressed compression blades, which has bearings (12C) at both ends and can be temporarily assembled by an annular inner output blade (8s) screw assembly and fixing. Various energy storage cycle coalescence engines and coalescence methods.   A counter-rotating water (52a) with a bearing (12C) at both ends and an annular inner output vane (8s) screw assembly fixing and the like, and a counter-rotating air injection engine (12F) for cooling compression blade compression; Various energy storage cycle coalescence engines and coalescence methods.   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner output blade (8s) screw Various energy storage cycle coalescence engine and coalescence method as an engine (12G).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner output blade (8s) screw Various energy storage cycle coalescence engines and coalescence methods as an injection engine (12E).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner output blade (8s) screw Various energy storage cycle coalescence engine and coalescence method as an air injection engine (12F).   Double reversing water (52a) with cooling reversing blade compression (12G) equipped with bearings (12C) at both ends and enabling temporary assembly by annular inner output blade (8s) screw assembly fixing, etc. Various energy storage cycle coalescence engine and coalescence method as a reversing automobile (11B).   Double reversing water (52a) with cooling reversing blade compression (12G) equipped with bearings (12C) at both ends and enabling temporary assembly by annular inner output blade (8s) screw assembly fixing, etc. Various energy conservation cycle coalescence engine and coalescence method as an inverted ship (11C).   Double reversing water (52a) with cooling reversing blade compression (12G) equipped with bearings (12C) at both ends and enabling temporary assembly by annular inner output blade (8s) screw assembly fixing, etc. Various energy conservation cycle coalescence engine and coalescence method as a reversal airplane (11E).   A rotating blade with a counter rotating engine (12G) with a counter rotating water (52a) cooling compression blade compression equipped with bearings (12C) at both ends and enabling temporary assembly by an annular inner output blade (8s) screw assembly and fixing. Various energy storage cycle coalescence engine and coalescence method as an airplane (11I).   Bearings (12C) at both ends and an annular inner output blade (8s) screw assembly and fixing, enabling counter assembly processing (52a) Cooling compression blade compression counter rotating engine (12G) Osprey extra large (11M) Various energy storage cycle coalescence engines and coalescence methods.   A counter rotating water (52a) having a bearing (12C) at both ends and enabling temporary assembly by an annular inner output blade (8s) screw assembly fixing, etc. Various energy conservation cycle coalescence engine and coalescence method as a heavy reversal jet ship (11F).   A counter rotating water (52a) having a bearing (12C) at both ends and enabling temporary assembly by an annular inner output blade (8s) screw assembly fixing, etc. Various energy storage cycle coalescence engine and coalescence method as a heavy inversion jet airplane (11G).   A counter rotating water (52a) with a counter rotating injection engine (12E) equipped with a bearing (12C) at both ends and temporarily assembled by an annular inner output blade (8s) screw assembly and fixing, etc. Various energy conservation cycle coalescence engine and coalescence method as a wing jet airplane (11J).   Bearings (12C) at both ends and annular inner output blades (8s) with counter-rotating water (52a) cooled and compressed blade compression counter-rotating injection engine (12E) capable of temporary assembly by screw assembly fixing etc. Osprey Various energy conservation cycle coalescence engines and coalescence methods of large size (11N).   Provided with bearings (12C) at both ends and a counter-rotating water (52a) cooling-compressing-blade-compressing counter-rotating air injection engine (12F) that can be temporarily assembled by an annular inner output blade (8s) screw assembly and fixing. Various energy conservation cycle coalescence engine and coalescence method as a counter-rotating jet ship (11F).   Counter-rotating water (52a) with a bearing (12C) at both ends and enabling temporary assembly by annular inner output blade (8s) screw assembly and fixing, etc. Counter-rotating engine (12G) water for cooling compression blade compression (52a ) Various energy storage cycle coalescing engines and coalescence methods that are cooling outer compressor blades (8r) and inner compressor blades (8q).   Counter-rotating water (52a) with a bearing (12C) at both ends and enabling temporary assembly by annular inner output blade (8s) screw assembly and fixing, etc. Counter-rotating engine (12G) water for cooling compression blade compression (52a ) Various energy storage cycle coalescing engine and coalescence method with cooling outer compression blade (8r) inner compression blade (8q).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner output blade (8s) screw Engine (12G) Water (52a) Cooling outer compressor blade (8r) Inner compressor blade (8q) as various energy storage cycle coalescing engine and coalescence method.   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner output blade (8s) screw Engine (12G) Water (52a) Cooling outer compressor blade (8r) Inner compressor blade (8q) Various energy storage cycle coalescing engine and coalescence method.   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner output blade (8s) screw Various energy storage cycle coalescence engine and coalescence method as an engine (12G) equipped counter-rotating automobile (11B).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner output blade (8s) screw Various energy storage cycle coalescing engine and coalescence method as an engine (12G) equipped counter-reversing ship (11C).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner output blade (8s) screw Various energy storage cycle coalescence engine and coalescence method as an engine (12G) equipped contra-rotating airplane (11E).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner output blade (8s) screw Various energy storage cycle coalescing engine and coalescence method as engine (12G) equipped rotor blade airplane (11I).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner output blade (8s) screw Various energy storage cycle coalescing engine and coalescence method as an engine (12G) equipped Osprey extra large (11M).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner output blade (8s) screw Various energy conservation cycle coalescing engines and coalescence methods, including an injection engine (12E) and a counter-rotating jet ship (11F).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner output blade (8s) screw Various energy storage cycle coalescing engines and coalescence methods, including an injection engine (12E) and a counter-rotating jet airplane (11G).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner output blade (8s) screw Various energy conservation cycle coalescing engines and coalescence methods, including an injection engine (12E) equipped with a rotor blade jet airplane (11J).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner output blade (8s) screw Various energy storage cycle coalescing engine and coalescence method with injection engine (12E) and large osprey (11N).   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner output blade (8s) screw Various energy conservation cycle coalescing engines and coalescence methods, which are air injection engines (12F) and counter-rotating jets (11F).   Counter-rotating water (52a) with a bearing (12C) at both ends and enabling temporary assembly by annular inner output blade (8s) screw assembly and fixing, etc. Counter-rotating engine (12G) water for cooling compression blade compression (52a ) Cooling outer compression blade (8r) Inner compression blade (8q) Various energy storage cycle coalescence engine and coalescence method.   Counter-rotating water (52a) with a bearing (12C) at both ends and enabling temporary assembly by annular inner output blade (8s) screw assembly and fixing, etc. Counter-rotating engine (12G) water for cooling compression blade compression (52a ) Cooling outer compression blade (8r) Inner compression blade (8q) Various energy storage cycle coalescence engine and coalescence method as cooling compression blade.   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner output blade (8s) screw Engine (12G) Water (52a) Cooling outer compression blades (8r) Inner compression blades (8q) Cooling blades Various energy storage cycle coalescence engines and coalescence methods.   Double reversal with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the reversing water-cooled blades in the compression section so that temporary assembly processing is possible by assembling and fixing the annular inner output blade (8s) screw Engine (12G) Water (52a) Cooling outer compression blade (8r) Inner compression blade (8q) Cooling compression blade Various energy storage cycle coalescence engine and coalescence method.   Various energy as a counter-rotating engine (12G) for counter-rotating water (52a) cooling compressor blade compression with bearings (12C) at both ends and enabling temporary assembly by inserting and fixing the annular inner compressor blade (8q) Storage cycle coalescence engine and coalescence method.   Various energy as a double-reversed water (52a) cooling compressor blade compression two-stage compressor (12N) equipped with bearings (12C) at both ends and temporarily assembled by inserting and fixing the annular inner compressor blade (8q) Storage cycle coalescence engine and coalescence method.   Various types of counter-rotating water (52a) cooled counter-rotating jet compression counter-rotating injection engine (12E) equipped with bearings (12C) at both ends and capable of temporary assembly by inserting and fixing an annular inner compressor blade (8q) Energy conservation cycle coalescence engine and coalescence method.   The counter-rotating water (52a) is a counter-rotating air-injection engine (12F) for compressing compressed compressor blades, which has bearings (12C) at both ends and can be temporarily assembled by inserting and fixing the annular inner compressor blade (8q). Various energy storage cycle coalescence engines and coalescence methods.   A counter-rotating engine equipped with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with the compression part enabling temporary assembly by inserting and fixing the annular inner compressor blade (8q). (12G) Various energy storage cycle coalescence engines and coalescence methods.   Counter-rotating injection with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled blade with the compression section capable of temporary assembly by inserting and fixing the annular inner compressor blade (8q). Various energy storage cycle coalescence engine and coalescence method as an engine (12E).   Counter-rotating air having a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled blade with the compression section capable of temporary assembly by inserting and fixing the annular inner compressor blade (8q). Various energy storage cycle coalescing engine and coalescence method as an injection engine (12F).   Double reversing water (52a) with cooling reversing blade compression (12G) equipped with bearings (12C) at both ends and enabling temporary assembly by inserting and fixing the annular inner compression blade (8q) Various energy storage cycle coalescence engine and coalescence method for automobile (11B).   Double reversing water (52a) with cooling reversing blade compression (12G) equipped with bearings (12C) at both ends and enabling temporary assembly by inserting and fixing the annular inner compression blade (8q) Various energy conservation cycle coalescence engines and coalescence methods for a ship (11C).   Double reversing water (52a) with cooling reversing blade compression (12G) equipped with bearings (12C) at both ends and enabling temporary assembly by inserting and fixing the annular inner compression blade (8q) Various energy storage cycle coalescing engines and coalescence methods as an airplane (11E).   Rotating wing airplane equipped with bearings (12C) at both ends and counter-reversing water (52a) cooling-compressing wing compression counter-rotating engine (12G), which can be temporarily assembled by inserting and fixing an annular inner compression wing (8q) (11I) Various energy storage cycle coalescence engines and coalescence methods.   Double reversing water (52a) Cooling compression blade compression counter rotating engine (12G) equipped with bearings (12C) at both ends and temporarily assembled by inserting and fixing the annular inner compression blade (8q) Osprey extra large ( 11M) various energy storage cycle coalescence engines and coalescence methods.   Double reversing water (52a) cooled reversible compression blade compression counter rotating injection engine (12E) equipped with bearings (12C) at both ends and temporarily assembled by inserting and fixing annular inner compression blades (8q) Various energy conservation cycle coalescing engine and coalescence method as a reverse jet ship (11F).   Double reversing water (52a) cooled reversible compression blade compression counter rotating injection engine (12E) equipped with bearings (12C) at both ends and temporarily assembled by inserting and fixing annular inner compression blades (8q) Various energy storage cycle coalescence engine and coalescence method as a reverse jet airplane (11G).   Rotating blades equipped with counter-rotating water (52a) cooling compression blade compression counter-rotating injection engine (12E) equipped with bearings (12C) at both ends and capable of temporary assembly by inserting and fixing the annular inner compression blade (8q) Various energy storage cycle coalescing engines and coalescence methods as an injection plane (11J).   Osprey large size equipped with bearing (12C) at both ends and counter-inverted water (52a) cooling-compressed-blade-compressed counter-rotating injection engine (12E) capable of temporary assembly by inserting and fixing the annular inner compressor blade (8q) (11N) Various energy storage cycle coalescence engines and coalescence methods.   Provided with bearings (12C) at both ends, and provided with a counter-rotating water (52a) cooling-compressing-blade-compressing counter-rotating air injection engine (12F) capable of temporary assembly by inserting and fixing the annular inner compressor blade (8q). Various energy conservation cycle coalescence engine and coalescence method as a heavy reversal jet ship (11F).   A counter-rotating engine equipped with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with the compression part enabling temporary assembly by inserting and fixing the annular inner compressor blade (8q). (12G) Various energy storage cycle coalescence engine and coalescence method for a counter-rotating automobile (11B).   A counter-rotating engine equipped with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with the compression part enabling temporary assembly by inserting and fixing the annular inner compressor blade (8q). (12G) Various energy storage cycle coalescing engines and coalescence methods, which are provided as a counter-rotating ship (11C).   A counter-rotating engine equipped with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with the compression part enabling temporary assembly by inserting and fixing the annular inner compressor blade (8q). (12G) Various energy storage cycle coalescing engines and coalescence methods that are provided as a counter-rotating airplane (11E).   A counter-rotating engine equipped with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with the compression part enabling temporary assembly by inserting and fixing the annular inner compressor blade (8q). (12G) Various energy storage cycle coalescing engines and coalescence methods, which are equipped rotor blade airplanes (11I).   A counter-rotating engine equipped with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with the compression part enabling temporary assembly by inserting and fixing the annular inner compressor blade (8q). (12G) Various energy storage cycle coalescing engines and coalescence methods, which are Osprey Osprey Extra Large (11M).   A counter-rotating injection engine having bearings (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that can be temporarily assembled by inserting and fixing an annular inner compressor blade (8q). (12E) Various energy storage cycle coalescing engines and coalescence methods for a counter-rotating jet ship (11F).   A counter-rotating injection engine having bearings (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that can be temporarily assembled by inserting and fixing an annular inner compressor blade (8q). (12E) Various energy storage cycle coalescing engines and coalescence methods, including a counter-rotating jet airplane (11G).   A counter-rotating injection engine having bearings (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that can be temporarily assembled by inserting and fixing an annular inner compressor blade (8q). (12E) Various energy storage cycle coalescing engines and coalescence methods, which are equipped rotor bladed airplanes (11J).   A counter-rotating injection engine having bearings (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that can be temporarily assembled by inserting and fixing an annular inner compressor blade (8q). (12E) Various energy storage cycle coalescing engines and coalescence methods, each having a large osprey large size (11N).   A counter-rotating air jet having a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression part that can be temporarily assembled by inserting and fixing an annular inner compressor blade (8q). Various energy storage cycle coalescing engine and coalescence method as an engine (12F) equipped counter-rotating jet ship (11F).   Various energy as a counter rotating water (52a) counter rotating engine (12G) for cooling compression blade compression, which has bearings (12C) at both ends and can be temporarily assembled by inserting and fixing an annular outer compression blade (8r). Storage cycle coalescence engine and coalescence method.   Various energy as a double-reversed water (52a) cooling compressor blade compression two-stage compressor (12N) equipped with bearings (12C) at both ends and temporarily assembled by inserting and fixing an annular outer compressor blade (8r) Storage cycle coalescence engine and coalescence method.   Various counter-rotating water (52a) cooling compression blade compression counter-rotating injection engine (12E) equipped with bearings (12C) at both ends and capable of temporary assembly by inserting and fixing an annular outer compression blade (8r). Energy conservation cycle coalescence engine and coalescence method.   The counter-rotating water (52a) is a counter-rotating air-injection engine (12F) for cooling compression blade compression, which has bearings (12C) at both ends and can be temporarily assembled by inserting and fixing an annular outer compression blade (8r). Various energy storage cycle coalescence engines and coalescence methods.   A counter-rotating engine having a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled blade by compressing the compression section to allow temporary assembly processing by inserting and fixing an annular outer compressor blade (8r). (12G) Various energy storage cycle coalescence engines and coalescence methods.   A counter-rotating jet with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that allows temporary assembly by inserting and fixing the annular outer compressor blade (8r). Various energy storage cycle coalescence engine and coalescence method as an engine (12E).   Counter-rotating air having a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled blade with the compression section capable of temporary assembly by inserting and fixing the annular outer compressor blade (8r). Various energy storage cycle coalescing engine and coalescence method as an injection engine (12F).   Provided with bearings (12C) at both ends and an annular outer compression blade (8r) fitted and fixed, etc., enabling counter assembly processing (52a) Cooling compression blade compression counter rotation engine (12G) Various energy storage cycle coalescence engine and coalescence method for automobile (11B).   Provided with bearings (12C) at both ends and an annular outer compression blade (8r) fitted and fixed, etc., enabling counter assembly processing (52a) Cooling compression blade compression counter rotation engine (12G) Various energy conservation cycle coalescence engines and coalescence methods for a ship (11C).   Provided with bearings (12C) at both ends and an annular outer compression blade (8r) fitted and fixed, etc., enabling counter assembly processing (52a) Cooling compression blade compression counter rotation engine (12G) Various energy storage cycle coalescing engines and coalescence methods as an airplane (11E).   Rotating wing airplane equipped with bearing (12C) at both ends and counter-reversing water (52a) cooling compression-blade compression counter-rotating engine (12G) that can be temporarily assembled by inserting and fixing the annular outer compression wing (8r) (11I) Various energy storage cycle coalescence engines and coalescence methods.   Double reversing water (52a) Cooling compression blade compression counter rotating engine (12G) equipped with bearings (12C) at both ends and temporarily assembled by inserting and fixing an annular outer compression blade (8r) Osprey extra large ( 11M) various energy storage cycle coalescence engines and coalescence methods.   Double reversing water (52a) cooled reversible compression blade compression reversing injection engine (12E) equipped with bearings (12C) at both ends and temporarily assembled by inserting and fixing an annular outer compression blade (8r) Various energy conservation cycle coalescing engine and coalescence method as a reverse jet ship (11F).   Double reversing water (52a) cooled reversible compression blade compression reversing injection engine (12E) equipped with bearings (12C) at both ends and temporarily assembled by inserting and fixing an annular outer compression blade (8r) Various energy storage cycle coalescence engine and coalescence method as a reverse jet airplane (11G).   Rotating blades equipped with counter-rotating water (52a) cooling compression blade compression counter-rotating injection engine (12E) equipped with bearings (12C) at both ends and temporarily assembled by inserting and fixing annular outer compression blades (8r) Various energy storage cycle coalescing engines and coalescence methods as an injection plane (11J).   Osprey large size equipped with bearings (12C) at both ends and counter-reversing water (52a) cooling-compressed-blade compression counter-rotating injection engine (12E) that enables temporary assembly by inserting and fixing the annular outer compression blade (8r) (11N) Various energy storage cycle coalescence engines and coalescence methods.   Provided with bearings (12C) at both ends, and provided with a counter-rotating water (52a) cooling-compressing-blade-compressing counter-rotating air injection engine (12F) capable of temporary assembly by inserting and fixing an annular outer compressor blade (8r) Various energy conservation cycle coalescence engine and coalescence method as a heavy reversal jet ship (11F).   A counter-rotating engine having a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled blade by compressing the compression section to allow temporary assembly processing by inserting and fixing an annular outer compressor blade (8r). (12G) Various energy storage cycle coalescence engine and coalescence method for a counter-rotating automobile (11B).   A counter-rotating engine having a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled blade by compressing the compression section to allow temporary assembly processing by inserting and fixing an annular outer compressor blade (8r). (12G) Various energy storage cycle coalescing engines and coalescence methods, which are provided as a counter-rotating ship (11C).   A counter-rotating engine having a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled blade by compressing the compression section to allow temporary assembly processing by inserting and fixing an annular outer compressor blade (8r). (12G) Various energy storage cycle coalescing engines and coalescence methods that are provided as a counter-rotating airplane (11E).   A counter-rotating engine having a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled blade by compressing the compression section to allow temporary assembly processing by inserting and fixing an annular outer compressor blade (8r). (12G) Various energy storage cycle coalescing engines and coalescence methods, which are equipped rotor blade airplanes (11I).   A counter-rotating engine having a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled blade by compressing the compression section to allow temporary assembly processing by inserting and fixing an annular outer compressor blade (8r). (12G) Various energy storage cycle coalescing engines and coalescence methods, which are Osprey Osprey Extra Large (11M).   A counter-rotating jet with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that allows temporary assembly by inserting and fixing the annular outer compressor blade (8r). Various energy storage cycle coalescing engine and coalescence method as an engine (12E) equipped counter-rotating jet ship (11F).   A counter-rotating jet with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that allows temporary assembly by inserting and fixing the annular outer compressor blade (8r). Various energy storage cycle coalescing engine and coalescence method as engine (12E) equipped counter-rotating jet airplane (11G).   A counter-rotating jet with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that allows temporary assembly by inserting and fixing the annular outer compressor blade (8r). Various energy storage cycle coalescing engine and coalescence method as engine (12E) equipped rotor blade jet airplane (11J).   A counter-rotating jet with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that allows temporary assembly by inserting and fixing the annular outer compressor blade (8r). Various energy storage cycle coalescing engine and coalescence method with engine (12E) equipped osprey large (11N).   Counter-rotating air having a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled blade with the compression section capable of temporary assembly by inserting and fixing the annular outer compressor blade (8r). Various energy storage cycle coalescing engines and coalescence methods, including an injection engine (12F) and a counter-rotating jet ship (11F).   Various energy as a counter-rotating engine (12G) of counter-rotating water (52a) cooling compression blade compression equipped with bearings (12C) at both ends and enabling temporary assembly processing by inserting and fixing the annular outer output vane (8t). Storage cycle coalescence engine and coalescence method.   Various energy as a double-reversed water (52a) cooling compressor blade compression two-stage compressor (12N) equipped with bearings (12C) at both ends and temporarily assembled by inserting and fixing an annular outer output blade (8t) Storage cycle coalescence engine and coalescence method.   Various types of counter rotating water (52a) cooling compression blade compression counter rotating injection engine (12E) equipped with bearings (12C) at both ends and capable of temporary assembly by inserting and fixing an annular outer output blade (8t). Energy conservation cycle coalescence engine and coalescence method.   The counter-rotating water (52a) is a counter-rotating air-injection engine (12F) for cooling / compressing blade compression, which has bearings (12C) at both ends and can be temporarily assembled by inserting and fixing an annular outer output blade (8t). Various energy storage cycle coalescence engines and coalescence methods.   A counter-rotating engine provided with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that enables temporary assembly by inserting and fixing an annular outer output blade (8t). (12G) Various energy storage cycle coalescence engines and coalescence methods.   A counter-rotating jet with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the compressor with counter-rotating water-cooled blades to enable temporary assembly by inserting and fixing the annular outer output blade (8t). Various energy storage cycle coalescence engine and coalescence method as an engine (12E).   Counter-rotating air with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled blade with a compression section that enables temporary assembly by inserting and fixing the annular outer output blade (8t). Various energy storage cycle coalescing engine and coalescence method as an injection engine (12F).   Provided with bearings (12C) at both ends and an annular outer output blade (8t) fitted and fixed, etc., with counter-rotating water (52a), cooling-compressed blade compression counter-rotating engine (12G), counter-rotating Various energy storage cycle coalescence engine and coalescence method for automobile (11B).   Provided with bearings (12C) at both ends and an annular outer output blade (8t) fitted and fixed, etc., with counter-rotating water (52a), cooling-compressed blade compression counter-rotating engine (12G), counter-rotating Various energy conservation cycle coalescence engines and coalescence methods for a ship (11C).   Provided with bearings (12C) at both ends and an annular outer output blade (8t) fitted and fixed, etc., with counter-rotating water (52a), cooling-compressed blade compression counter-rotating engine (12G), counter-rotating Various energy storage cycle coalescing engines and coalescence methods as an airplane (11E).   Rotor plane equipped with counter rotating water (52a) cooling compression blade compression counter rotating engine (12G) that can be temporarily assembled by, for example, bearings (12C) squeezed at both ends and annular outer output blades (8t) fitted and fixed. (11I) Various energy storage cycle coalescence engines and coalescence methods.   Double reversing water (52a) Cooling compression blade compression reversing engine (12G) equipped with bearings (12C) at both ends and temporarily assembled by inserting and fixing an annular outer output blade (8t) Osprey extra large ( 11M) various energy storage cycle coalescence engines and coalescence methods.   Double reversing water (52a) cooled reversible compression blade compression reversing injection engine (12E) equipped with bearings (12C) at both ends and temporarily assembled by inserting and fixing an annular outer output blade (8t) Various energy conservation cycle coalescing engine and coalescence method as a reverse jet ship (11F).   Double reversing water (52a) cooled reversible compression blade compression reversing injection engine (12E) equipped with bearings (12C) at both ends and temporarily assembled by inserting and fixing an annular outer output blade (8t) Various energy storage cycle coalescence engine and coalescence method as a reverse jet airplane (11G).   Rotating blades equipped with a counter rotating water engine (12E) with a counter rotating water (52a) cooling compression blade compression, which has bearings (12C) at both ends and can be temporarily assembled by inserting and fixing an annular outer output blade (8t). Various energy storage cycle coalescing engines and coalescence methods as an injection plane (11J).   Osprey large size equipped with bearing (12C) at both ends and counter-reversing water (52a) cooled and compressed blade compression counter-rotating injection engine (12E) that can be temporarily assembled by inserting and fixing annular outer output blade (8t) (11N) Various energy storage cycle coalescence engines and coalescence methods.   Provided with bearings (12C) at both ends, and provided with a counter-rotating water (52a) cooling-compressing-blade-compressing counter-rotating air injection engine (12F) capable of temporary assembly by inserting and fixing an annular outer output blade (8t), etc. Various energy conservation cycle coalescence engine and coalescence method as a heavy reversal jet ship (11F).   Counter-rotating water (52a) cooled counter-rotating blade compression counter-rotating engine (12G) water (52a) equipped with bearings (12C) at both ends and capable of temporary assembly by inserting and fixing the annular outer output blade (8t) Various energy storage cycle coalescing engines and coalescence methods for cooling outer compression blades (8r) and inner compression blades (8q).   Counter-rotating water (52a) cooled counter-rotating blade compression counter-rotating engine (12G) water (52a) equipped with bearings (12C) at both ends and capable of temporary assembly by inserting and fixing the annular outer output blade (8t) Various energy storage cycle coalescing engines and coalescence methods for cooling outer compression blades (8r) and inner compression blades (8q).   A counter-rotating engine provided with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that enables temporary assembly by inserting and fixing an annular outer output blade (8t). (12G) Various energy storage cycle coalescing engines and coalescence methods including water (52a) cooled outer compressor blades (8r) and inner compressor blades (8q).   A counter-rotating engine provided with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that enables temporary assembly by inserting and fixing an annular outer output blade (8t). (12G) Various energy storage cycle coalescing engines and coalescing methods in which water (52a) is cooled as an outer compressor blade (8r) and an inner compressor blade (8q).   A counter-rotating engine provided with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that enables temporary assembly by inserting and fixing an annular outer output blade (8t). (12G) Various energy storage cycle coalescence engine and coalescence method for a counter-rotating automobile (11B).   A counter-rotating engine provided with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that enables temporary assembly by inserting and fixing an annular outer output blade (8t). (12G) Various energy storage cycle coalescing engines and coalescence methods, which are provided as a counter-rotating ship (11C).   A counter-rotating engine provided with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that enables temporary assembly by inserting and fixing an annular outer output blade (8t). (12G) Various energy storage cycle coalescing engines and coalescence methods that are provided as a counter-rotating airplane (11E).   A counter-rotating engine provided with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that enables temporary assembly by inserting and fixing an annular outer output blade (8t). (12G) Various energy storage cycle coalescing engines and coalescence methods, which are equipped rotor blade airplanes (11I).   A counter-rotating engine provided with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that enables temporary assembly by inserting and fixing an annular outer output blade (8t). (12G) Various energy storage cycle coalescing engines and coalescence methods, which are Osprey Osprey Extra Large (11M).   A counter-rotating jet with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the compressor with counter-rotating water-cooled blades to enable temporary assembly by inserting and fixing the annular outer output blade (8t). Various energy storage cycle coalescing engine and coalescence method as an engine (12E) equipped counter-rotating jet ship (11F).   A counter-rotating jet with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the compressor with counter-rotating water-cooled blades to enable temporary assembly by inserting and fixing the annular outer output blade (8t). Various energy storage cycle coalescing engine and coalescence method as engine (12E) equipped counter-rotating jet airplane (11G).   A counter-rotating jet with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the compressor with counter-rotating water-cooled blades to enable temporary assembly by inserting and fixing the annular outer output blade (8t). Various energy storage cycle coalescing engine and coalescence method as engine (12E) equipped rotor blade jet airplane (11J).   A counter-rotating jet with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the compressor with counter-rotating water-cooled blades to enable temporary assembly by inserting and fixing the annular outer output blade (8t). Various energy storage cycle coalescing engine and coalescence method with engine (12E) equipped osprey large (11N).   Counter-rotating air with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled blade with a compression section that enables temporary assembly by inserting and fixing the annular outer output blade (8t). Various energy storage cycle coalescing engines and coalescence methods, including an injection engine (12F) and a counter-rotating jet ship (11F).   Counter-rotating water (52a) cooled counter-rotating blade compression counter-rotating engine (12G) water (52a) equipped with bearings (12C) at both ends and capable of temporary assembly by inserting and fixing the annular outer output blade (8t) Various energy storage cycle coalescing engines and coalescence methods for cooling outer compression blades (8r) inner compression blades (8q) cooling blades.   Counter-rotating water (52a) cooled counter-rotating blade compression counter-rotating engine (12G) water (52a) equipped with bearings (12C) at both ends and capable of temporary assembly by inserting and fixing the annular outer output blade (8t) Various energy storage cycle coalescing engines and coalescence methods for cooling outer compression blades (8r) inner compression blades (8q) cooling compression blades.   A counter-rotating engine provided with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that enables temporary assembly by inserting and fixing an annular outer output blade (8t). (12G) Water (52a) Cooling outer compressor blades (8r) Inner compressor blades (8q) Cooling blades and various energy storage cycle coalescing engines and coalescence methods.   A counter-rotating engine provided with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that enables temporary assembly by inserting and fixing an annular outer output blade (8t). (12G) Water (52a) Cooled outer compressor blade (8r) Inner compressor blade (8q) Cooled compressor blade and various energy storage cycle coalescing engines and coalescence methods.   Various energy as a counter-rotating engine (12G) for counter-rotating water (52a) cooling compression blade compression with bearings (12C) at both ends and enabling temporary assembly by inserting and fixing the annular inner output vane (8s) Storage cycle coalescence engine and coalescence method.   Various energy as a double-reversed water (52a) cooling compression blade compression two-stage compressor (12N) equipped with bearings (12C) at both ends and enabling temporary assembly processing by inserting and fixing the annular inner output blade (8s) Storage cycle coalescence engine and coalescence method.   Various types of counter-rotating injection engine (12E) for counter-rotating water (52a) cooling compression blade compression, which has bearings (12C) at both ends and can be temporarily assembled by inserting and fixing the annular inner output vane (8s). Energy conservation cycle coalescence engine and coalescence method.   The counter-rotating water (52a) is a counter-rotating air-injection engine (12F) for cooling / compressing blade compression, which has bearings (12C) at both ends and can be temporarily assembled by inserting and fixing an annular inner output blade (8s). Various energy storage cycle coalescence engines and coalescence methods.   A counter-rotating engine provided with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that enables temporary assembly by inserting and fixing an annular inner output vane (8s). (12G) Various energy storage cycle coalescence engines and coalescence methods.   Counter-rotating injection with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the compressor with counter-rotating water-cooled blades to enable temporary assembly by inserting and fixing the annular inner output blade (8s). Various energy storage cycle coalescence engine and coalescence method as an engine (12E).   Counter-rotating air with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled blades for compression by enabling the temporary assembly by fitting the annular inner output blade (8s) into place. Various energy storage cycle coalescing engine and coalescence method as an injection engine (12F).   Provided with bearings (12C) at both ends and an annular inner output blade (8s) fitted and fixed, enabling counter assembly processing (52a) Cooling compression blade compression counter rotating engine (12G) and counter rotating Various energy storage cycle coalescence engine and coalescence method for automobile (11B).   Provided with bearings (12C) at both ends and an annular inner output blade (8s) fitted and fixed, enabling counter assembly processing (52a) Cooling compression blade compression counter rotating engine (12G) and counter rotating Various energy conservation cycle coalescence engines and coalescence methods for a ship (11C).   Provided with bearings (12C) at both ends and an annular inner output blade (8s) fitted and fixed, enabling counter assembly processing (52a) Cooling compression blade compression counter rotating engine (12G) and counter rotating Various energy storage cycle coalescing engines and coalescence methods as an airplane (11E).   A rotating wing airplane equipped with bearings (12C) at both ends and a counter rotating water (52a) cooling compression blade compression counter rotating engine (12G) capable of temporary assembly by inserting and fixing an annular inner output blade (8s). (11I) Various energy storage cycle coalescence engines and coalescence methods.   Double reversing water (52a) Cooling compression blade compression reversing engine (12G) equipped with bearings (12C) at both ends and temporarily assembled by inserting and fixing the annular inner output blade (8s) Osprey extra large ( 11M) various energy storage cycle coalescence engines and coalescence methods.   Double reversing water (52a) cooled reversible compression blade compression reversing injection engine (12E) equipped with bearings (12C) at both ends and temporarily assembled by inserting and fixing the annular inner output blade (8s) Various energy conservation cycle coalescing engine and coalescence method as a reverse jet ship (11F).   Double reversing water (52a) cooled reversible compression blade compression reversing injection engine (12E) equipped with bearings (12C) at both ends and temporarily assembled by inserting and fixing the annular inner output blade (8s) Various energy storage cycle coalescence engine and coalescence method as a reverse jet airplane (11G).   A rotating blade with a counter rotating water engine (12E) with a counter rotating water (52a) cooling compression blade compression, which has a bearing (12C) at both ends and can be temporarily assembled by inserting and fixing an annular inner output blade (8s). Various energy storage cycle coalescing engines and coalescence methods as an injection plane (11J).   Osprey large size equipped with bearing (12C) at both ends and counter-inverted water (52a) cooled compression compression blade compression counter-rotating injection engine (12E) that can be temporarily assembled by inserting and fixing the annular inner output blade (8s) (11N) Various energy storage cycle coalescence engines and coalescence methods.   Provided with bearings (12C) at both ends, and provided with a counter-rotating water (52a) cooling-compressing-blade-compressing counter-rotating air injection engine (12F) capable of temporary assembly by inserting and fixing an annular inner output blade (8s), etc. Various energy conservation cycle coalescence engine and coalescence method as a heavy reversal jet ship (11F).   Counter-rotating water (52a) cooling counter-rotating blade compression counter-rotating engine (12G) water (52a) equipped with bearings (12C) at both ends and capable of temporary assembly by inserting and fixing the annular inner output blade (8s) Various energy storage cycle coalescing engines and coalescence methods for cooling outer compression blades (8r) and inner compression blades (8q).   Counter-rotating water (52a) cooling counter-rotating blade compression counter-rotating engine (12G) water (52a) equipped with bearings (12C) at both ends and capable of temporary assembly by inserting and fixing the annular inner output blade (8s) Various energy storage cycle coalescing engines and coalescence methods for cooling outer compression blades (8r) and inner compression blades (8q).   A counter-rotating engine provided with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that enables temporary assembly by inserting and fixing an annular inner output vane (8s). (12G) Various energy storage cycle coalescing engines and coalescence methods including water (52a) cooled outer compressor blades (8r) and inner compressor blades (8q).   A counter-rotating engine provided with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that enables temporary assembly by inserting and fixing an annular inner output vane (8s). (12G) Various energy storage cycle coalescing engines and coalescing methods in which water (52a) is cooled as an outer compressor blade (8r) and an inner compressor blade (8q).   A counter-rotating engine provided with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that enables temporary assembly by inserting and fixing an annular inner output vane (8s). (12G) Various energy storage cycle coalescence engine and coalescence method for a counter-rotating automobile (11B).   A counter-rotating engine provided with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that enables temporary assembly by inserting and fixing an annular inner output vane (8s). (12G) Various energy storage cycle coalescing engines and coalescence methods, which are provided as a counter-rotating ship (11C).   A counter-rotating engine provided with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that enables temporary assembly by inserting and fixing an annular inner output vane (8s). (12G) Various energy storage cycle coalescing engines and coalescence methods that are provided as a counter-rotating airplane (11E).   A counter-rotating engine provided with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that enables temporary assembly by inserting and fixing an annular inner output vane (8s). (12G) Various energy storage cycle coalescing engines and coalescence methods, which are equipped rotor blade airplanes (11I).   A counter-rotating engine provided with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled vane with a compression section that enables temporary assembly by inserting and fixing an annular inner output vane (8s). (12G) Various energy storage cycle coalescing engines and coalescence methods, which are Osprey Osprey Extra Large (11M).   Counter-rotating injection with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the compressor with counter-rotating water-cooled blades to enable temporary assembly by inserting and fixing the annular inner output blade (8s). Various energy storage cycle coalescing engine and coalescence method as an engine (12E) equipped counter-rotating jet ship (11F).   Counter-rotating injection with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the compressor with counter-rotating water-cooled blades to enable temporary assembly by inserting and fixing the annular inner output blade (8s). Various energy storage cycle coalescing engine and coalescence method as engine (12E) equipped counter-rotating jet airplane (11G).   Counter-rotating injection with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the compressor with counter-rotating water-cooled blades to enable temporary assembly by inserting and fixing the annular inner output blade (8s). Various energy storage cycle coalescing engine and coalescence method as engine (12E) equipped rotor blade jet airplane (11J).   Counter-rotating injection with a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the compressor with counter-rotating water-cooled blades to enable temporary assembly by inserting and fixing the annular inner output blade (8s). Various energy storage cycle coalescing engine and coalescence method with engine (12E) equipped osprey large (11N).   Counter-rotating air with bearings (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled blades for compression by enabling the temporary assembly by fitting the annular inner output blade (8s) into place. Various energy storage cycle coalescing engines and coalescence methods, including an injection engine (12F) and a counter-rotating jet ship (11F).   Counter-rotating water (52a) cooling counter-rotating blade compression counter-rotating engine (12G) water (52a) equipped with bearings (12C) at both ends and capable of temporary assembly by inserting and fixing the annular inner output blade (8s) Various energy storage cycle coalescing engines and coalescence methods for cooling outer compression blades (8r) inner compression blades (8q) cooling blades.   Counter-rotating water (52a) cooling counter-rotating blade compression counter-rotating engine (12G) water (52a) equipped with bearings (12C) at both ends and capable of temporary assembly by inserting and fixing the annular inner output blade (8s) Various energy storage cycle coalescing engines and coalescence methods for cooling outer compression blades (8r) inner compression blades (8q) cooling compression blades.   A counter-rotating engine (12N) having a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled blade with a compression section that can be temporarily assembled by fitting and fixing the annular inner output blade (8s). 12G) Water (52a) Cooling outer compression blade (8r) Inner compression blade (8q) Cooling blade, various energy storage cycle coalescence engine and coalescence method.   A counter-rotating engine (12N) having a bearing (12C) at both ends and a two-stage compressor (12N) that compresses the counter-rotating water-cooled blade with a compression section that can be temporarily assembled by fitting and fixing the annular inner output blade (8s). 12G) Water (52a) Cooling outer compression blade (8r) Inner compression blade (8q) Cooling compression blade and various energy storage cycle coalescence engines and coalescence methods.   Various bearings (12C) equipped with bearings (12C) at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool (52a). Energy conservation cycle coalescence engine and coalescence method.   Water (52a) Cooling blade compression two-stage compressor (12N) with bearings (12C) at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine. Storage cycle coalescence engine and coalescence method.   The bearing (12C) is provided at both ends, and the water (52a) cooled and compressed blade-compressed counter-rotating injection engine (12E) is disassembled after confirming that both ends are held by a temporary assembly machine tool and the ultra-high speed rotation balance processing is good. Various energy storage cycle coalescence engines and coalescence methods.   Water (52a) cooled and compressed blade compression counter-rotating air injection engine (12F) equipped with bearings (12C) at both ends and disassembled after confirming the goodness of both ends holding ultra-high speed rotation balance processing with a temporary assembly machine tool; Various energy storage cycle coalescence engines and coalescence methods.   Bearings (12C) are provided at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool, and the compressor is turned into a two-stage compressor (12N) that compresses the counter-rotating water cooling blade in this assembly. Various energy storage cycle coalescence engine and coalescence method as a counter-rotating engine (12G).   Bearings (12C) are provided at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool, and the compressor is turned into a two-stage compressor (12N) that compresses the counter-rotating water cooling blade in this assembly. Various energy storage cycle coalescence engine and coalescence method as a counter-rotating injection engine (12E).   Bearings (12C) are provided at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool, and the compressor is turned into a two-stage compressor (12N) that compresses the counter-rotating water cooling blade in this assembly. Various energy storage cycle coalescence engine and coalescence method as a counter-rotating air injection engine (12F).   Bearings (12C) at both ends, both ends held with a temporary assembly machine tool, and after confirmation of good balance processing of ultra-high speed rotation water (52a) cooled and compressed blade compression counter rotating engine (12G) Various energy storage cycle coalescence engine and coalescence method as a reversing automobile (11B).   Bearings (12C) at both ends, both ends held with a temporary assembly machine tool, and after confirmation of good balance processing of ultra-high speed rotation water (52a) cooled and compressed blade compression counter rotating engine (12G) Various energy conservation cycle coalescence engine and coalescence method as an inverted ship (11C).   Bearings (12C) at both ends, both ends held with a temporary assembly machine tool, and after confirmation of good balance processing of ultra-high speed rotation water (52a) cooled and compressed blade compression counter rotating engine (12G) Various energy conservation cycle coalescence engine and coalescence method as a reversal airplane (11E).   Water (52a) Cooling compression blade compression counter-rotating engine (12G) equipped with bearings (12C) at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool. Various energy storage cycle coalescence engine and coalescence method as an airplane (11I).   Bearing (12C) at both ends and temporary assembly machine tool with both ends held Ultra high speed rotation balance processing disassembled after confirmation of good processing (52a) Cooling compression blade compression counter rotating engine (12G) Osprey extra large (11M) Various energy storage cycle coalescence engines and coalescence methods.   Bearings (12C) are provided at both ends, and water (52a) cooled and compressed blade-compressed counter-rotating injection engine (12E) is provided after disassembling after temporarily confirming that both ends are held by a temporary assembly machine tool. Various energy conservation cycle coalescence engine and coalescence method as a heavy reversal jet ship (11F).   Bearings (12C) are provided at both ends, and water (52a) cooled and compressed blade-compressed counter-rotating injection engine (12E) is provided after disassembling after temporarily confirming that both ends are held by a temporary assembly machine tool. Various energy storage cycle coalescence engine and coalescence method as a heavy inversion jet airplane (11G).   Bearings (12C) on both ends, both ends held with a temporary assembly machine tool, and after confirmation of good balance processing of ultra-high speed rotation water (52a) cooled and compressed blade compression counter rotating injection engine (12E) equipped and rotated Various energy conservation cycle coalescence engine and coalescence method as a wing jet airplane (11J).   Bearings (12C) at both ends, both ends held by a temporary assembly machine tool, and disassembled after confirmation of good balance processing at ultra high speed rotation (52a) Cooling compression blade compression counter-rotating injection engine (12E) Various energy conservation cycle coalescence engines and coalescence methods of large size (11N).   Equipped with bearings (12C) at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool (52a) and a counter-rotating air injection engine (12F) with cooling compression blade compression Various energy conservation cycle coalescence engine and coalescence method as a counter-rotating jet ship (11F).   Water (52a) Cooling compression blade compression counter-rotating engine (12G) Water (52a) equipped with bearings (12C) at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool ) Various energy storage cycle coalescing engines and coalescence methods that are cooling outer compressor blades (8r) and inner compressor blades (8q).   Water (52a) Cooling compression blade compression counter-rotating engine (12G) Water (52a) equipped with bearings (12C) at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool ) Various energy storage cycle coalescing engine and coalescence method with cooling outer compression blade (8r) inner compression blade (8q).   Bearings (12C) are provided at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool, and the compressor is turned into a two-stage compressor (12N) that compresses the counter-rotating water cooling blade in this assembly. Various energy storage cycle coalescing engine and coalescence method as counter rotating engine (12G) water (52a) cooled outer compressor blade (8r) inner compressor blade (8q).   Bearings (12C) are provided at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool, and the compressor is turned into a two-stage compressor (12N) that compresses the counter-rotating water cooling blade in this assembly. Various energy storage cycle coalescing engine and coalescence method comprising a counter rotating engine (12G) water (52a) cooled outer compressor blade (8r) and inner compressor blade (8q).   Bearings (12C) are provided at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool, and the compressor is turned into a two-stage compressor (12N) that compresses the counter-rotating water cooling blade in this assembly. Various energy storage cycle coalescence engines and coalescence methods for a counter rotating engine (12G) and a counter rotating automobile (11B).   Bearings (12C) are provided at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool, and the compressor is turned into a two-stage compressor (12N) that compresses the counter-rotating water cooling blade in this assembly. Various energy storage cycle coalescing engine and coalescence method as a contra-rotating engine (12G) and a contra-rotating ship (11C).   Bearings (12C) are provided at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool, and the compressor is turned into a two-stage compressor (12N) that compresses the counter-rotating water cooling blade in this assembly. Various energy storage cycle coalescing engine and coalescence method as a contra-rotating engine (12G) and a contra-rotating airplane (11E).   Bearings (12C) are provided at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool, and the compressor is turned into a two-stage compressor (12N) that compresses the counter-rotating water cooling blade in this assembly. Various energy storage cycle coalescing engine and coalescence method as a counter rotating engine (12G) equipped rotor blade airplane (11I).   Bearings (12C) are provided at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool, and the compressor is turned into a two-stage compressor (12N) that compresses the counter-rotating water cooling blade in this assembly. Various energy storage cycle coalescence engines and coalescence methods, including a counter rotating engine (12G) and an Osprey extra large (11M).   Bearings (12C) are provided at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool, and the compressor is turned into a two-stage compressor (12N) that compresses the counter-rotating water cooling blade in this assembly. Various energy storage cycle coalescing engines and coalescence methods, including a counter-rotating jet engine (12E) and a counter-rotating jet ship (11F).   Bearings (12C) are provided at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool, and the compressor is turned into a two-stage compressor (12N) that compresses the counter-rotating water cooling blade in this assembly. Various energy storage cycle coalescing engines and coalescence methods, including a contra-rotating jet engine (12E) and a contra-rotating jet airplane (11G).   Bearings (12C) are provided at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool, and the compressor is turned into a two-stage compressor (12N) that compresses the counter-rotating water cooling blade in this assembly. Various energy conservation cycle coalescing engines and coalescence methods, including a counter-rotating jet engine (12E) and a rotary blade jet airplane (11J).   Bearings (12C) are provided at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool, and the compressor is turned into a two-stage compressor (12N) that compresses the counter-rotating water cooling blade in this assembly. Various energy storage cycle coalescing engine and coalescence method with counter rotating injection engine (12E) and Osprey large size (11N).   Bearings (12C) are provided at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool, and the compressor is turned into a two-stage compressor (12N) that compresses the counter-rotating water cooling blade in this assembly. Various energy storage cycle coalescence engines and coalescence methods, including a counter-rotating air injection engine (12F) and a counter-rotating injection ship (11F).   Water (52a) Cooling compression blade compression counter-rotating engine (12G) Water (52a) equipped with bearings (12C) at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool ) Cooling outer compression blade (8r) Inner compression blade (8q) Various energy storage cycle coalescence engine and coalescence method.   Water (52a) Cooling compression blade compression counter-rotating engine (12G) Water (52a) equipped with bearings (12C) at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool ) Cooling outer compression blade (8r) Inner compression blade (8q) Various energy storage cycle coalescence engine and coalescence method as cooling compression blade.   Bearings (12C) are provided at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool, and the compressor is turned into a two-stage compressor (12N) that compresses the counter-rotating water cooling blade in this assembly. Various energy storage cycle coalescing engine and coalescence method as a counter rotating engine (12G) water (52a) cooled outer compression blade (8r) inner compression blade (8q) cooling blade.   Bearings (12C) are provided at both ends and disassembled after confirming that both ends are held at a high-speed rotational balance with a temporary assembly machine tool, and the compressor is turned into a two-stage compressor (12N) that compresses the counter-rotating water cooling blade in this assembly. Various energy storage cycle coalescing engine and coalescence method as counter rotating engine (12G) water (52a) cooled outer compressor blade (8r) inner compressor blade (8q) cooled compressor blade.   Water (52a) cooling compression blades which are provided with bearings (12C) at both ends, disassembled after confirming that both ends are held at the high-speed rotational balance by temporary assembly machine tools, such as an annular inner compression blade (8q) screw assembly fixing, etc. Various energy storage cycle coalescence engine and coalescence method as a compression counter rotating engine (12G).   Water (52a) Cooling blade compression that is disassembled after both bearings (12C) are provided at both ends, the inner assembly blades (8q) are assembled and fixed at the temporary assembly machine tool, etc. Various energy storage cycle coalescing engine and coalescence method as a two-stage compressor (12N).   Water (52a) cooling compression blades which are provided with bearings (12C) at both ends, disassembled after confirming that both ends are held at the high-speed rotational balance by temporary assembly machine tools, such as an annular inner compression blade (8q) screw assembly fixing, etc. Various energy storage cycle coalescing engine and coalescence method as a compression counter-rotating injection engine (12E).   Water (52a) cooling compression blades which are provided with bearings (12C) at both ends, disassembled after confirming that both ends are held at the high-speed rotational balance by temporary assembly machine tools, such as an annular inner compression blade (8q) screw assembly fixing, etc. Various energy storage cycle coalescence engine and coalescence method as a compression counter-rotating air injection engine (12F).   Bearings (12C) are provided at both ends, annular inner compression blade (8q) screw assembly fixed, etc. Temporary assembly machine tool is held at both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble water-reversed water in this assembly Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating engine (12G) made into a two-stage compressor (12N) for blade compression.   Bearings (12C) are provided at both ends, annular inner compression blade (8q) screw assembly fixed, etc. Temporary assembly machine tool is held at both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble water-reversed water in this assembly Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating injection engine (12E) that is a two-stage compressor (12N) that compresses blades.   Bearings (12C) are provided at both ends, annular inner compression blade (8q) screw assembly fixed, etc. Temporary assembly machine tool is held at both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble water-reversed water in this assembly Various energy storage cycle coalescence engine and coalescence method as a counter-rotating air injection engine (12F) which is a two-stage compressor (12N) for blade compression.   Water (52a) cooling compression blades which are provided with bearings (12C) at both ends, disassembled after confirming that both ends are held at the high-speed rotational balance by temporary assembly machine tools, such as an annular inner compression blade (8q) screw assembly fixing, etc. Various energy storage cycle coalescing engine and coalescence method as a counter rotating automobile (11B) equipped with a compression counter rotating engine (12G).   Water (52a) cooling compression blades which are provided with bearings (12C) at both ends, disassembled after confirming that both ends are held at the high-speed rotational balance by temporary assembly machine tools, such as an annular inner compression blade (8q) screw assembly fixing, etc. Various energy storage cycle coalescence engines and coalescence methods, including a compression counter-rotating engine (12G) and a counter-rotating ship (11C).   Water (52a) cooling compression blades which are provided with bearings (12C) at both ends, disassembled after confirming that both ends are held at the high-speed rotational balance by temporary assembly machine tools, such as an annular inner compression blade (8q) screw assembly fixing, etc. Various energy storage cycle coalescing engine and coalescence method as a counter rotating aircraft (11E) equipped with a compression counter rotating engine (12G).   Water (52a) cooling compression blades which are provided with bearings (12C) at both ends, disassembled after confirming that both ends are held at the high-speed rotational balance by temporary assembly machine tools, such as an annular inner compression blade (8q) screw assembly fixing, etc. Various energy storage cycle coalescing engines and coalescing methods, including a compression counter-rotating engine (12G) and a rotary wing airplane (11I).   Water (52a) cooling compression blades which are provided with bearings (12C) at both ends, disassembled after confirming that both ends are held at the high-speed rotational balance by temporary assembly machine tools, such as an annular inner compression blade (8q) screw assembly fixing, etc. Various energy storage cycle coalescence engines and coalescence methods, including a compression counter rotating engine (12G) and an Osprey extra large (11M).   Water (52a) cooling compression blades which are provided with bearings (12C) at both ends, disassembled after confirming that both ends are held at the high-speed rotational balance by temporary assembly machine tools, such as an annular inner compression blade (8q) screw assembly fixing, etc. Various energy storage cycle coalescing engines and coalescence methods, including a counter rotating counter-rotating injection engine (12E) and a counter-rotating injection ship (11F).   Water (52a) cooling compression blades which are provided with bearings (12C) at both ends, disassembled after confirming that both ends are held at the high-speed rotational balance by temporary assembly machine tools, such as an annular inner compression blade (8q) screw assembly fixing, etc. Various energy storage cycle coalescence engines and coalescence methods, including a counter-rotating jet engine (12E) and a counter-rotating jet airplane (11G).   Water (52a) cooling compression blades which are provided with bearings (12C) at both ends, disassembled after confirming that both ends are held at the high-speed rotational balance by temporary assembly machine tools, such as an annular inner compression blade (8q) screw assembly fixing, etc. Various energy storage cycle coalescence engines and coalescence methods, including a compression counter-rotating injection engine (12E) and a rotary blade injection airplane (11J).   Water (52a) cooling compression blades which are provided with bearings (12C) at both ends, disassembled after confirming that both ends are held at the high-speed rotational balance by temporary assembly machine tools, such as an annular inner compression blade (8q) screw assembly fixing, etc. Various energy storage cycle coalescence engines and coalescence methods, including a compression counter-rotating injection engine (12E) and an Osprey large size (11N).   Water (52a) cooling compressor blades which are provided with bearings (12C) at both ends, disassembled after confirming that both ends are held at the high speed rotation balance processing with a temporary assembly machine tool by fixing the annular inner compression blade (8q) screw, etc. Various energy storage cycle coalescence engines and coalescence methods, including a counter-rotating air injection engine (12F) and a counter-rotating injection ship (11F).   Bearings (12C) are provided at both ends, annular inner compression blade (8q) screw assembly fixed, etc. Temporary assembly machine tool is held at both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble water-reversed water in this assembly Various energy storage cycle coalescence engine and coalescence method as a counter-rotating engine (12G) equipped with a counter-rotating engine (12G) having a two-stage compressor (12N) for blade compression.   Bearings (12C) are provided at both ends, annular inner compression blade (8q) screw assembly fixed, etc. Temporary assembly machine tool is held at both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble water-reversed water in this assembly Various energy storage cycle coalescing engine and coalescence method as a contra-rotating ship (11C) equipped with a counter-rotating engine (12G) as a two-stage compressor (12N) for blade compression.   Bearings (12C) are provided at both ends, annular inner compression blade (8q) screw assembly fixed, etc. Temporary assembly machine tool is held at both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble water-reversed water in this assembly Various energy storage cycle coalescence engine and coalescence method as a contra-rotating aircraft (11E) equipped with a counter-rotating engine (12G) that is a two-stage compressor (12N) that compresses blades.   Bearings (12C) are provided at both ends, annular inner compression blade (8q) screw assembly fixed, etc. Temporary assembly machine tool is held at both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble water-reversed water in this assembly Various energy storage cycle coalescence engine and coalescence method as a rotary wing airplane (11I) equipped with a counter-rotating engine (12G) which is a two-stage compressor (12N) for blade compression.   Bearings (12C) are provided at both ends, annular inner compression blade (8q) screw assembly fixed, etc. Temporary assembly machine tool is held at both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble water-reversed water in this assembly Various energy storage cycle coalescing engine and coalescence method with a double reversing engine (12G) equipped with a two-stage compressor (12N) for blade compression and an Osprey extra large (11M).   Bearings (12C) are provided at both ends, annular inner compression blade (8q) screw assembly fixed, etc. Temporary assembly machine tool is held at both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble water-reversed water in this assembly Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating injection ship (11F) equipped with a counter-rotating injection engine (12E) that is a two-stage compressor (12N) that compresses blades.   Bearings (12C) at both ends, annular inner compression blade (8q) screw assembly fixed, etc. Temporary assembly machine tool is supported at both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and compress the compression part so that it can be assembled Various energy storage cycle coalescence engine and coalescence method as a counter-rotating injection airplane (11G) equipped with a counter-rotating injection engine (12E) that is a two-stage compressor (12N) that compresses water-cooled blades.   Bearings (12C) are provided at both ends, annular inner compression blade (8q) screw assembly fixed, etc. Temporary assembly machine tool is held at both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble water-reversed water in this assembly Various energy storage cycle coalescence engine and coalescence method as a rotary blade injection airplane (11J) equipped with a counter-rotating injection engine (12E) which is a two-stage compressor (12N) for blade compression.   Bearings (12C) are provided at both ends, annular inner compression blade (8q) screw assembly fixed, etc. Temporary assembly machine tool is held at both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble water-reversed water in this assembly Various energy storage cycle coalescence engine and coalescence method with a counter rotating injection engine (12E) equipped with a two-stage compressor (12N) for blade compression and an Osprey large size (11N).   Bearings (12C) are provided at both ends, annular inner compression blade (8q) screw assembly fixed, etc. Temporary assembly machine tool is held at both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble water-reversed water in this assembly Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating jet ship (11F) equipped with a counter-rotating air injection engine (12F) that is a two-stage compressor (12N) that compresses blades.   Water (52a) cooled compression blades which are provided with bearings (12C) at both ends and disassembled after confirming that both ends are held at both ends with a temporary assembly machine tool by fixing the annular outer compression blade (8r) with screws, etc. Various energy storage cycle coalescence engine and coalescence method as a compression counter rotating engine (12G).   Water (52a) Cooling blade compression that is disassembled after the bearings (12C) are provided at both ends, the outer outer blades (8r) are assembled and fixed at the temporary assembly machine tool, etc., and the assembly is disassembled after confirming that both ends are super-high-speed rotation balance processing. Various energy storage cycle coalescing engine and coalescence method as a two-stage compressor (12N).   Water (52a) cooled compression blades which are provided with bearings (12C) at both ends and disassembled after confirming that both ends are held at both ends with a temporary assembly machine tool by fixing the annular outer compression blade (8r) with screws, etc. Various energy storage cycle coalescing engine and coalescence method as a compression counter-rotating injection engine (12E).   Water (52a) cooled compression blades which are provided with bearings (12C) at both ends and disassembled after confirming that both ends are held at both ends with a temporary assembly machine tool by fixing the annular outer compression blade (8r) with screws, etc. Various energy storage cycle coalescence engine and coalescence method as a compression counter-rotating air injection engine (12F).   Bearings (12C) at both ends, annular outer compression blades (8r) screw assembly fixed, etc. Temporary assembly machine tool is supported after both ends hold after ultra-high speed rotation balance processing is disassembled and disassembled in this assembly to reverse-invert water cooling Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating engine (12G) made into a two-stage compressor (12N) for blade compression.   Bearings (12C) at both ends, annular outer compression blades (8r) screw assembly fixed, etc. Temporary assembly machine tool is supported after both ends hold after ultra-high speed rotation balance processing is disassembled and disassembled in this assembly to reverse-invert water cooling Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating injection engine (12E) that is a two-stage compressor (12N) that compresses blades.   Bearings (12C) at both ends, annular outer compression blades (8r) screw assembly fixed, etc. Temporary assembly machine tool is supported after both ends hold after ultra-high speed rotation balance processing is disassembled and disassembled in this assembly to reverse-invert water cooling Various energy storage cycle coalescence engine and coalescence method as a counter-rotating air injection engine (12F) which is a two-stage compressor (12N) for blade compression.   Water (52a) cooled compression blades which are provided with bearings (12C) at both ends and disassembled after confirming that both ends are held at both ends with a temporary assembly machine tool by fixing the annular outer compression blade (8r) with screws, etc. Various energy storage cycle coalescing engine and coalescence method as a counter rotating automobile (11B) equipped with a compression counter rotating engine (12G).   Water (52a) cooled compression blades which are provided with bearings (12C) at both ends and disassembled after confirming that both ends are held at both ends with a temporary assembly machine tool by fixing the annular outer compression blade (8r) with screws, etc. Various energy storage cycle coalescence engines and coalescence methods, including a compression counter-rotating engine (12G) and a counter-rotating ship (11C).   Water (52a) cooled compression blades which are provided with bearings (12C) at both ends and disassembled after confirming that both ends are held at both ends with a temporary assembly machine tool by fixing the annular outer compression blade (8r) with screws, etc. Various energy storage cycle coalescing engine and coalescence method as a counter rotating aircraft (11E) equipped with a compression counter rotating engine (12G).   Water (52a) cooled compression blades which are provided with bearings (12C) at both ends and disassembled after confirming that both ends are held at both ends with a temporary assembly machine tool by fixing the annular outer compression blade (8r) with screws, etc. Various energy storage cycle coalescing engines and coalescing methods, including a compression counter-rotating engine (12G) and a rotary wing airplane (11I).   Water (52a) cooled compression blades which are provided with bearings (12C) at both ends and disassembled after confirming that both ends are held at both ends with a temporary assembly machine tool by fixing the annular outer compression blade (8r) with screws, etc. Various energy storage cycle coalescence engines and coalescence methods, including a compression counter rotating engine (12G) and an Osprey extra large (11M).   Water (52a) cooled compression blades which are provided with bearings (12C) at both ends and disassembled after confirming that both ends are held at both ends with a temporary assembly machine tool by fixing the annular outer compression blade (8r) with screws, etc. Various energy storage cycle coalescing engines and coalescence methods, including a counter rotating counter-rotating injection engine (12E) and a counter-rotating injection ship (11F).   Water (52a) cooled compression blades which are provided with bearings (12C) at both ends and disassembled after confirming that both ends are held at both ends with a temporary assembly machine tool by fixing the annular outer compression blade (8r) with screws, etc. Various energy storage cycle coalescence engines and coalescence methods, including a counter-rotating jet engine (12E) and a counter-rotating jet airplane (11G).   Water (52a) cooled compression blades which are provided with bearings (12C) at both ends and disassembled after confirming that both ends are held at both ends with a temporary assembly machine tool by fixing the annular outer compression blade (8r) with screws, etc. Various energy storage cycle coalescence engines and coalescence methods, including a compression counter-rotating injection engine (12E) and a rotary blade injection airplane (11J).   Water (52a) cooled compression blades which are provided with bearings (12C) at both ends and disassembled after confirming that both ends are held at both ends with a temporary assembly machine tool by fixing the annular outer compression blade (8r) with screws, etc. Various energy storage cycle coalescence engines and coalescence methods, including a compression counter-rotating injection engine (12E) and an Osprey large size (11N).   Water (52a) cooled compression blades which are provided with bearings (12C) at both ends and disassembled after confirming that both ends are held at both ends with a temporary assembly machine tool by fixing the annular outer compression blade (8r) with screws, etc. Various energy storage cycle coalescence engines and coalescence methods, including a counter-rotating air injection engine (12F) and a counter-rotating injection ship (11F).   Bearings (12C) at both ends, annular outer compression blades (8r) screw assembly fixed, etc. Temporary assembly machine tool is supported after both ends hold after ultra-high speed rotation balance processing is disassembled and disassembled in this assembly to reverse-invert water cooling Various energy storage cycle coalescence engine and coalescence method as a counter-rotating engine (12G) equipped with a counter-rotating engine (12G) having a two-stage compressor (12N) for blade compression.   Bearings (12C) at both ends, annular outer compression blades (8r) screw assembly fixed, etc. Temporary assembly machine tool is supported after both ends hold after ultra-high speed rotation balance processing is disassembled and disassembled in this assembly to reverse-invert water cooling Various energy storage cycle coalescing engine and coalescence method as a contra-rotating ship (11C) equipped with a counter-rotating engine (12G) as a two-stage compressor (12N) for blade compression.   Bearings (12C) at both ends, annular outer compression blades (8r) screw assembly fixed, etc. Temporary assembly machine tool is supported after both ends hold after ultra-high speed rotation balance processing is disassembled and disassembled in this assembly to reverse-invert water cooling Various energy storage cycle coalescence engine and coalescence method as a contra-rotating aircraft (11E) equipped with a counter-rotating engine (12G) that is a two-stage compressor (12N) that compresses blades.   Bearings (12C) at both ends, annular outer compression blades (8r) screw assembly fixed, etc. Temporary assembly machine tool is supported after both ends hold after ultra-high speed rotation balance processing is disassembled and disassembled in this assembly to reverse-invert water cooling Various energy storage cycle coalescence engine and coalescence method as a rotary wing airplane (11I) equipped with a counter-rotating engine (12G) which is a two-stage compressor (12N) for blade compression.   Bearings (12C) at both ends, annular outer compression blades (8r) screw assembly fixed, etc. Temporary assembly machine tool is supported after both ends hold after ultra-high speed rotation balance processing is disassembled and disassembled in this assembly to reverse-invert water cooling Various energy storage cycle coalescing engine and coalescence method with a double reversing engine (12G) equipped with a two-stage compressor (12N) for blade compression and an Osprey extra large (11M).   Bearings (12C) at both ends, annular outer compression blades (8r) screw assembly fixed, etc. Temporary assembly machine tool is supported after both ends hold after ultra-high speed rotation balance processing is disassembled and disassembled in this assembly to reverse-invert water cooling Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating injection ship (11F) equipped with a counter-rotating injection engine (12E) that is a two-stage compressor (12N) that compresses blades.   Bearings (12C) at both ends, annular outer compression blades (8r) screw assembly fixed, etc. Temporary assembly machine tool is supported after both ends hold after ultra-high speed rotation balance processing is disassembled and disassembled in this assembly to reverse-invert water cooling Various energy storage cycle coalescing engine and coalescence method as a counter-rotating injection airplane (11G) equipped with a counter-rotating injection engine (12E) as a two-stage compressor (12N) for blade compression.   Bearings (12C) at both ends, annular outer compression blades (8r) screw assembly fixed, etc. Temporary assembly machine tool is supported after both ends hold after ultra-high speed rotation balance processing is disassembled and disassembled in this assembly to reverse-invert water cooling Various energy storage cycle coalescence engine and coalescence method as a rotary blade injection airplane (11J) equipped with a counter-rotating injection engine (12E) which is a two-stage compressor (12N) for blade compression.   Bearings (12C) at both ends, annular outer compression blades (8r) screw assembly fixed, etc. Temporary assembly machine tool is supported after both ends hold after ultra-high speed rotation balance processing is disassembled and disassembled in this assembly to reverse-invert water cooling Various energy storage cycle coalescence engine and coalescence method with a counter rotating injection engine (12E) equipped with a two-stage compressor (12N) for blade compression and an Osprey large size (11N).   Bearings (12C) at both ends, annular outer compression blades (8r) screw assembly fixed, etc. Temporary assembly machine tool is supported after both ends hold after ultra-high speed rotation balance processing is disassembled and disassembled in this assembly to reverse-invert water cooling Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating jet ship (11F) equipped with a counter-rotating air injection engine (12F) that is a two-stage compressor (12N) that compresses blades.   Water (52a) Cooling compression blades which are disassembled after having confirmed bearings (12C) at both ends, an annular outer output blade (8t) screw assembly fixing, etc., and holding both ends with a temporary assembly machine tool, and confirming good balance machining at both ends. Various energy storage cycle coalescence engine and coalescence method as a compression counter rotating engine (12G).   Water (52a) Cooling blade compression that was disassembled after the bearings (12C) were provided at both ends, the outer assembly of the annular outer output blade (8t) was screwed and fixed, etc. Various energy storage cycle coalescing engine and coalescence method as a two-stage compressor (12N).   Water (52a) Cooling compression blades which are disassembled after having confirmed bearings (12C) at both ends, an annular outer output blade (8t) screw assembly fixing, etc., and holding both ends with a temporary assembly machine tool, and confirming good balance machining at both ends. Various energy storage cycle coalescing engine and coalescence method as a compression counter-rotating injection engine (12E).   Water (52a) Cooling compression blades which are disassembled after having confirmed bearings (12C) at both ends, an annular outer output blade (8t) screw assembly fixing, etc., and holding both ends with a temporary assembly machine tool, and confirming good balance machining at both ends. Various energy storage cycle coalescence engine and coalescence method as a compression counter-rotating air injection engine (12F).   Bearings (12C) at both ends, annular outer output blade (8t), screw assembly fixed, etc. Temporary assembly machine tool, both ends held, ultra-high-speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating engine (12G) made into a two-stage compressor (12N) for blade compression.   Bearings (12C) at both ends, annular outer output blade (8t), screw assembly fixed, etc. Temporary assembly machine tool, both ends held, ultra-high-speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating injection engine (12E) that is a two-stage compressor (12N) that compresses blades.   Bearings (12C) at both ends, annular outer output blade (8t), screw assembly fixed, etc. Temporary assembly machine tool, both ends held, ultra-high-speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engine and coalescence method as a counter-rotating air injection engine (12F) which is a two-stage compressor (12N) for blade compression.   Water (52a) Cooling compression blades which are disassembled after having confirmed bearings (12C) at both ends, an annular outer output blade (8t) screw assembly fixing, etc., and holding both ends with a temporary assembly machine tool, and confirming good balance machining at both ends. Various energy storage cycle coalescing engine and coalescence method as a counter rotating automobile (11B) equipped with a compression counter rotating engine (12G).   Water (52a) Cooling compression blades which are disassembled after having confirmed bearings (12C) at both ends, an annular outer output blade (8t) screw assembly fixing, etc., and holding both ends with a temporary assembly machine tool, and confirming good balance machining at both ends. Various energy storage cycle coalescence engines and coalescence methods, including a compression counter-rotating engine (12G) and a counter-rotating ship (11C).   Water (52a) Cooling compression blades which are disassembled after having confirmed bearings (12C) at both ends, an annular outer output blade (8t) screw assembly fixing, etc., and holding both ends with a temporary assembly machine tool, and confirming good balance machining at both ends. Various energy storage cycle coalescing engine and coalescence method as a counter rotating aircraft (11E) equipped with a compression counter rotating engine (12G).   Water (52a) Cooling compression blades disassembled into a main assembly after confirming that both ends have a bearing (12C) squeeze and an annular outer output blade (8t) screw assembly assembly and the like are temporarily assembled, and both ends are held and ultra-high speed rotation balance processing is confirmed. Various energy storage cycle coalescing engines and coalescing methods, including a compression counter-rotating engine (12G) and a rotary wing airplane (11I).   Water (52a) Cooling compression blades which are disassembled after having confirmed bearings (12C) at both ends, an annular outer output blade (8t) screw assembly fixing, etc., and holding both ends with a temporary assembly machine tool, and confirming good balance machining at both ends. Various energy storage cycle coalescence engines and coalescence methods, including a compression counter rotating engine (12G) and an Osprey extra large (11M).   Water (52a) Cooling compression blades which are disassembled after having confirmed bearings (12C) at both ends, an annular outer output blade (8t) screw assembly fixing, etc., and holding both ends with a temporary assembly machine tool, and confirming good balance machining at both ends. Various energy storage cycle coalescing engines and coalescence methods, including a counter rotating counter-rotating injection engine (12E) and a counter-rotating injection ship (11F).   Water (52a) Cooling compression blades which are disassembled after having confirmed bearings (12C) at both ends, an annular outer output blade (8t) screw assembly fixing, etc., and holding both ends with a temporary assembly machine tool, and confirming good balance machining at both ends. Various energy storage cycle coalescence engines and coalescence methods, including a counter-rotating jet engine (12E) and a counter-rotating jet airplane (11G).   Water (52a) Cooling compression blades which are disassembled after having confirmed bearings (12C) at both ends, an annular outer output blade (8t) screw assembly fixing, etc., and holding both ends with a temporary assembly machine tool, and confirming good balance machining at both ends. Various energy storage cycle coalescence engines and coalescence methods, including a compression counter-rotating injection engine (12E) and a rotary blade injection airplane (11J).   Water (52a) Cooling compression blades which are disassembled after having confirmed bearings (12C) at both ends, an annular outer output blade (8t) screw assembly fixing, etc., and holding both ends with a temporary assembly machine tool, and confirming good balance machining at both ends. Various energy storage cycle coalescence engines and coalescence methods, including a compression counter-rotating injection engine (12E) and an Osprey large size (11N).   Water (52a) Cooling compression blades which are disassembled after having confirmed bearings (12C) at both ends, an annular outer output blade (8t) screw assembly fixing, etc., and holding both ends with a temporary assembly machine tool, and confirming good balance machining at both ends. Various energy storage cycle coalescence engines and coalescence methods, including a counter-rotating air injection engine (12F) and a counter-rotating injection ship (11F).   Water (52a) Cooling compression blades which are disassembled after having confirmed bearings (12C) at both ends, an annular outer output blade (8t) screw assembly fixing, etc., and holding both ends with a temporary assembly machine tool, and confirming good balance machining at both ends. Various energy storage cycle coalescence engines and coalescence methods, including a compression counter-rotating engine (12G), water (52a), a cooling outer compression blade (8r), and an inner compression blade (8q).   Water (52a) Cooling compression blades which are disassembled after having confirmed bearings (12C) at both ends, an annular outer output blade (8t) screw assembly fixing, etc., and holding both ends with a temporary assembly machine tool, and confirming good balance machining at both ends. Compressed counter rotating engine (12G) Water (52a) Cooling outer compression blade (8r) Inner compression blade (8q)   Bearings (12C) at both ends, annular outer output blade (8t), screw assembly fixed, etc. Temporary assembly machine tool, both ends held, ultra-high-speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescing engine and coalescence method using a double reversing engine (12G) water (52a) cooled outer compressor blade (8r) and inner compressor blade (8q) in a two-stage compressor (12N) for blade compression.   Bearings (12C) at both ends, annular outer output blade (8t), screw assembly fixed, etc. Temporary assembly machine tool, both ends held, ultra-high-speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated by water cooling in this assembly Combined engine and method for combining various energy conservation cycles with a counter rotating engine (12G) water (52a) cooled outer compression blade (8r) and inner compression blade (8q) made into a two-stage compressor (12N) for blade compression.   Bearings (12C) at both ends, annular outer output blade (8t), screw assembly fixed, etc. Temporary assembly machine tool, both ends held, ultra-high-speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engine and coalescence method as a counter-rotating engine (12G) equipped with a counter-rotating engine (12G) having a two-stage compressor (12N) for blade compression.   Bearings (12C) at both ends, annular outer output blade (8t), screw assembly fixed, etc. Temporary assembly machine tool, both ends held, ultra-high-speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescing engine and coalescence method as a contra-rotating ship (11C) equipped with a counter-rotating engine (12G) as a two-stage compressor (12N) for blade compression.   Bearings (12C) at both ends, annular outer output blade (8t), screw assembly fixed, etc. Temporary assembly machine tool, both ends held, ultra-high-speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engine and coalescence method as a contra-rotating aircraft (11E) equipped with a counter-rotating engine (12G) that is a two-stage compressor (12N) that compresses blades.   Bearings (12C) at both ends, annular outer output blade (8t), screw assembly fixed, etc. Temporary assembly machine tool, both ends held, ultra-high-speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engine and coalescence method as a rotary wing airplane (11I) equipped with a counter-rotating engine (12G) which is a two-stage compressor (12N) for blade compression.   Bearings (12C) at both ends, annular outer output blade (8t), screw assembly fixed, etc. Temporary assembly machine tool, both ends held, ultra-high-speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescing engine and coalescence method with a double reversing engine (12G) equipped with a two-stage compressor (12N) for blade compression and an Osprey extra large (11M).   Bearings (12C) at both ends, annular outer output blade (8t), screw assembly fixed, etc. Temporary assembly machine tool, both ends held, ultra-high-speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating injection ship (11F) equipped with a counter-rotating injection engine (12E) that is a two-stage compressor (12N) that compresses blades.   Bearings (12C) at both ends, annular outer output blade (8t), screw assembly fixed, etc. Temporary assembly machine tool, both ends held, ultra-high-speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescing engine and coalescence method as a counter-rotating injection airplane (11G) equipped with a counter-rotating injection engine (12E) as a two-stage compressor (12N) for blade compression.   Bearings (12C) at both ends, annular outer output blade (8t), screw assembly fixed, etc. Temporary assembly machine tool, both ends held, ultra-high-speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engine and coalescence method as a rotary blade injection airplane (11J) equipped with a counter-rotating injection engine (12E) which is a two-stage compressor (12N) for blade compression.   Bearings (12C) at both ends, annular outer output blade (8t), screw assembly fixed, etc. Temporary assembly machine tool, both ends held, ultra-high-speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engine and coalescence method with a counter rotating injection engine (12E) equipped with a two-stage compressor (12N) for blade compression and an Osprey large size (11N).   Bearings (12C) at both ends, annular outer output blade (8t), screw assembly fixed, etc. Temporary assembly machine tool, both ends held, ultra-high-speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating jet ship (11F) equipped with a counter-rotating air injection engine (12F) that is a two-stage compressor (12N) that compresses blades.   Water (52a) Cooling compression blades which are disassembled after having confirmed bearings (12C) at both ends, an annular outer output blade (8t) screw assembly fixing, etc., and holding both ends with a temporary assembly machine tool, and confirming good balance machining at both ends. Various energy storage cycle coalescing engines and coalescence methods comprising a compression counter rotating engine (12G) water (52a) cooled outer compressor blade (8r) inner compressor blade (8q) cooling blade.   Water (52a) Cooling compression blades which are disassembled after having confirmed bearings (12C) at both ends, an annular outer output blade (8t) screw assembly fixing, etc., and holding both ends with a temporary assembly machine tool, and confirming good balance machining at both ends. Various energy storage cycle coalescence engines and coalescence methods, including compression counter-rotating engine (12G) water (52a) cooled outer compressor blade (8r) inner compressor blade (8q) cooled compressor blade.   Bearings (12C) at both ends, annular outer output blade (8t), screw assembly fixed, etc. Temporary assembly machine tool, both ends held, ultra-high-speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated by water cooling in this assembly Combined engine and method for combining various energy conservation cycles as a double reversing engine (12G) water (52a) cooled outer compression blade (8r) inner compression blade (8q) cooling blade in a two-stage compressor (12N) for blade compression .   Bearings (12C) at both ends, annular outer output blade (8t), screw assembly fixed, etc. Temporary assembly machine tool, both ends held, ultra-high-speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated by water cooling in this assembly Combined engine and combination of various energy storage cycles as a double reversing engine (12G) water (52a) cooled outer compressor blade (8r) inner compressor blade (8q) cooled compressor blade with a two-stage compressor (12N) for blade compression Method.   Water (52a) cooling compression blades which are equipped with bearings (12C) at both ends, disassembled after confirming that both ends are held at the both ends with a temporary assembly machine tool by means of a temporary assembly machine tool by fixing the annular inner output blade (8s), etc. Various energy storage cycle coalescence engine and coalescence method as a compression counter rotating engine (12G).   Bearing (12C) at both ends, annular inner output blade (8s) screw assembly fixed, etc. Temporary assembly machine tool supported by both ends Ultra-high speed rotation Balance processing was confirmed after being disassembled and finally assembled water (52a) Cooling blade compression Various energy storage cycle coalescing engine and coalescence method as a two-stage compressor (12N).   Water (52a) cooling compression blades which are equipped with bearings (12C) at both ends, disassembled after confirming that both ends are held at the both ends with a temporary assembly machine tool by means of a temporary assembly machine tool by fixing the annular inner output blade (8s), etc. Various energy storage cycle coalescing engine and coalescence method as a compression counter-rotating injection engine (12E).   Water (52a) cooling compression blades which are equipped with bearings (12C) at both ends, disassembled after confirming that both ends are held at the both ends with a temporary assembly machine tool by means of a temporary assembly machine tool by fixing the annular inner output blade (8s), etc. Various energy storage cycle coalescence engine and coalescence method as a compression counter-rotating air injection engine (12F).   Bearings (12C) at both ends, annular inner output wing (8s) screw assembly fixed by temporary assembly machine tool, disassembled after confirming good balance processing at both ends with ultra-high speed rotation balance, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating engine (12G) made into a two-stage compressor (12N) for blade compression.   Bearings (12C) at both ends, annular inner output wing (8s) screw assembly fixed by temporary assembly machine tool, disassembled after confirming good balance processing at both ends with ultra-high speed rotation balance, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating injection engine (12E) that is a two-stage compressor (12N) that compresses blades.   Bearings (12C) at both ends, annular inner output wing (8s) screw assembly fixed by temporary assembly machine tool, disassembled after confirming good balance processing at both ends with ultra-high speed rotation balance, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engine and coalescence method as a counter-rotating air injection engine (12F) which is a two-stage compressor (12N) for blade compression.   Water (52a) cooling compression blades which are equipped with bearings (12C) at both ends, disassembled after confirming that both ends are held at the both ends with a temporary assembly machine tool by means of a temporary assembly machine tool by fixing the annular inner output blade (8s), etc. Various energy storage cycle coalescing engine and coalescence method as a counter rotating automobile (11B) equipped with a compression counter rotating engine (12G).   Water (52a) cooling compression blades which are equipped with bearings (12C) at both ends, disassembled after confirming that both ends are held at the both ends with a temporary assembly machine tool by means of a temporary assembly machine tool by fixing the annular inner output blade (8s), etc. Various energy storage cycle coalescence engines and coalescence methods, including a compression counter-rotating engine (12G) and a counter-rotating ship (11C).   Water (52a) cooling compression blades which are equipped with bearings (12C) at both ends, disassembled after confirming that both ends are held at the both ends with a temporary assembly machine tool by means of a temporary assembly machine tool by fixing the annular inner output blade (8s), etc. Various energy storage cycle coalescing engine and coalescence method as a counter rotating aircraft (11E) equipped with a compression counter rotating engine (12G).   Water (52a) cooling compression blades which are equipped with bearings (12C) at both ends, disassembled after confirming that both ends are held at the both ends with a temporary assembly machine tool by means of a temporary assembly machine tool by fixing the annular inner output blade (8s), etc. Various energy storage cycle coalescing engines and coalescing methods, including a compression counter-rotating engine (12G) and a rotary wing airplane (11I).   Water (52a) cooling compression blades which are equipped with bearings (12C) at both ends, disassembled after confirming that both ends are held at the both ends with a temporary assembly machine tool by means of a temporary assembly machine tool by fixing the annular inner output blade (8s), etc. Various energy storage cycle coalescence engines and coalescence methods, including a compression counter rotating engine (12G) and an Osprey extra large (11M).   Water (52a) cooling compression blades which are equipped with bearings (12C) at both ends, disassembled after confirming that both ends are held at the both ends with a temporary assembly machine tool by means of a temporary assembly machine tool by fixing the annular inner output blade (8s), etc. Various energy storage cycle coalescing engines and coalescence methods, including a counter rotating counter-rotating injection engine (12E) and a counter-rotating injection ship (11F).   Water (52a) cooling compression blades which are equipped with bearings (12C) at both ends, disassembled after confirming that both ends are held at the both ends with a temporary assembly machine tool by means of a temporary assembly machine tool by fixing the annular inner output blade (8s), etc. Various energy storage cycle coalescence engines and coalescence methods, including a counter-rotating jet engine (12E) and a counter-rotating jet airplane (11G).   Water (52a) cooling compression blades which are equipped with bearings (12C) at both ends, disassembled after confirming that both ends are held at the both ends with a temporary assembly machine tool by means of a temporary assembly machine tool by fixing the annular inner output blade (8s), etc. Various energy storage cycle coalescence engines and coalescence methods, including a compression counter-rotating injection engine (12E) and a rotary blade injection airplane (11J).   Water (52a) cooling compression blades which are equipped with bearings (12C) at both ends, disassembled after confirming that both ends are held at the both ends with a temporary assembly machine tool by means of a temporary assembly machine tool by fixing the annular inner output blade (8s), etc. Various energy storage cycle coalescence engines and coalescence methods, including a compression counter-rotating injection engine (12E) and an Osprey large size (11N).   Water (52a) cooling compression blades which are equipped with bearings (12C) at both ends, disassembled after confirming that both ends are held at the both ends with a temporary assembly machine tool by means of a temporary assembly machine tool by fixing the annular inner output blade (8s), etc. Various energy storage cycle coalescence engines and coalescence methods, including a counter-rotating air injection engine (12F) and a counter-rotating injection ship (11F).   Water (52a) cooling compression blades which are equipped with bearings (12C) at both ends, disassembled after confirming that both ends are held at the both ends with a temporary assembly machine tool by means of a temporary assembly machine tool by fixing the annular inner output blade (8s), etc. Various energy storage cycle coalescence engines and coalescence methods, including a compression counter-rotating engine (12G), water (52a), a cooling outer compression blade (8r), and an inner compression blade (8q).   Water (52a) cooling compression blades which are equipped with bearings (12C) at both ends, disassembled after confirming that both ends are held at the both ends with a temporary assembly machine tool by means of a temporary assembly machine tool by fixing the annular inner output blade (8s), etc. Compressed counter rotating engine (12G) Water (52a) Cooling outer compression blade (8r) Inner compression blade (8q)   Bearings (12C) at both ends, annular inner output wing (8s) screw assembly fixed by temporary assembly machine tool, disassembled after confirming good balance processing at both ends with ultra-high speed rotation balance, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescing engine and coalescence method using a double reversing engine (12G) water (52a) cooled outer compressor blade (8r) and inner compressor blade (8q) in a two-stage compressor (12N) for blade compression.   Bearings (12C) at both ends, annular inner output wing (8s) screw assembly fixed by temporary assembly machine tool, disassembled after confirming good balance processing at both ends with ultra-high speed rotation balance, and the compressed part is counter-rotated by water cooling in this assembly Combined engine and method for combining various energy conservation cycles with a counter rotating engine (12G) water (52a) cooled outer compression blade (8r) and inner compression blade (8q) made into a two-stage compressor (12N) for blade compression.   Bearings (12C) at both ends, annular inner output wing (8s) screw assembly fixed by temporary assembly machine tool, disassembled after confirming good balance processing at both ends with ultra-high speed rotation balance, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engine and coalescence method as a counter-rotating engine (12G) equipped with a counter-rotating engine (12G) having a two-stage compressor (12N) for blade compression.   Bearings (12C) at both ends, annular inner output wing (8s) screw assembly fixed by temporary assembly machine tool, disassembled after confirming good balance processing at both ends with ultra-high speed rotation balance, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescing engine and coalescence method as a contra-rotating ship (11C) equipped with a counter-rotating engine (12G) as a two-stage compressor (12N) for blade compression.   Bearings (12C) at both ends, annular inner output wing (8s) screw assembly fixed by temporary assembly machine tool, disassembled after confirming good balance processing at both ends with ultra-high speed rotation balance, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engine and coalescence method as a contra-rotating aircraft (11E) equipped with a counter-rotating engine (12G) that is a two-stage compressor (12N) that compresses blades.   Bearings (12C) at both ends, annular inner output wing (8s) screw assembly fixed by temporary assembly machine tool, disassembled after confirming good balance processing at both ends with ultra-high speed rotation balance, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engine and coalescence method as a rotary wing airplane (11I) equipped with a counter-rotating engine (12G) which is a two-stage compressor (12N) for blade compression.   Bearings (12C) at both ends, annular inner output wing (8s) screw assembly fixed by temporary assembly machine tool, disassembled after confirming good balance processing at both ends with ultra-high speed rotation balance, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescing engine and coalescence method with a double reversing engine (12G) equipped with a two-stage compressor (12N) for blade compression and an Osprey extra large (11M).   Bearings (12C) at both ends, annular inner output wing (8s) screw assembly fixed by temporary assembly machine tool, disassembled after confirming good balance processing at both ends with ultra-high speed rotation balance, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating injection ship (11F) equipped with a counter-rotating injection engine (12E) that is a two-stage compressor (12N) that compresses blades.   Bearings (12C) at both ends, annular inner output wing (8s) screw assembly fixed by temporary assembly machine tool, disassembled after confirming good balance processing at both ends with ultra-high speed rotation balance, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescing engine and coalescence method as a counter-rotating injection airplane (11G) equipped with a counter-rotating injection engine (12E) as a two-stage compressor (12N) for blade compression.   Bearings (12C) at both ends, annular inner output wing (8s) screw assembly fixed by temporary assembly machine tool, disassembled after confirming good balance processing at both ends with ultra-high speed rotation balance, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engine and coalescence method as a rotary blade injection airplane (11J) equipped with a counter-rotating injection engine (12E) which is a two-stage compressor (12N) for blade compression.   Bearings (12C) at both ends, annular inner output wing (8s) screw assembly fixed by temporary assembly machine tool, disassembled after confirming good balance processing at both ends with ultra-high speed rotation balance, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engine and coalescence method with a counter rotating injection engine (12E) equipped with a two-stage compressor (12N) for blade compression and an Osprey large size (11N).   Bearings (12C) at both ends, annular inner output wing (8s) screw assembly fixed by temporary assembly machine tool, disassembled after confirming good balance processing at both ends with ultra-high speed rotation balance, and the compressed part is counter-rotated by water cooling in this assembly Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating jet ship (11F) equipped with a counter-rotating air injection engine (12F) that is a two-stage compressor (12N) that compresses blades.   Water (52a) cooling compression blades which are equipped with bearings (12C) at both ends, disassembled after confirming that both ends are held at the both ends with a temporary assembly machine tool by means of a temporary assembly machine tool by fixing the annular inner output blade (8s), etc. Various energy storage cycle coalescing engines and coalescence methods comprising a compression counter rotating engine (12G) water (52a) cooled outer compressor blade (8r) inner compressor blade (8q) cooling blade.   Water (52a) cooling compression blades which are equipped with bearings (12C) at both ends, disassembled after confirming that both ends are held at the both ends with a temporary assembly machine tool by means of a temporary assembly machine tool by fixing the annular inner output blade (8s), etc. Various energy storage cycle coalescence engines and coalescence methods, including compression counter-rotating engine (12G) water (52a) cooled outer compressor blade (8r) inner compressor blade (8q) cooled compressor blade.   Bearings (12C) at both ends, annular inner output wing (8s) screw assembly fixed by temporary assembly machine tool, disassembled after confirming good balance processing at both ends with ultra-high speed rotation balance, and the compressed part is counter-rotated by water cooling in this assembly Combined engine and method for combining various energy conservation cycles as a double reversing engine (12G) water (52a) cooled outer compression blade (8r) inner compression blade (8q) cooling blade in a two-stage compressor (12N) for blade compression .   Bearings (12C) at both ends, annular inner output wing (8s) screw assembly fixed by temporary assembly machine tool, disassembled after confirming good balance processing at both ends with ultra-high speed rotation balance, and the compressed part is counter-rotated by water cooling in this assembly Combined engine and combination of various energy storage cycles as a double reversing engine (12G) water (52a) cooled outer compressor blade (8r) inner compressor blade (8q) cooled compressor blade with a two-stage compressor (12N) for blade compression Method.   Water (52a) cooling compression blade compression which was disassembled after the bearing (12C) was provided at both ends, and the inner inner compression blade (8q) was fitted and fixed, etc., was confirmed by temporary assembly machine tools and both ends were held and ultra-high speed rotation balance processing was confirmed. Various energy storage cycle coalescing engines and coalescence methods of a non-reversing engine (12G).   Bearings (12C) at both ends, annular inner compression blades (8q) fitted and fixed, etc. Temporary assembly machine tool is used for both-end holding ultra-high speed rotation balance processing and after disassembling the water (52a) cooling blade compression Various energy storage cycle coalescence engine and coalescence method as a two-stage compressor (12N).   Water (52a) cooling compression blade compression which was disassembled after the bearing (12C) was provided at both ends, and the inner inner compression blade (8q) was fitted and fixed, etc., was confirmed by temporary assembly machine tools and both ends were held and ultra-high speed rotation balance processing was confirmed. Various energy storage cycle coalescing engines and coalescence methods of the counter-rotating injection engine (12E).   Water (52a) cooling compression blade compression which was disassembled after the bearing (12C) was provided at both ends, and the inner inner compression blade (8q) was fitted and fixed, etc., was confirmed by temporary assembly machine tools and both ends were held and ultra-high speed rotation balance processing was confirmed. Various energy storage cycle coalescence engines and coalescence methods of the counter-rotating air injection engine (12F).   Bearings (12C) at both ends and annular inner compression blades (8q) fitted and fixed, etc. are temporarily assembled by a machine tool and disassembled after confirming that both ends are held at ultra-high speed rotation balance processing. Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating engine (12G), which is a two-stage compressor (12N) for compression.   Bearings (12C) at both ends and annular inner compression blades (8q) fitted and fixed, etc. are temporarily assembled by a machine tool and disassembled after confirming that both ends are held at ultra-high speed rotation balance processing. Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating injection engine (12E) which is a two-stage compressor (12N) for compression.   Bearings (12C) at both ends and annular inner compression blades (8q) fitted and fixed, etc. are temporarily assembled by a machine tool and disassembled after confirming that both ends are held at ultra-high speed rotation balance processing. Various energy storage cycle coalescence engine and coalescence method as a counter-rotating air injection engine (12F) which is a two-stage compressor (12N) for compression.   Water (52a) cooling compression blade compression which was disassembled after the bearing (12C) was provided at both ends, and the inner inner compression blade (8q) was fitted and fixed, etc., was confirmed by temporary assembly machine tools and both ends were held and ultra-high speed rotation balance processing was confirmed. Non-reversing engine (12G) and non-reversing motor vehicle (11B).   Water (52a) cooling compression blade compression which was disassembled after the bearing (12C) was provided at both ends, and the inner inner compression blade (8q) was fitted and fixed, etc., was confirmed by temporary assembly machine tools and both ends were held and ultra-high speed rotation balance processing was confirmed. Non-reversing engine (12G) equipped with non-reversing ship (11C), various energy storage cycle combining engines and combining methods.   Water (52a) cooling compression blade compression which was disassembled after the bearing (12C) was provided at both ends, and the inner inner compression blade (8q) was fitted and fixed, etc., was confirmed by temporary assembly machine tools and both ends were held and ultra-high speed rotation balance processing was confirmed. Various energy storage cycle coalescing engines and coalescing methods, including a contra-rotating engine (12G) and a contra-rotating airplane (11E).   Water (52a) cooling compression blade compression which was disassembled after the bearing (12C) was provided at both ends, and the inner inner compression blade (8q) was fitted and fixed, etc., was confirmed by temporary assembly machine tools and both ends were held and ultra-high speed rotation balance processing was confirmed. Various energy storage cycle coalescing engines and coalescence methods of a counter rotating engine (12G) equipped with a rotary wing airplane (11I).   Water (52a) cooling compression blade compression which was disassembled after the bearing (12C) was provided at both ends, and the inner inner compression blade (8q) was fitted and fixed, etc., was confirmed by temporary assembly machine tools and both ends were held and ultra-high speed rotation balance processing was confirmed. Non-reversing engine (12G) equipped with Osprey extra large (11M) various energy storage cycle coalescing engine and coalescence method.   Water (52a) cooling compression blade compression which was disassembled after the bearing (12C) was provided at both ends, and the inner inner compression blade (8q) was fitted and fixed, etc., was confirmed by temporary assembly machine tools and both ends were held and ultra-high speed rotation balance processing was confirmed. Non-reversing injection engine (12E) equipped with counter-rotating injection ship (11F) and various energy storage cycle combining engines and combining methods.   Water (52a) cooling compression blade compression which was disassembled after the bearing (12C) was provided at both ends, and the inner inner compression blade (8q) was fitted and fixed, etc., was confirmed by temporary assembly machine tools and both ends were held and ultra-high speed rotation balance processing was confirmed. Non-reversing injection engine (12E) equipped with a counter-reversing injection airplane (11G) and various energy storage cycle combining engines and combining methods.   Water (52a) cooling compression blade compression which was disassembled after the bearing (12C) was provided at both ends, and the inner inner compression blade (8q) was fitted and fixed, etc., was confirmed by temporary assembly machine tools and both ends were held and ultra-high speed rotation balance processing was confirmed. Various energy storage cycle coalescing engines and coalescing methods, including a counter-rotating jet engine (12E) and a rotor blade jet airplane (11J).   Water (52a) cooling compression blade compression which was disassembled after the bearing (12C) was provided at both ends, and the inner inner compression blade (8q) was fitted and fixed, etc., was confirmed by temporary assembly machine tools and both ends were held and ultra-high speed rotation balance processing was confirmed. Non-reversing injection engine (12E) and various types of energy storage cycle coalescence engine and coalescence method with Osprey large size (11N).   Water (52a) cooling compression blade compression which was disassembled after the bearing (12C) was provided at both ends, and the inner inner compression blade (8q) was fitted and fixed, etc., was confirmed by temporary assembly machine tools and both ends were held and ultra-high speed rotation balance processing was confirmed. Non-reversing air injection engine (12F) equipped with a counter-rotating injection ship (11F) and various energy storage cycle combining engines and combining methods.   Bearings (12C) at both ends and annular inner compression blades (8q) fitted and fixed, etc. are temporarily assembled by a machine tool and disassembled after confirming that both ends are held at ultra-high speed rotation balance processing. Various energy storage cycle coalescing engine and coalescence method as a counter rotating vehicle (11B) equipped with a counter rotating engine (12G) as a two-stage compressor (12N) for compression.   Bearings (12C) at both ends and annular inner compression blades (8q) fitted and fixed, etc. are temporarily assembled by a machine tool and disassembled after confirming that both ends are held at ultra-high speed rotation balance processing. Various energy storage cycle coalescing engine and coalescence method as a contra-rotating ship (11C) equipped with a counter-rotating engine (12G) as a two-stage compressor (12N) for compression.   Bearings (12C) at both ends and annular inner compression blades (8q) fitted and fixed, etc. are temporarily assembled by a machine tool and disassembled after confirming that both ends are held at ultra-high speed rotation balance processing. Various energy storage cycle coalescence engine and coalescence method as a counter-rotating aircraft (11E) equipped with a counter-rotating engine (12G) as a two-stage compressor (12N) for compression.   Bearings (12C) at both ends and annular inner compression blades (8q) fitted and fixed, etc. are temporarily assembled by a machine tool and disassembled after confirming that both ends are held at ultra-high speed rotation balance processing. Various energy storage cycle coalescence engine and coalescence method as a rotary wing airplane (11I) equipped with a counter rotating engine (12G) which is a two-stage compressor (12N) for compression.   Bearings (12C) at both ends and annular inner compression blades (8q) fitted and fixed, etc. are temporarily assembled by a machine tool and disassembled after confirming that both ends are held at ultra-high speed rotation balance processing. Various energy storage cycle coalescence engines and coalescence methods, including a double reversing engine (12G) equipped with a two-stage compressor (12N) for compression and an Osprey extra large (11M).   Bearings (12C) at both ends and annular inner compression blades (8q) fitted and fixed, etc. are temporarily assembled by a machine tool and disassembled after confirming that both ends are held at ultra-high speed rotation balance processing. Various energy storage cycle coalescence engine and coalescence method as a counter-rotating jet engine (12E) equipped with a counter-rotating injection engine (12E) which is a two-stage compressor (12N) for compression.   Bearings (12C) at both ends and annular inner compression blades (8q) fitted and fixed, etc. are temporarily assembled by a machine tool and disassembled after confirming that both ends are held at ultra-high speed rotation balance processing. Various energy storage cycle coalescing engine and coalescence method as a counter-rotating injection airplane (11G) equipped with a counter-rotating injection engine (12E) in a two-stage compressor (12N) for compression.   Bearings (12C) at both ends and annular inner compression blades (8q) fitted and fixed, etc. are temporarily assembled by a machine tool and disassembled after confirming that both ends are held at ultra-high speed rotation balance processing. Various energy storage cycle coalescence engine and coalescence method as a rotary blade injection airplane (11J) equipped with a counter-rotating injection engine (12E) in a two-stage compressor (12N) for compression.   Bearings (12C) at both ends and annular inner compression blades (8q) fitted and fixed, etc. are temporarily assembled by a machine tool and disassembled after confirming that both ends are held at ultra-high speed rotation balance processing. Various energy storage cycle coalescing engine and coalescence method with a counter rotating injection engine (12E) equipped with a two-stage compressor (12N) for compression and an Osprey large size (11N).   Bearings (12C) at both ends and annular inner compression blades (8q) fitted and fixed, etc. are temporarily assembled by a machine tool and disassembled after confirming that both ends are held at ultra-high speed rotation balance processing. Various energy storage cycle coalescence engine and coalescence method as a counter-rotating jet ship (11F) equipped with a counter-rotating air injection engine (12F) that is a two-stage compressor (12N) for compression.   Water (52a) cooling compressor blade compression which is disassembled after the bearing (12C) is provided at both ends and the annular outer compression blade (8r) is fitted and fixed, and the both ends are held by a temporary assembly machine tool, and the ultra-high speed rotation balance processing is confirmed. Various energy storage cycle coalescing engines and coalescence methods of a non-reversing engine (12G).   Bearing (12C) at both ends, annular outer compression blades (8r) fitted and fixed, etc. Temporary assembly machine tool, both ends held after ultra-high speed rotation balance processing confirmed to be disassembled and finally assembled into water (52a) cooling blade compression Various energy storage cycle coalescence engine and coalescence method as a two-stage compressor (12N).   Water (52a) cooling compressor blade compression which is disassembled after the bearing (12C) is provided at both ends and the annular outer compression blade (8r) is fitted and fixed, and the both ends are held by a temporary assembly machine tool, and the ultra-high speed rotation balance processing is confirmed. Various energy storage cycle coalescing engines and coalescence methods of the counter-rotating injection engine (12E).   Water (52a) cooling compressor blade compression which is disassembled after the bearing (12C) is provided at both ends and the annular outer compression blade (8r) is fitted and fixed, and the both ends are held by a temporary assembly machine tool, and the ultra-high speed rotation balance processing is confirmed. Various energy storage cycle coalescence engines and coalescence methods of the counter-rotating air injection engine (12F).   Bearings (12C) at both ends, annular outer compression blades (8r) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high-speed rotation balance processing is confirmed and disassembled, and the reversing water cooling blade is compressed into the main assembly. Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating engine (12G), which is a two-stage compressor (12N) for compression.   Bearings (12C) at both ends, annular outer compression blades (8r) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high-speed rotation balance processing is confirmed and disassembled, and the reversing water cooling blade is compressed into the main assembly. Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating injection engine (12E) which is a two-stage compressor (12N) for compression.   Bearings (12C) at both ends, annular outer compression blades (8r) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high-speed rotation balance processing is confirmed and disassembled, and the reversing water cooling blade is compressed into the main assembly. Various energy storage cycle coalescence engine and coalescence method as a counter-rotating air injection engine (12F) which is a two-stage compressor (12N) for compression.   Water (52a) cooling compressor blade compression which is disassembled after the bearing (12C) is provided at both ends and the annular outer compression blade (8r) is fitted and fixed, and the both ends are held by a temporary assembly machine tool, and the ultra-high speed rotation balance processing is confirmed. Non-reversing engine (12G) and non-reversing motor vehicle (11B).   Water (52a) cooling compressor blade compression which is disassembled after the bearing (12C) is provided at both ends and the annular outer compression blade (8r) is fitted and fixed, and the both ends are held by a temporary assembly machine tool, and the ultra-high speed rotation balance processing is confirmed. Non-reversing engine (12G) equipped with non-reversing ship (11C), various energy storage cycle combining engines and combining methods.   Water (52a) cooling compressor blade compression which is disassembled after the bearing (12C) is provided at both ends and the annular outer compression blade (8r) is fitted and fixed, and the both ends are held by a temporary assembly machine tool, and the ultra-high speed rotation balance processing is confirmed. Various energy storage cycle coalescing engines and coalescing methods, including a contra-rotating engine (12G) and a contra-rotating airplane (11E).   Water (52a) cooling compressor blade compression which is disassembled after the bearing (12C) is provided at both ends and the annular outer compression blade (8r) is fitted and fixed, and the both ends are held by a temporary assembly machine tool, and the ultra-high speed rotation balance processing is confirmed. Various energy storage cycle coalescing engines and coalescence methods of a counter rotating engine (12G) equipped with a rotary wing airplane (11I).   Water (52a) cooling compressor blade compression which is disassembled after the bearing (12C) is provided at both ends and the annular outer compression blade (8r) is fitted and fixed, and the both ends are held by a temporary assembly machine tool, and the ultra-high speed rotation balance processing is confirmed. Non-reversing engine (12G) equipped with Osprey extra large (11M) various energy storage cycle coalescing engine and coalescence method.   Water (52a) cooling compressor blade compression which is disassembled after the bearing (12C) is provided at both ends and the annular outer compression blade (8r) is fitted and fixed, and the both ends are held by a temporary assembly machine tool, and the ultra-high speed rotation balance processing is confirmed. Non-reversing injection engine (12E) equipped with counter-rotating injection ship (11F) and various energy storage cycle combining engines and combining methods.   Water (52a) cooling compressor blade compression which is disassembled after the bearing (12C) is provided at both ends and the annular outer compression blade (8r) is fitted and fixed, and the both ends are held by a temporary assembly machine tool, and the ultra-high speed rotation balance processing is confirmed. Non-reversing injection engine (12E) equipped with a counter-reversing injection airplane (11G) and various energy storage cycle combining engines and combining methods.   Water (52a) cooling compressor blade compression which is disassembled after the bearing (12C) is provided at both ends and the annular outer compression blade (8r) is fitted and fixed, and the both ends are held by a temporary assembly machine tool, and the ultra-high speed rotation balance processing is confirmed. Various energy storage cycle coalescing engines and coalescing methods, including a counter-rotating jet engine (12E) and a rotor blade jet airplane (11J).   Water (52a) cooling compressor blade compression which is disassembled after the bearing (12C) is provided at both ends and the annular outer compression blade (8r) is fitted and fixed, and the both ends are held by a temporary assembly machine tool, and the ultra-high speed rotation balance processing is confirmed. Non-reversing injection engine (12E) and various types of energy storage cycle coalescence engine and coalescence method with Osprey large size (11N).   Water (52a) cooling compressor blade compression which is disassembled after the bearing (12C) is provided at both ends and the annular outer compression blade (8r) is fitted and fixed, and the both ends are held by a temporary assembly machine tool, and the ultra-high speed rotation balance processing is confirmed. Non-reversing air injection engine (12F) equipped with a counter-rotating injection ship (11F) and various energy storage cycle combining engines and combining methods.   Bearings (12C) at both ends, annular outer compression blades (8r) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high-speed rotation balance processing is confirmed and disassembled, and the reversing water cooling blade is compressed into the main assembly. Various energy storage cycle coalescing engine and coalescence method as a counter rotating vehicle (11B) equipped with a counter rotating engine (12G) as a two-stage compressor (12N) for compression.   Bearings (12C) at both ends, annular outer compression blades (8r) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high-speed rotation balance processing is confirmed and disassembled, and the reversing water cooling blade is compressed into the main assembly. Various energy storage cycle coalescing engine and coalescence method as a contra-rotating ship (11C) equipped with a counter-rotating engine (12G) as a two-stage compressor (12N) for compression.   Bearings (12C) at both ends, annular outer compression blades (8r) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high-speed rotation balance processing is confirmed and disassembled, and the reversing water cooling blade is compressed into the main assembly. Various energy storage cycle coalescence engine and coalescence method as a counter-rotating aircraft (11E) equipped with a counter-rotating engine (12G) as a two-stage compressor (12N) for compression.   Bearings (12C) at both ends, annular outer compression blades (8r) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high-speed rotation balance processing is confirmed and disassembled, and the reversing water cooling blade is compressed into the main assembly. Various energy storage cycle coalescence engine and coalescence method as a rotary wing airplane (11I) equipped with a counter rotating engine (12G) which is a two-stage compressor (12N) for compression.   Bearings (12C) at both ends, annular outer compression blades (8r) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high-speed rotation balance processing is confirmed and disassembled, and the reversing water cooling blade is compressed into the main assembly. Various energy storage cycle coalescence engines and coalescence methods, including a double reversing engine (12G) equipped with a two-stage compressor (12N) for compression and an Osprey extra large (11M).   Bearings (12C) at both ends, annular outer compression blades (8r) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high-speed rotation balance processing is confirmed and disassembled, and the reversing water cooling blade is compressed into the main assembly. Various energy storage cycle coalescence engine and coalescence method as a counter-rotating jet engine (12E) equipped with a counter-rotating injection engine (12E) which is a two-stage compressor (12N) for compression.   Bearings (12C) at both ends, annular outer compression blades (8r) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high-speed rotation balance processing is confirmed and disassembled, and the reversing water cooling blade is compressed into the main assembly. Various energy storage cycle coalescing engine and coalescence method as a counter-rotating injection airplane (11G) equipped with a counter-rotating injection engine (12E) in a two-stage compressor (12N) for compression.   Bearings (12C) at both ends, annular outer compression blades (8r) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high-speed rotation balance processing is confirmed and disassembled, and the reversing water cooling blade is compressed into the main assembly. Various energy storage cycle coalescence engine and coalescence method as a rotary blade injection airplane (11J) equipped with a counter-rotating injection engine (12E) in a two-stage compressor (12N) for compression.   Bearings (12C) at both ends, annular outer compression blades (8r) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high-speed rotation balance processing is confirmed and disassembled, and the reversing water cooling blade is compressed into the main assembly. Various energy storage cycle coalescing engine and coalescence method with a counter rotating injection engine (12E) equipped with a two-stage compressor (12N) for compression and an Osprey large size (11N).   Bearings (12C) at both ends, annular outer compression blades (8r) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high-speed rotation balance processing is confirmed and disassembled, and the reversing water cooling blade is compressed into the main assembly. Various energy storage cycle coalescence engine and coalescence method as a counter-rotating jet ship (11F) equipped with a counter-rotating air injection engine (12F) that is a two-stage compressor (12N) for compression.   Water (52a) cooling compressor blade compression disassembled after the bearings (12C) at both ends are fitted and fixed to the annular outer output blade (8t) and fixed at both ends with a temporary assembly machine tool after confirming that both ends are super-high speed rotation balance processing. Various energy storage cycle coalescing engines and coalescence methods of a non-reversing engine (12G).   Bearings (12C) provided at both ends, annular outer output blades (8t) fitted and fixed, etc. Temporary assembly machine tool confirmed that both ends are held and the high-speed rotation balance processing is confirmed, and then disassembled into the main assembly (52a) for cooling blade compression Various energy storage cycle coalescence engine and coalescence method as a two-stage compressor (12N).   Water (52a) cooling compressor blade compression disassembled after the bearings (12C) at both ends are fitted and fixed to the annular outer output blade (8t) and fixed at both ends with a temporary assembly machine tool after confirming that both ends are super-high speed rotation balance processing. Various energy storage cycle coalescing engines and coalescence methods of the counter-rotating injection engine (12E).   Water (52a) cooling compressor blade compression disassembled after the bearings (12C) at both ends are fitted and fixed to the annular outer output blade (8t) and fixed at both ends with a temporary assembly machine tool after confirming that both ends are super-high speed rotation balance processing. Various energy storage cycle coalescence engines and coalescence methods of the counter-rotating air injection engine (12F).   Bearings (12C) are provided at both ends and the annular outer output blade (8t) is fitted and fixed. Temporary assembly machine tool holds both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble the compressed part in this assembly. Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating engine (12G), which is a two-stage compressor (12N) for compression.   Bearings (12C) are provided at both ends and the annular outer output blade (8t) is fitted and fixed. Temporary assembly machine tool holds both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble the compressed part in this assembly. Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating injection engine (12E) which is a two-stage compressor (12N) for compression.   Bearings (12C) are provided at both ends and the annular outer output blade (8t) is fitted and fixed. Temporary assembly machine tool holds both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble the compressed part in this assembly. Various energy storage cycle coalescence engine and coalescence method as a counter-rotating air injection engine (12F) which is a two-stage compressor (12N) for compression.   Water (52a) cooling compressor blade compression disassembled after the bearings (12C) at both ends are fitted and fixed to the annular outer output blade (8t) and fixed at both ends with a temporary assembly machine tool after confirming that both ends are super-high speed rotation balance processing. Non-reversing engine (12G) and non-reversing motor vehicle (11B).   Water (52a) cooling compressor blade compression disassembled after the bearings (12C) at both ends are fitted and fixed to the annular outer output blade (8t) and fixed at both ends with a temporary assembly machine tool after confirming that both ends are super-high speed rotation balance processing. Non-reversing engine (12G) equipped with non-reversing ship (11C), various energy storage cycle combining engines and combining methods.   Water (52a) cooling compressor blade compression disassembled after the bearings (12C) at both ends are fitted and fixed to the annular outer output blade (8t) and fixed at both ends with a temporary assembly machine tool after confirming that both ends are super-high speed rotation balance processing. Various energy storage cycle coalescing engines and coalescing methods, including a contra-rotating engine (12G) and a contra-rotating airplane (11E).   Water (52a) cooling compression blade compression disassembled after the bearing (12C) squeezed at both ends and disassembled after confirming that both ends are held at the high-speed rotation balance with a temporary assembly machine tool by fixing the annular outer output blade (8t). Various energy storage cycle coalescing engines and coalescence methods of a counter rotating engine (12G) equipped with a rotary wing airplane (11I).   Water (52a) cooling compressor blade compression disassembled after the bearings (12C) at both ends are fitted and fixed to the annular outer output blade (8t) and fixed at both ends with a temporary assembly machine tool after confirming that both ends are super-high speed rotation balance processing. Non-reversing engine (12G) equipped with Osprey extra large (11M) various energy storage cycle coalescing engine and coalescence method.   Water (52a) cooling compressor blade compression disassembled after the bearings (12C) at both ends are fitted and fixed to the annular outer output blade (8t) and fixed at both ends with a temporary assembly machine tool after confirming that both ends are super-high speed rotation balance processing. Non-reversing injection engine (12E) equipped with counter-rotating injection ship (11F) and various energy storage cycle combining engines and combining methods.   Water (52a) cooling compressor blade compression disassembled after the bearings (12C) at both ends are fitted and fixed to the annular outer output blade (8t) and fixed at both ends with a temporary assembly machine tool after confirming that both ends are super-high speed rotation balance processing. Non-reversing injection engine (12E) equipped with a counter-reversing injection airplane (11G) and various energy storage cycle combining engines and combining methods.   Water (52a) cooling compressor blade compression disassembled after the bearings (12C) at both ends are fitted and fixed to the annular outer output blade (8t) and fixed at both ends with a temporary assembly machine tool after confirming that both ends are super-high speed rotation balance processing. Various energy storage cycle coalescing engines and coalescing methods, including a counter-rotating jet engine (12E) and a rotor blade jet airplane (11J).   Water (52a) cooling compressor blade compression disassembled after the bearings (12C) at both ends are fitted and fixed to the annular outer output blade (8t) and fixed at both ends with a temporary assembly machine tool after confirming that both ends are super-high speed rotation balance processing. Non-reversing injection engine (12E) and various types of energy storage cycle coalescence engine and coalescence method with Osprey large size (11N).   Water (52a) cooling compressor blade compression disassembled after the bearings (12C) at both ends are fitted and fixed to the annular outer output blade (8t) and fixed at both ends with a temporary assembly machine tool after confirming that both ends are super-high speed rotation balance processing. Non-reversing air injection engine (12F) equipped with a counter-rotating injection ship (11F) and various energy storage cycle combining engines and combining methods.   Water (52a) cooling compressor blade compression disassembled after the bearings (12C) at both ends are fitted and fixed to the annular outer output blade (8t) and fixed at both ends with a temporary assembly machine tool after confirming that both ends are super-high speed rotation balance processing. Non-reversing engine (12G) Water (52a) Cooling outer compression blade (8r) Inner compression blade (8q)   Water (52a) cooling compressor blade compression disassembled after the bearings (12C) at both ends are fitted and fixed to the annular outer output blade (8t) and fixed at both ends with a temporary assembly machine tool after confirming that both ends are super-high speed rotation balance processing. Non-reversing engine (12G) Water (52a) Cooling outer compression blade (8r) Inner compression blade (8q)   Bearings (12C) are provided at both ends and the annular outer output blade (8t) is fitted and fixed. Temporary assembly machine tool holds both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble the compressed part in this assembly. Various energy storage cycle coalescing engines and coalescence methods comprising a counter rotating engine (12G) water (52a) cooled outer compressor blade (8r) and inner compressor blade (8q) in a two-stage compressor (12N) for compression.   Bearings (12C) are provided at both ends and the annular outer output blade (8t) is fitted and fixed. Temporary assembly machine tool holds both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble the compressed part in this assembly. Combined engine and method for combining various energy storage cycles into a counter rotating engine (12G) water (52a) cooled outer compression blade (8r) and inner compression blade (8q) made into a two-stage compressor (12N) for compression.   Bearings (12C) are provided at both ends and the annular outer output blade (8t) is fitted and fixed. Temporary assembly machine tool holds both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble the compressed part in this assembly. Various energy storage cycle coalescing engine and coalescence method as a counter rotating vehicle (11B) equipped with a counter rotating engine (12G) as a two-stage compressor (12N) for compression.   Bearings (12C) are provided at both ends and the annular outer output blade (8t) is fitted and fixed. Temporary assembly machine tool holds both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble the compressed part in this assembly. Various energy storage cycle coalescing engine and coalescence method as a contra-rotating ship (11C) equipped with a counter-rotating engine (12G) as a two-stage compressor (12N) for compression.   Bearings (12C) are provided at both ends and the annular outer output blade (8t) is fitted and fixed. Temporary assembly machine tool holds both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble the compressed part in this assembly. Various energy storage cycle coalescence engine and coalescence method as a counter-rotating aircraft (11E) equipped with a counter-rotating engine (12G) as a two-stage compressor (12N) for compression.   Bearings (12C) are provided at both ends and the annular outer output blade (8t) is fitted and fixed. Temporary assembly machine tool holds both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble the compressed part in this assembly. Various energy storage cycle coalescence engine and coalescence method as a rotary wing airplane (11I) equipped with a counter rotating engine (12G) which is a two-stage compressor (12N) for compression.   Bearings (12C) are provided at both ends and the annular outer output blade (8t) is fitted and fixed. Temporary assembly machine tool holds both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble the compressed part in this assembly. Various energy storage cycle coalescence engines and coalescence methods, including a double reversing engine (12G) equipped with a two-stage compressor (12N) for compression and an Osprey extra large (11M).   Bearings (12C) are provided at both ends and the annular outer output blade (8t) is fitted and fixed. Temporary assembly machine tool holds both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble the compressed part in this assembly. Various energy storage cycle coalescence engine and coalescence method as a counter-rotating jet engine (12E) equipped with a counter-rotating injection engine (12E) which is a two-stage compressor (12N) for compression.   Bearings (12C) are provided at both ends and the annular outer output blade (8t) is fitted and fixed. Temporary assembly machine tool holds both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble the compressed part in this assembly. Various energy storage cycle coalescing engine and coalescence method as a counter-rotating injection airplane (11G) equipped with a counter-rotating injection engine (12E) in a two-stage compressor (12N) for compression.   Bearings (12C) are provided at both ends and the annular outer output blade (8t) is fitted and fixed. Temporary assembly machine tool holds both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble the compressed part in this assembly. Various energy storage cycle coalescence engine and coalescence method as a rotary blade injection airplane (11J) equipped with a counter-rotating injection engine (12E) in a two-stage compressor (12N) for compression.   Bearings (12C) are provided at both ends and the annular outer output blade (8t) is fitted and fixed. Temporary assembly machine tool holds both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble the compressed part in this assembly. Various energy storage cycle coalescing engine and coalescence method with a counter rotating injection engine (12E) equipped with a two-stage compressor (12N) for compression and an Osprey large size (11N).   Bearings (12C) are provided at both ends and the annular outer output blade (8t) is fitted and fixed. Temporary assembly machine tool holds both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble the compressed part in this assembly. Various energy storage cycle coalescence engine and coalescence method as a counter-rotating jet ship (11F) equipped with a counter-rotating air injection engine (12F) that is a two-stage compressor (12N) for compression.   Water (52a) cooling compressor blade compression disassembled after the bearings (12C) at both ends are fitted and fixed to the annular outer output blade (8t) and fixed at both ends with a temporary assembly machine tool after confirming that both ends are super-high speed rotation balance processing. Non-reversing engine (12G) Water (52a) Cooling outer compressor blade (8r) Inner compressor blade (8q) Cooling blade   Water (52a) cooling compressor blade compression disassembled after the bearings (12C) at both ends are fitted and fixed to the annular outer output blade (8t) and fixed at both ends with a temporary assembly machine tool after confirming that both ends are super-high speed rotation balance processing. Non-reversing engine (12G) Water (52a) Cooling outer compression blade (8r) Inner compression blade (8q) Cooling compression blade Various energy storage cycle coalescence engine and coalescence method.   Bearings (12C) are provided at both ends and the annular outer output blade (8t) is fitted and fixed. Temporary assembly machine tool holds both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble the compressed part in this assembly. Various energy storage cycle coalescence engine and coalescence method as a double reversing engine (12G) water (52a) cooled outer compression blade (8r) inner compression blade (8q) cooling blade in a two-stage compressor (12N) for compression.   Bearings (12C) are provided at both ends and the annular outer output blade (8t) is fitted and fixed. Temporary assembly machine tool holds both ends, and after confirming good balance processing of ultra-high speed rotation, disassemble and disassemble the compressed part in this assembly. Rotating compressor (12G) water reversing engine (12a) water (52a) cooled outer compressor blade (8r) inner compressor blade (8q) cooled compressor blade combined with various energy storage cycle engines and coalescence method .   Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Various energy storage cycle coalescing engines and coalescence methods of a non-reversing engine (12G).   Bearing (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is used for both-end holding Ultra-high speed rotation Balance processing is disassembled after confirming good processing (52a) cooling blade compression Various energy storage cycle coalescence engine and coalescence method as a two-stage compressor (12N).   Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Various energy storage cycle coalescing engines and coalescence methods of the counter-rotating injection engine (12E).   Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Various energy storage cycle coalescence engines and coalescence methods of the counter-rotating air injection engine (12F).   Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating engine (12G), which is a two-stage compressor (12N) for compression.   Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly Various energy storage cycle coalescence engines and coalescence methods as a counter-rotating injection engine (12E) which is a two-stage compressor (12N) for compression.   Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly Various energy storage cycle coalescence engine and coalescence method as a counter-rotating air injection engine (12F) which is a two-stage compressor (12N) for compression.   Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Non-reversing engine (12G) and non-reversing motor vehicle (11B).   Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Non-reversing engine (12G) equipped with non-reversing ship (11C), various energy storage cycle combining engines and combining methods.   Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Various energy storage cycle coalescing engines and coalescing methods, including a contra-rotating engine (12G) and a contra-rotating airplane (11E).   Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Various energy storage cycle coalescing engines and coalescence methods of a counter rotating engine (12G) equipped with a rotary wing airplane (11I).   Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Non-reversing engine (12G) equipped with Osprey extra large (11M) various energy storage cycle coalescing engine and coalescence method.   Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Non-reversing injection engine (12E) equipped with counter-rotating injection ship (11F) and various energy storage cycle combining engines and combining methods.   Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Non-reversing injection engine (12E) equipped with a counter-reversing injection airplane (11G) and various energy storage cycle combining engines and combining methods.   Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Various energy storage cycle coalescing engines and coalescing methods, including a counter-rotating jet engine (12E) and a rotor blade jet airplane (11J).   Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Non-reversing injection engine (12E) and various types of energy storage cycle coalescence engine and coalescence method with Osprey large size (11N).   Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Non-reversing air injection engine (12F) equipped with a counter-rotating injection ship (11F) and various energy storage cycle combining engines and combining methods.   Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Non-reversing engine (12G) Water (52a) Cooling outer compression blade (8r) Inner compression blade (8q)   Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Non-reversing engine (12G) Water (52a) Cooling outer compression blade (8r) Inner compression blade (8q)   Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly Various energy storage cycle coalescing engines and coalescence methods comprising a counter rotating engine (12G) water (52a) cooled outer compressor blade (8r) and inner compressor blade (8q) in a two-stage compressor (12N) for compression.   Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly Combined engine and method for combining various energy storage cycles into a counter rotating engine (12G) water (52a) cooled outer compression blade (8r) and inner compression blade (8q) made into a two-stage compressor (12N) for compression.   Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly Various energy storage cycle coalescing engine and coalescence method as a counter rotating vehicle (11B) equipped with a counter rotating engine (12G) as a two-stage compressor (12N) for compression.   Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly Various energy storage cycle coalescing engine and coalescence method as a contra-rotating ship (11C) equipped with a counter-rotating engine (12G) as a two-stage compressor (12N) for compression.   Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly Various energy storage cycle coalescence engine and coalescence method as a counter-rotating aircraft (11E) equipped with a counter-rotating engine (12G) as a two-stage compressor (12N) for compression.   Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly Various energy storage cycle coalescence engine and coalescence method as a rotary wing airplane (11I) equipped with a counter rotating engine (12G) which is a two-stage compressor (12N) for compression.   Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly Various energy storage cycle coalescence engines and coalescence methods, including a double reversing engine (12G) equipped with a two-stage compressor (12N) for compression and an Osprey extra large (11M).   Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly Various energy storage cycle coalescence engine and coalescence method as a counter-rotating jet engine (12E) equipped with a counter-rotating injection engine (12E) which is a two-stage compressor (12N) for compression.   Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly Various energy storage cycle coalescing engine and coalescence method as a counter-rotating injection airplane (11G) equipped with a counter-rotating injection engine (12E) in a two-stage compressor (12N) for compression.   Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly Various energy storage cycle coalescence engine and coalescence method as a rotary blade injection airplane (11J) equipped with a counter-rotating injection engine (12E) in a two-stage compressor (12N) for compression.   Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly Various energy storage cycle coalescing engine and coalescence method with a counter rotating injection engine (12E) equipped with a two-stage compressor (12N) for compression and an Osprey large size (11N).   Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly Various energy storage cycle coalescence engine and coalescence method as a counter-rotating jet ship (11F) equipped with a counter-rotating air injection engine (12F) that is a two-stage compressor (12N) for compression.   Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Non-reversing engine (12G) Water (52a) Cooling outer compressor blade (8r) Inner compressor blade (8q) Cooling blade   Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Non-reversing engine (12G) Water (52a) Cooling outer compression blade (8r) Inner compression blade (8q) Cooling compression blade Various energy storage cycle coalescence engine and coalescence method.   Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly Various energy storage cycle coalescence engine and coalescence method as a double reversing engine (12G) water (52a) cooled outer compression blade (8r) inner compression blade (8q) cooling blade in a two-stage compressor (12N) for compression.   Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly Rotating compressor (12G) water reversing engine (12a) water (52a) cooled outer compressor blade (8r) inner compressor blade (8q) cooled compressor blade combined with various energy storage cycle engines and coalescence method .   Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Various reversible engine (12G) using solar heater (21) heated air (28a) as intake air and water (52a) cooling outer compression blade (8r) inner compression blade (8q) cooling energy Storage cycle coalescence engine and coalescence method.   Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Various reversing engines (12G) using solar heater (21) heated air (28a) for intake air, water (52a) cooling outer compression blade (8r) inner compression blade (8q) cooling compression blade Energy conservation cycle coalescence engine and coalescence method.   Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly A double reversing engine (12G) made into a two-stage compressor (12N) for compression uses solar air heater (21) heated air (28a) for intake air, water (52a) cooling outer compression blade (8r) inner compression Various energy storage cycle coalescence engine and coalescence method using blade (8q) cooling blade.   Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly A double reversing engine (12G) made into a two-stage compressor (12N) for compression uses solar air heater (21) heated air (28a) for intake air, water (52a) cooling outer compression blade (8r) inner compression Various energy storage cycle coalescing engine and coalescence method using a blade (8q) cooled compression blade.   Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Non-reversing engine (12G) using air (28a) heated by exhaust gas as intake air, water (52a) cooling outer compression blade (8r) inner compression blade (8q) cooling blade combined with various energy storage cycle combined engines And coalescing method.   Water (52a) cooling compression blade compression which was disassembled after the bearings (12C) at both ends and the inner ring output blade (8s) fitted and fixed at the both ends, etc. were confirmed with a temporary assembly machine tool after both ends were held and ultra-high speed rotation balance processing was confirmed. Combined with various energy storage cycles using the air (28a) heated by exhaust as the intake air of the counter-rotating engine (12G) of water (52a) cooled outer compressor blade (8r) inner compressor blade (8q) cooled compressor blade Organization and coalescence method.   Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly A counter-rotating engine (12G) made of a two-stage compressor (12N) for compression uses air (28a) heated by exhaust as intake air and water (52a) cooling outer compression blade (8r) inner compression blade (8q) Various energy storage cycle coalescence engines and coalescence methods as cooling blades.   Bearings (12C) at both ends, annular inner output blade (8s) fitted and fixed, etc. Temporary assembly machine tool is supported after both ends hold and ultra-high speed rotation balance processing is confirmed and disassembled, and the compressed part is counter-rotated with water cooling blade in this assembly A counter-rotating engine (12G) made of a two-stage compressor (12N) for compression uses air (28a) heated by exhaust as intake air and water (52a) cooling outer compression blade (8r) inner compression blade (8q) Various energy storage cycle coalescence engines and coalescence methods as cooling compression blades.