JP2009191836A - Various energy conservation cycle combined engine - Google Patents

Abstract

<P>PROBLEM TO BE SOLVED: To solve a problem that there is a risk of annihilation since thermal and nuclear power generation causes a rise in seawater temperatures by the whole electric-generating capacity and heat quantity, seawater temperatures exceed thousand times within a century if China continues to grow at the rate of 10%, and this increases torrential rain and the wind speed of a typhoon 10 to 100 times. <P>SOLUTION: Combustion gas heat quantity explosion power and combustion gas mass explosion power are dividedly conserved and used. Water is accelerated with gravity acceleration of 9.8 meters at each second added downward in a vertical direction within a vacuum for driving a full moving blade mercury turbine and a full moving blade water turbine. Heat consumption is set to 1/539 by the use of gasification explosion power as the maximum acceleration in a human history in comparison by the use of superheated vapor. Power having the same speed and the same heat quantity as the atmosphere pressure with an uncalculated large output of the whole moving blade with the worst stator blades of the existing turbine abolished is increased 910,000 times the use of superheated vapor. An electric-generating capacity is increased 200 times the existing steam turbine using the same amount of fuel by the water injection of a volumetric capacity of 1/4,000 of superheated vapor. The full moving blade gas turbine is driven around 0 Kelvin of an exhaust gas temperature by the combustion gas mass explosion power. Thereby, there are no rise in seawater temperatures and CO<SB>2</SB>emission, and marine algae, fishes or the like which are cooled at the bottom of sea are grown by combustion gas-dissolved water after recovering and using cold. <P>COPYRIGHT: (C)2009,JPO&INPIT

Description

  Various energy storage cycle coalescing engines of the theoretical best engine invention drive all blade vane mercury turbines to a vacuum higher than or equal to that of existing steam turbines, and heat recovery intake air 28a temperature from around 220 degrees Celsius to 60-100 heat recovery intake air temperature. As the heat pump 1G, the combustion gas 49 heat amount or the compressed air heat amount is recovered to around 200 degrees by the compression heat recovery device 2C, and the compression is 600 to 1000 degrees by the energy storage compressor 20X or the existing compressor 20Y. Reduced compression chamber mercury heat is heated by mercury + water in the reduced diameter compression chamber mercury heat exchanger 2Z and the air temperature is cooled by mercury + water several times around 200 ° C. In the process of cooling the cooling heat recovery air temperature in the exchanger 2Z, the high pressure combustion heat exchange cooling combustion is performed without limit to the fuel injection combustion, and the high pressure high temperature mercury explosive force + high pressure high temperature water explosive force + High-pressure high-temperature water explosive power that is divided into pressure combustion gas mass explosive power and used as CO2 exhaust gas 0 seawater temperature rise 0 power generation, etc. + High pressure combustion gas mass It relates to the technology to prevent the global warming by dividing and storing it into the explosive force of the CO2 exhaust gas, 0 seawater temperature rise 0 power generation, etc.

  Mercury deficiency is obvious, usually divided into high pressure high temperature water explosive force + high pressure combustion gas mass explosive force, and low temperature high pressure combustion gas mass explosive force around 40 degrees C ordinarily low temperature such as 24-400MPa, all rotor blade gas The maximum amount of cold collected by the turbine is maximized, and cold heat such as CO2 is supplied to the seawater cooling seabed as combustion gas-dissolved water, phytoplankton and seaweeds are propagated, and fish depletion due to the food chain is reversed and increased. The combustion gas 49 heat quantity or the compressed air heat quantity 28b is recovered and compressed by the intake air 28a, and the heat is recovered by the compression heat recovery unit 2C, and is compressed by the diameter expansion compression chamber 10a of the energy storage compressor 20X to about 200 degrees 28a. In the course of cooling the final compression heat recovery air 28a in the water heat exchanger 2Y at 600 to 1000 degrees, the high pressure combustion heat exchange cooling combustion is performed as much as fuel injection combustion, high pressure high temperature water 52b explosive force + high pressure combustion gas 49 mass explosion The high-pressure high-temperature water 52b is injected from the water injection pump 6z and used to divide the power into the power, and the full-blade water turbine is driven as the high-temperature water 52b vaporization explosive force such as 374 degrees 400 MPa, and the existing fuel amount is the same. The invention relates to a technology for preventing global warming by generating a seawater temperature rise 0 power generation by cooling the cooling heat 52e in the exhaust process.

  When the entire blade blade water turbine is driven by the explosive force of the critical temperature of 374 degrees 400 MPa high-pressure high-temperature water 52b, the heat consumption is reduced to 1/539 of that using superheated steam, and the gravity acceleration is 9.8 m vertically downward in vacuum. / Acceleration per second is added, and high-pressure high-temperature water 52b is concentrated in the low-pressure part at the rear of the traveling direction in the process of acceleration, making it the second best theoretical acceleration that far exceeds the use of superheated steam. The selected turbine blade section 40X output side heating high temperature means 3B or the like is used as a high temperature turbine blade, and the configuration is such that the entire blade blade water turbine is driven by the rolling contact of the high temperature water 52b by vaporization of the contact surface. The steam turbine is set to 1700 times * 539 = approx. The target speed is 1/4000 calorie water injection at the same speed as the bottle, and 200 times rotation output is aimed at. The exhaust gas is cooled by cooling 52e, the seawater temperature rises to 0 power generation, the saturation exhaust temperature is about 25 degrees maximum vacuum maximum rotation output, and about 40 degrees 24 degrees. The present invention relates to a technology that enables a mass explosive force of 49 MPa low-temperature high-pressure combustion gas, etc., and enables maximum recovery and use of cold heat by all rotor blade gas turbines, and maximum combustion amount maximum rotation output.

  In the process of using the high-pressure high-temperature mercury explosive force stored separately, for example, by using the vaporization explosive force of high-pressure high-temperature mercury 1d such as 430 to 800 degrees 400 MPa, the heat consumption is reduced to 0.035 / 0.999 by specific heat. = Reduced to about 1/28, 400 MPa high pressure injection speed of mercury injection pump 6Z appropriately configured with gear pump, etc. High pressure high temperature mercury is injected vertically downward, acceleration of gravity is 9.8 m / second per second in vacuum , The vaporization explosive force is concentrated on the low-pressure part at the rear of the high-speed liquid mercury to achieve the best theoretical acceleration, and the high-pressure high-temperature mercury 1d surface tension has the maximum rolling output with minimal friction loss due to rolling contact. Exceeding the large power output of all rotor blades that completely abolished the worst blades of the turbine, the atmospheric pressure, the same speed, and the same calorific power, kg weight m / sec, was 910,000 times that of using superheated steam * 13.5 * 28 = about 34,000 Many times With the same speed 1 / 1.7 million heat quantity mercury injection, the rotation output is about 200 times that of superheated steam, and it is mainly used for spacecrafts. The present invention relates to various energy storage cycle coalescence engine technologies used for various heating facilities and various heating facilities.

  In the process of using the high-pressure combustion gas mass explosive force stored separately, for example, the existing gas turbine 100-times pressure rotation output and 1000-times injection pressure injection propulsion output, etc. In the process of generating all rotor blade gas turbine drive rotation output, the turbine blade 8c of the turbine blade cross section 4X is provided with cold heat recovery means 3C to recover the cold heat with alcohol 1C, etc., and moisture, dry ice, etc. In the exhaust process, all the combustion gas is brought close to 0 degrees, and heat is exchanged with alcohol, air, or water in the internal and external cold recovery units 103, 103, and alcohol cold 52e or compressed air cold 52e approaches -100 degrees and -210 degrees, and CO2 is stored in dry ice below -80 degrees for optimal use for large fish growth. Enables the maximum use of production and sales together with the equipment, dissolves the remaining combustion gas in water Combustion gas dissolved water, cools the nutrient supply seawater to the seabed, and supplies an appropriate amount of CO2 in the process of supplying nutrients to the seabed Maximizing the use of seaweed and phytoplankton that proliferate the most CO2 and increasing the number of fish, etc. by the food chain, increasing the seawater temperature of the existing power generation technology, killing phytoplankton, and drastically reducing fish by the food chain It is related to various energy conservation cycle coalescence engine technology that reverses and prevents seawater cooling power generation and human extinction.

  Uses all-blade mercury turbine + all-blade water turbine for the rotational output of the jet propulsion output of a spacecraft, etc., and uses all-blade water turbine for the rotational output of the ship injection propulsion to respond to scarce mercury resources Combustion with a large residual amount of oxygen such as 24-400 MPa around 40 degrees Celsius, which was used for heating of mercury + water and water by adding injection of superheated steam 50-around 400 degrees around 400 degrees to increase injection propulsion output The gas 49 is mass-produced, for example, the superheated steam 50 is supplied to the superheated steam reservoir 95c on the outer periphery of the combined engine injection unit 79K combustor 1Y, the combustion gas is supplied to the combustor 1Y, the fuel is injected and burned, and the superheated steam temperature on the outer periphery is increased. The combustor 1Y is cooled and burned by the long cooling fin 5B of the combustor 1Y, the fuel combustion amount is increased and the combustion temperature is increased to increase the injection propulsion output, and the fuel is injected into the combustion gas injection flow. The theoretical air fuel ratio Nearly firing, the propulsion power is increased, the simplest theoretical best jet propulsion is 10 times the propulsion power of the existing technology, and the wing levitation is a totally abandoned stable flight wing. It is used for various airplanes, various spacecrafts, and various ships, and is used as a facility for supplying heat, electricity, and cold during the outage. Thus, the present invention relates to various energy storage cycle coalescence engines that postpone the danger of becoming impossible to prevent human extinction due to abnormal weather in around 100 years.

  Elementary school engine output and work load kg weight m / second, etc., are all mass * speed within unit time, and the existing reciprocating engine, steam turbine and gas turbine inventions were rejected by elementary school science in addition to failure. For example, in existing steam turbines, the atmospheric pressure, the same speed, and the same calorific power are set to 1 / 910,000 kg weight m / second of the whole blade water turbine, and the blades are further reduced. To reduce the rotational output and drive generators. At nuclear power plants and thermal power plants around the world, the sea surface temperature is increased by 7 degrees Celsius with the total amount of heat used. Decreasing cooling, making it impossible for the natural phenomenon of supplying nutrients such as oxygen, nitrogen and CO2 to the sea floor, gradually increasing the dead sea such as corals and accelerating extinction of seaweeds and seafood, etc. And, for example, 1 ton for the birth of a 1kg fish in the waters near Japan Necessary phytoplankton is killed, and the number of sardine inhabitants is reduced to 1/200 by the food chain. The Arctic and Antarctic ice is melted around 100 years and the sea level rises by 5-6 meters or nearly 70 meters. Then, the sea surface temperature is increased from 45 to 50 degrees, and typhoons and seasonal winds such as 300 meters / second are expected to be created. There is an urgent need for the invention of a power generation engine and a ship engine that reduce CO2 exhaust and prevent seawater temperature rise to prevent global warming.

  Increasing seawater temperature anomalous weather Methane hydrate decomposition Increasing the danger of human extinction, exhausting all used combustion gases and CO2 into the atmosphere, increasing the danger of global warming and human extinction The thermal power plants and nuclear power plants in the world have an enormous heat demand by improving the obsolete invention when it was sufficient to generate rotational output, but the seawater temperature 80 to 160 times the amount of steam generated by the steam turbine To 7 degrees Celsius, melting the Arctic and Antarctic ice, increasing the risk of methane hydrate decomposition and extinction of mankind, generating rotational output with superheated steam with atmospheric pressure weight of 1/23000, A deadly stupid rotation in which the pressure at the same speed and the power kg kg m / sec are reduced to 1/23000 of the total turbine mercury turbine, the superheated steam velocity is dammed by the stationary blade, the direction of deceleration is changed, and the blade is injected into the blade. Output, mass of combustion gas or heat In addition to the silly rotational output that is not used at all, various rotational output drive devices such as thermal power plants, vehicles, ships and airplanes exhaust all the combustion gas and CO2 used to the atmosphere, There are many deadly foolish parts that accelerate global warming, and there are no inventions around 100 years ago, so there are background technologies where the number of inventions exceeds 1 million and becomes enormous.

  The existing jet aircraft is a deadly stupid that repeats conversion to decelerated air pressure by damaging the compressed air velocity by moving blades with stationary blades by improving the obsolete invention when it is sufficient to generate rotation output and injection propulsion output Compressed air, generates rotational output with a high-temperature combustion gas whose atmospheric pressure weight is 1/29000 of mercury, makes the atmospheric pressure same speed power kg weight m / sec to 1/28800 of the whole moving blade mercury turbine, combustion gas Stupid rotation output that dams the speed with a stationary blade and changes the direction of deceleration and injects it onto the rotor blade. When divided and used as combustion gas calorie output + combustion gas mass output, it sucks in compressed air heat and exhaust heat. Theoretical best heat pump that uses recovered and compressed heat recovery with air can be configured, but in addition to the foolish rotation output that does not use the combustion gas calorific value at all, the combustion gas that has become a very low pressure and low speed by generating a rotation output Spray The injection propulsion output as stupid configuration be greatly reduced, etc. to be very extremely insignificant the injection propulsion output, stupid part is there is a very large background technology.

  Existing gasoline engines and diesel engines improve the obsolete invention at the time when it is sufficient to generate rotational output, and because it uses a volume that does not consider a rational configuration at all, near dead center or near dead center that does not generate rotational output For the best machine that emits the maximum energy and generates 90 degree rotation output after dead center, the most foolish rotation output that reduces the released energy to 1/6 or less is used in power generation, vehicles, ships and airplanes. There are many deadly stupid parts that exhaust all the high-temperature combustion gas and CO2 used to the atmosphere and accelerate global warming, and the engine cannot be improved. There is a background technology that becomes, and in addition, there is a background technology where compression technology for compressing gas and liquid is very good.

I decided to invent the theoretical best engine in Showa 17-18 and started prototyping at the contract of the Okayama Regional Invention Center in 1963 and continued to make the prototype myself, but the engine prototype is very difficult. Therefore, in February 1982, we started requesting cooperation from a large number of domestic large corporations, etc., but there was no cooperation from Japanese companies, etc., and every time we asked for the cooperation of President Clinton, the only request from foreign countries, three times a year, The 1992 US Patent 5133305, 1993 US Patent 5230307, and 1995 US Patent 5429078 were found to be useless. It was found that there were so many fatal faults in the existing engine that it was impossible to invent the first one, and suddenly, the 1997 homepage was opened and an improvement patent was filed one by one for the faults. It is what you have reached.
There are US Pat. No. 6,119,650, Chinese Patent No. 8818, EU British Patent No. 902175, US Pat. No. 6,263,664, which is an invention in the process of improving the above-mentioned many background technologies and the following Patent Document 2 theoretical best engine invention. As prior applications, Japanese Patent Application No. 2005-34153, Japanese Patent Application No. 2005-114523, Japanese Patent Application No. 2005-137216, Japanese Patent Application No. 2005-177793, Japanese Patent Application No. 2005-223970, Japanese Patent Application No. 2005-230604, Japanese Patent Application No. 2005 No. 237413, Japanese Patent Application No. 2005-24783, Japanese Patent Application No. 2005-289820, Japanese Patent Application No. 2005-305330, Japanese Patent Application No. 2005-319358, Japanese Patent Application No. 2005-338172, Japanese Patent Application No. 2006-260020, Japanese Patent Application No. 2006-327809. No., Japanese Patent Application No. 2007-179204, Japanese Patent Application No. 2007-221970, Japanese Patent Application No. 2007-237367, Japanese Patent Application No. 2007-250348, Japanese Patent Application No. 2007-265115, Japanese Patent Application No. 2008-006612, and Japanese Patent Application No. 2008-022246. , Japanese Patent Application No. 2008-02465 Patent, Japanese Patent Application No. 2008-028582, there is Japanese Patent Application No. 2008-030162.

  Thermal power plants and nuclear power plants in the existing world will increase the sea surface temperature by 7 degrees Celsius with the total amount of heat generated, and if China continues to grow 10%, for example, the rate of sea water temperature will increase by 1000 times in around 100 years Methane hydride that melts ice from Antarctica, etc. beyond sea level, increases the sea level by 5-6 m, increases the risk of typhoons and seasonal winds such as 300 m / sec, and begins to decompose at a seawater temperature rise of 2-3 degrees Rate-decomposition Increases the danger of human extinction, for example, kills phytoplankton even in the seas near Japan, drastically reduces zooplankton, drastically reduces the number of sardine inhabitants to 1/200, etc. by the food chain, Since it has started to update the record of heavy rain, heavy snow, typhoon wind speed, tornado, seasonal wind speed, cold wave, heat wave, hail, etc. And cold heat Used as equipment, heat exchange is performed by using heat pump 1G with a heat pump of about 900 degrees of compression, and excess heat corresponding to the amount of heat supplied is also about 900 degrees of heat. Heat exchange Various types of heating for home and business use There is a problem that it is used for applications and injected into permafrost methane or methane hydrate to evaporate and recover methane and to prevent seawater temperature from rising.

  The existing steam turbine does not use the combustion gas mass output at all, and also uses the combustion gas calorific power to generate rotational output with superheated steam whose atmospheric pressure weight is 1/23000 of mercury, and the work rate of unit blade area Since kg weight m / sec is close to 1/23000 of mercury, stationary blades are provided in multiple stages, weirs are blocked in multiple stages, the steam velocity is reduced, and the output is brought close to 1/200, so high temperature water 52b vaporization explosion With the use of speed, the heat consumption is reduced to 1/539 of the use of superheated steam, the high-temperature mercury 1d vaporization explosion speed is used, and the specific heat is 1/28 of water. The output of all rotor blades, which have completely abolished the stationary blades, is excluded from the calculation. * 28 = Approx. 340 million times high-temperature mercury 1d finish The 100% combustion gas pressure full-blade gas turbine drive is provided so that bearings, thrust bearings, and turbine blade groups that can be used safely even at high output can be assembled. Because it approaches 0 degrees, the use of cold heat 52e with a manufacturing cost of nearly 0 and recovery and use as combustion gas dissolved water 52g, the same fuel amount of CO2 exhaust 0, 200 times the power generation amount of existing steam turbines, etc. There is.

  In areas where water is scarce during the process of recovery and use as hot and cold water, the excess heat generated from the power generation is produced and sold to consumers as distilled water and salt using a seawater desalination unit, etc., and converted to high-temperature superheated steam using the theoretical best heat pump 1G. Heat the water in the consumer water tank, drive and use the heat pump 1G with the theoretically best rotation output, heating equipment for household use, commercial use, agricultural greenhouse heating, drinking water production equipment, washing Used in dryers, dishwashers, various types of cooking equipment, bathhouses, hot water pools, etc. Cooling heat is stored in a small size, such as square ice, mass-produced and stored at low temperatures, and equipped with a blower that can cool ice in urban areas. It is sold together with ice containers, and cold water after ice cooling is sold as drinking water, making the whole city a cooling cold summer city, reversing the heat island, supplying cold ethyl alcohol directly in the vicinity of the power plant, In hot water, it manufactures and sells refrigeration equipment, refrigeration equipment, ice making equipment, cooling equipment, etc. for household and commercial use. Combustion gas dissolved water is used for the production of cold and hot water, and CO2 etc. Supplying combustion gas-dissolved water with the components nitrogen and oxygen to the seabed to increase the food production of seaweeds and seafood, such as algae and phytoplankton required for the birth of 1 kilogram of fish There is a challenge to postpone human extinction.

  Since all existing engines are the worst and cannot be improved, they are not adopted and are divided into combustion gas calorie output + combustion gas mass explosive force, and all blade mercury turbine + all blade water turbine + all blade gas The turbine is driven, or all blade blade water turbine + all blade blade gas turbine is driven to cope with mercury shortage, and the whole blade combustion section 32X or the combined engine combustion section 31X is driven with high-temperature water to reduce the heat consumption by 1 / 539 theoretical best all-blade water turbine, atmospheric pressure, same speed, same calorific power, kg weight m / sec, 910,000 times, special high-temperature mercury drive, 340 million times power, in the process of injection propulsion Combustion gas mass explosive force + Combustion engine injection unit 79K or water jet 79M is driven by the superheated steam explosive force of combustion gas calorific value, and various water injection vessels, various water injection battle vessels and various air injection vessels , Various air-injected combat ships, various air-injected aircraft carriers, various air-injected airplanes, various air-injected combat airplanes, various space return aircraft, various air-injected flying ships, various vertically rising vertical descent airplanes, There is a challenge to drive most efficiently all kinds of vertical ascending vertical descent combat airplanes, various space return parent airplanes, various air transport mobile devices, various supersonic airplanes, and anything that can be driven by engines.

  In addition to the advanced technology improvements of existing gas compressors, the eight types of existing reciprocating engines and foreign patent reciprocating engines such as the United States have the greatest advantage when used exclusively for compression of air, etc. As the theoretical best heat pump 1G that is driven at the best theoretical rotation, the exhaust heat amount and the compressed air heat amount of mercury exhaust around 220 degrees are recovered, for example, 1/30 * 1/30 * 1/30 = 1/7000. Because it enables volumetric compressed air, 8 types of energy storage compressors 20X and existing compressors 20Y are fully used for various applications, and high pressure compression high pressure combustion heat exchange cooling combustion and exhaust heat quantity are collected to the limit. Utilize, for example, a mercury explosion force of 430 to 800 degrees saturation pressure or higher + a water explosion force of 374 degrees saturation pressure or more + a water explosion power of about 40 to 24 degrees Celsius and a mass explosion force of 24 to 400 MPa. Hot mercury 1d + mercury injection pump 6Z accelerates the mercury velocity in the vertical downward vacuum direction, facilitates high-pressure injection of 400MPa, etc., and adds gravity acceleration of 9.8m / second in vacuum, high temperature water 52b + water injection pump In the same way, the acceleration of water by 6z and the acceleration of gravity are added, and there is a problem of 200 times rotation output by 1 / 1.700 million heat quantity mercury injection and 1/4000 heat quantity water injection at the same speed as superheated steam.

  Air extraction Vacuum rise around 220 degrees Mercury saturation temperature The most important thing in the recovery process of exhaust heat is not to extract vaporized mercury with air. Therefore, the partition wall 11A is provided at a sufficient height to separate the mercury chamber 11B and the air chamber 11C, and the mercury chamber 11B is sufficiently cooled to eliminate, for example, 150 ° C. or less of the cooled vaporized mercury and communicate with the air chamber 11C. The vacuum is raised by 51, the exhaust heat is recovered by the intake air, the compression heat is recovered, the high pressure compression high pressure combustion heat exchange cooling combustion is performed, and the exhaust heat is recovered to the limit as the theoretical best rotational output + theoretical best heat pump 1G. The engine is divided into combustion gas calorie output + combustion gas mass output, and rotation output is generated in all. In injection propulsion, the rotation output combustion unit is driven by combustion gas calorie output, and the combined engine is obtained by combustion gas calorie output + combustion gas mass output. Drives the injection unit 79K or the water jet 79M to generate the most efficient rotation output and injection propulsion output, the same fuel amount 200 times mercury rotation output of the existing engine Is in the water rotation output, as well as 10-fold injection propulsion output, there is a challenge to completely eliminate the pollution of response and mercury to mercury shortage.

  Thermal power plants and nuclear power plants in the existing world have raised the seawater surface temperature by 7 degrees Celsius with the total amount of heat generated, increasing the danger of human extinction. The intake air 28a recovers the amount of heat of compressed air 28b around 200 degrees, and the expanded piston 21 compresses the theoretical best heat pump 1G to a configuration of 600 to 1000 degrees or more once, so that the energy storage compressor 20X or the existing compressor 20Y is Theoretical best heat pump 1G, high pressure compression, water heat exchanger 2Y heat recovery final air cooling process, high pressure combustion heat exchange cooling heat recovery without limit to fuel injection combustion, 374 degrees 24MPa high temperature water explosive force + around 40 degrees 24 to 400 MPa Combustion gas 49 Divided and used for explosive force, high-temperature water 52b is most efficiently injected and accelerated by water injection pump 6z at 400 MPa, etc. 1/539 of hot steam is used to drive all rotor blade water turbines, the atmospheric pressure, the same speed, and the same calorific power are 1700 * 539 times that of superheated steam = approximately 910,000 times that of superheated steam, 1/4000 heat water of superheated steam Aiming for 200 times rotation output by injection, in the process of exhausting, cooling 52e cooling will delay the extinction of mankind as seawater temperature rises 0, aiming at maximum vacuum and gravitational acceleration at exhaust saturation temperature around 25 degrees, dedicated for rotation output for power generation, etc. Then, the excess supply heat equivalent is effectively used with superheated steam temperature 52d etc. of 400 degrees.

  Driven by a pressure approaching 100 to 1000 times that of existing gas turbines, the cold turbine 52e maximum recovery amount and maximum rotational output can be driven by the explosion and combustion power of around 40-degree 24-400MPa combustion gas 49 divided and stored. The combustion gas exhaust temperature is brought close to -273 degrees to achieve the maximum cold recovery power generation, and the cold heat is made into a mass production storage low temperature with ice cold heat 52e such as a square, and a blower is provided that can cool an urban area etc. with ice. Selling with ice containers, processing and selling cold water after cooling into drinking water, cooling the urban area as a cool summer city, reversing the heat island, dissolving the combustion gas after cold recovery into water and dissolving the combustion gas Supplying combustion gas dissolved water such as oxygen, nitrogen and CO2 to the sea as water, seaweeds, corals, etc. are proliferated, fishes are proliferated through the food chain, and the same fuel amount of existing steam turbine 200 Use heat, electricity, and cold supply equipment for power generation, and use the heat pump 1G + water heat exchanger 2Y to generate high-pressure and high-temperature superheated steam to heat the water in the consumer water tank. It can be used as a storage battery, and almost all automobiles and rotating output drive devices are driven by storage batteries to prevent global warming by cooling CO2 exhaust and seawater.

  The existing jet aircraft is a spacecraft, and is divided and used as high-temperature mercury 1d explosive force + combustion gas 49 explosive force, and the mercury injection pump 6Z facilitates high-temperature mercury 1d injection pressure 400MPa, and gravity acceleration 9 in a substantially vertical downward vacuum direction. .8m / second / second of injection acceleration, atmospheric pressure, same speed, same calorific power, kg weight m / second, 910,000 times * 13.5 * 28 = approx. The mercury turbine is driven by rolling contact with mercury with the maximum surface tension, and the exhaust saturation temperature is about 220 degrees of heat and the compressed air heat amount 28b is recovered and compressed with the intake air 28a, about 300 degrees is compressed 800 to 1000 degrees, and the mercury 1d temperature is set. The pressure is set to 430 to 800 degrees, and the mercury jet pump 6Z is jetted in the vertical downward vacuum direction at 400 MPa or the like. The steam turbine has a 200-fold rotational output, and in the course of injection propulsion, the injection pressure of the combustion gas 49 and superheated steam 50 approaches 1000 times that of existing jets, and approaches 10 times or more the speed of jet propulsion and the speed of light. Make the trip prime.

  The mercury turbine is driven by the high-temperature mercury 1d explosive force, the mercury saturation exhaust temperature is set to around 220 ° C., a partition wall 11A is provided at a sufficient height to isolate the mercury chamber 11B and the air chamber 11C, 11B is sufficiently cooled, for example, 150 to 100 degrees Celsius or the like, no mercury vaporized and no mercury pollution, and the vacuum is raised by the air extractor 51 connected to the air chamber 11C to increase the amount of compressed air and heat recovered, Combustion gas with a large amount of remaining oxygen is increased. Mercury + water is heated with compressed air 28a or combustion gas 49 of the water heat exchanger 2Y to form high-temperature mercury 1d + superheated steam. 95c, the superheated steam on the outer periphery of the fuel injection combustion is injected into the 24-400MPa combustion gas of the combustor 1Y, respectively, and approaches the theoretical air-fuel ratio combustion, aiming at injection propulsion output more than 10 times that of existing jet aircraft And then, in a vacuum will increase significantly and the infinite acceleration aim. Ships are driven by resource-rich all-blade water turbines, and the jet propulsion speed is made close to the speed of sound, and CO2 exhaust is supplied together with nitrogen and oxygen in seawater to prevent fish growth and global warming.

  CO2 exhaust 0, seawater temperature rise 0 pollution is zero, the same amount of fuel is generated 200 times that of the existing steam turbine, 400MPa injection is facilitated by pump injection, and gravity acceleration is 9.8m / second per second in the vertical downward vacuum direction With the added acceleration, the atmospheric pressure, the same speed, and the same caloric power are set to 340 million times the total blade mercury turbine and 910,000 times the full blade water turbine of the existing turbine. Turbine rotation output is generated, and 1/17 million heat quantity mercury injection and 1/4000 heat quantity water injection at the same speed as superheated steam, and full blade mercury turbine and all blade water turbine with 200 times rotation output of existing steam turbine The same fuel injection propulsion output is also close to the 1000 times pressure injection of the existing technology, and it has the effect of being able to aim at 10 times speed or more, and it is the world's highest profit rate and prevents global warming Effect is also available.

  Acceleration with gravitational acceleration in a vacuum, and the output of all rotor blades, which completely abolished the worst blades of existing technology, were excluded from the calculation. As a mercury turbine or 910,000-times full rotor blade water turbine, the corresponding bearings, thrust bearings, turbine blades, etc. are assembled with special strengths that can be used safely. Drive all-blade mercury turbines and all-blade water turbines, and aim for 200 times rotation output of existing technology with the same maximum fuel output and the same fuel amount 10 times injection propulsion output, generators and vehicles As well as driving ships and airplanes, it has outstanding effects as a global warming prevention technology and military technology.

  In order to drive the entire rotor blade gas turbine having the optimum turbine blade cross section 40X by the explosive force of the 100 times pressure combustion gas 49 of the existing gas turbine, the heat, electricity and cold supply facilities are driven most efficiently, and the ice cold heat 52e The city is ice-cooled with the maximum recovery amount of heat, the heat island is turned into a cold summer city, and the remaining CO2 is dissolved in water as combustion gas-dissolved water 52 g and supplied to the seabed to provide seagrasses and phytoplanktons It increases the production of fish and human food through the food chain, and has the effect of maximizing seawater cooling, preventing global warming and preventing human extinction.

  A full-blade mercury turbine and a full-blade water turbine or a full-blade water turbine are driven as a turbine blade cross section 40X that is optimal for a full-blade turbine, and the combustion power is converted to a combustion gas 49 explosive force of about 24 to 400 MPa combustion gas around 40 degrees. Combined engine that sucks and injects forward air and vacuum by using the maximum fuel combustion amount of the existing gas turbine as 1000 times injection pressure combustion gas 49 injection, the superheated steam 50 in the outer superheated steam reservoir 95c is heated 1000 times pressure superheated steam injection As the jet part 79K, aiming at 10 times the injection propulsion speed of the existing technology and infinite acceleration by flying in vacuum, it is excellent as military technology and space technology to drive and propel ships, airplanes and spacecrafts. There is an effect.

  A full-blade mercury turbine and a full-blade water turbine or a full-blade water turbine are driven as a turbine blade cross section 40X that is optimal for a full-blade turbine, and the combustion power is converted to a combustion gas 49 explosive force of about 40-degree 24-400 MPa combustion gas 49 Supply fuel combustion amount 1000 times injection pressure combustion gas 49 injection of the existing gas turbine, superheated steam 50 of the peripheral superheated steam reservoir 95c is heated 1000 times pressure superheated steam injection, water jet 79M that sucks and injects water in front In order to proliferate phytoplankton as CO2 exhaust gas 0 by driving ships aiming at 10 times the injection propulsion speed of existing technology, dissolving combustion gas in superheated steam and further dissolving in seawater in the process of injection propulsion. It has the effect of preventing global warming and preventing the extinction of mankind, and has an outstanding effect as military technology.

  The heat pump 1G, which recovers the exhaust gas saturation temperature around 220 degrees, the combustion gas 49 heat quantity and the compressed air heat quantity 28b, is driven by the theoretical best rotational output and used for the recovery of compressed heat. It has the effect of making the maximum output 200 times the rotation output, and for power generation and other dedicated rotation outputs, heat exchange is performed for the amount of excess heat that is supplied, and the water in the consumer water tank is recovered with high-temperature superheated steam temperature 52d. It has the effect of maximizing the creation of various markets for the use of thermal energy, such as vaporizing and recovering methane hydrate with 52d of thermal energy with a manufacturing cost of approximately 0, using it in various heating and heating equipment for home and business use, etc. It also has the effect of reducing the worst seawater temperature rise of existing power generation to zero.

  Infinitely high-pressure combustion heat exchange cooling combustion, divided into maximum pressure combustion gas calorific value explosive force + maximum pressure low-temperature combustion gas mass explosive force, so it is highly efficient and uses only a small amount of fuel. In addition to being able to operate for a short time, low-temperature combustion gas that can burn a large amount of fuel with a large amount of remaining air 49 mass explosive force + superheated steam 50 injection and zero fuel combustion amount in a vacuum, etc. are very safe There is an effect that can be made into convenient airplanes and space shuttles.

  Embodiments and examples of the invention will be described with reference to the drawings, but the same names or reference numerals are given to the same parts as those of the embodiments and examples and the description above, and duplicate description will be omitted. Omitted as much as possible, and the characteristic parts and the lack of explanation will be added and explained sequentially. The idea is explained with hypothetical numbers for the very difficult brain invention best engine invention and to explain the intention and expectation concretely clearly, but the correct answer is the hypothetical number of the theoretical best engine as an experimental number. It is not limited to. The idea that seems to be the best is duplicated in many applications, the idea is selected and used according to the application, and the claims are changed to be used according to the various applications.

  The combined engine combustion section 31A in the front explanatory view of FIG. 1 and the all-blade propeller turbine in FIGS. 1 to 6 store energy from the eight types of energy storage compressors 20X and the existing compressor 20Y, with the existing gasoline engine dedicated to compression. For example, 1/30 * 1/30 * 1/30 = 1 by using the compressor 20A, making the piston top gap close to 0, and using multiple cylinders as one or more preload compressors to main pressure compressors. / Compressed with 27000 volume compressed air, etc., with energy storage compressor 20X or existing compressor 20Y, infinitely high pressure combustion heat exchange cooling combustion, divided and stored into combustion gas calorific value explosive force + combustion gas mass explosive force The high-temperature water explosive force + water injection pump 6z injection 374 degrees 400MPa, etc., to facilitate easy pressure injection, reduce heat consumption to 1/539 of using superheated steam, drive all blade impeller water turbine 8b and exhaust In the process, the temperature of seawater rises to 0 by cooling the alcohol cooler 52e by the cooler 2A, the exhaust temperature of the water 52a is about 25 degrees, and the air extractor 51 is set to a higher vacuum than the existing steam turbine, and the gravitational acceleration in the vacuum is 9.8 m / sec. The maximum addition of every second and the large output of all the moving blades with the abolished blades excluded from the calculation, the atmospheric pressure, the same speed and the same calorific power, kg weight m / second, 1700 times the existing superheated steam use * 539 = approx. Increase to 910,000 times.

  The compressed heat recovery unit 2C increases the intake air 28a temperature to around 200 degrees with the compressed air heat quantity 28b including the combustion gas 49 heat quantity, and the compressed air 28a temperature such as 600 to 1000 degrees with the expanded piston 21 Each time the compressor 2Y compresses at least once, the water 52a is subjected to heat exchange heating around 200 degrees, the compressed air 28a is cooled, and the high temperature water 52b such as 374 degrees 24 MPa is supplied to the high temperature water reservoir 95 such as a cylindrical length. A large number of water injection pumps 6z selected from various existing pumps can be easily and pressure-injected from 24MPa or the like to 400MPa, etc., and expanded and uniformly expanded in the turbine axial direction by a large number of nozzle injection parts 6b. As a configuration that acts evenly on the turbine blade 8c, the rotational output of the all-blade spring vehicle water turbine 8b is generated and selected from the turbine blade cross section 4A4B4C4D4E4F. Then, the turbine blades 8c having the turbine blade cross section 4X are provided in parallel in the axial direction, the turbine blades 8c generating the rotation output are reduced to about 1/10, the cooling amount of the heating high temperature means 3B is reduced, the rolling contact is optimized, and the injection propulsion is performed. Then, as superheated steam 50 + combustion gas 49, we aim at 400MPa injection propulsion output, respectively, and aim at 1000 times injection pressure 10 times speed of existing technology.

  For power generation, the amount corresponding to the amount of heat supplied is recovered by the high-temperature superheated steam temperature 52d by the heat pump 1G, heating the water in the consumer water tank, setting the worst seawater temperature rise of the existing power generation to 0, and using various heating equipment and various cooking equipment using heat Manufactures and sells equipment, various hot water equipment, various dishwashers, various washing dryers, various water heating and piping buildings, etc., and heats seawater with superheated steam heat 52d in each region to produce vacuum vaporized distilled water, distilled water and salt In order to eliminate serious water shortage areas, in the danger zone of methane hydrate decomposition, various enclosures such as a conical roof type are made with vinyl sheets etc., and heat, electricity and cold supply facilities are installed on ships and land In the process of recovering surplus heat with superheated steam temperature 52d, adding pipes insulated to the existing technology to vaporize and recover injected methane into methane hydrate and use it as fuel 2 is similar to the exhaust of the all blade impeller gas turbine 8a, which is close to 0 degrees in FIG. 2, and is stored in liquid by the multistage compression heat recovery cooling by the energy storage compressor 20X or the existing compressor 20Y, and is stored on land with electricity. Shipping and selling, supplying 52g of CO2 and other combustion gas dissolved water to the seabed Propagating seaweeds and phytoplankton, feeding fish in the food chain, reducing the risk of fish extinction and human extinction due to decomposition of methane hydrate To do.

  2 is provided with side plates 8d at both ends of the cylindrical body 8e and the turbine blade 8c, and the turbine blade 8c can be meshed in the opposed series shown in FIG. A side plate 8d is provided, and the high temperature water 52b is configured to generate a rotational output of the turbine blade 8c by accelerating using the theory that vaporization explosion concentrates in the low pressure portion at the rear of the injection direction. 4 is installed in multiple stages in the opposite series and vertical, or FIG. 6 is provided with an outer box vertical section 94A to add all the moving blade impeller water turbines 8b in multiple stages in series and vertical and completely eliminate the blades. A turbine blade turbine 8b is configured, and the turbine blade 8c is provided with a heating high temperature means 3B and a water repellent action 3A so as to generate a rotating output of the rolling contact, aiming at an exhaust saturation temperature of about 25 degrees in the exhaust process. Alcohol cooling of the cold cooler 2A As the cooling of 52e, the gravity acceleration is set to the maximum rotation output with the maximum vacuum, the cooled water 52a is heated by the hydrothermal exchanger 2Y, 374 degrees 24MPa, etc. With a mass explosive force, the atmospheric pressure, the same speed, and the same calorific power are about 910,000 times that of superheated steam, and the corresponding bearing 80 and thrust bearing 80a are provided.

  The all blade impeller gas turbine 8a in FIG. 1 side view of FIG. 2 selects the turbine blade cross section 4A4B4C4D4E4F from 4X, and has the blade shape that generates the rotational output most efficiently by providing the turbine blade 8c in parallel in the axial direction. The side plate 8d is provided at both ends of the cylindrical body 8e and the turbine blade 8c so as to be able to mesh with each other in the opposite series in FIG. 4, and in the vertical series in FIG. 6, the outer casing vertical portion 94A + the side plate 8d is provided. In the driving process, the combustion gas 49 having a temperature of about 40 to 24 to 400 MPa or the like is supplied to the cylindrical combustion gas reservoir 95a, and a plurality of combustion gas control valves 24 are provided. The combustion gas 49 is supplied to the open control combustor 1Y, and the combustion gas 49 is injected as it is from the combustion gas rocket nozzle 6M to maximize the amount of collected cold energy. During the injection process, the fuel control valve 2 b and the fuel injection valve 7 are opened, the fuel injection combustion amount is maximized in the combustor 1Y, the rotation output is maximized, the combustion gas 49 injection pressure is set to about 100 times that of the existing gas turbine, and the rotation output is set to about 10 times. , Superheated steam explosive force is added. Aiming at injection propulsion speed of 10 times or more at pressures around 1000 times each, corresponding bearing 80 and thrust bearing 80a are provided.

  In the process of generating the rotational output of the all-wheel impeller gas turbine 8a, the combustion gas 49 around 40 degrees around 24 to 400 MPa is injected from the combustion gas rocket nozzle 6M and expanded in the axial direction by the nozzle injection portion 6a, and becomes the turbine blade 8c. The turbine blade 8c is provided with a cold heat recovery means 3C to collect cold heat with alcohol 1C or the like to prevent sticking of dry ice, moisture, etc., and to increase the combustion gas volume to collect cold heat. The rotational output is increased by the combustion gas 49 approaching the exhaust temperature -273 degrees by increasing the amount and rotational output, and CO2 and SO2 etc. are separated and recovered as solids and liquids by the melting point difference etc. during the exhaust process, Alcohol cold heat 52e etc. is made by external cold heat recovery devices 103, 103, and ice is produced by alcohol cold heat 52e in the vicinity of the power plant, and mass production is made with ice of a certain size such as squares. Chilled, sold to urban areas, etc. with ice containers equipped with a blower that can cool ice, and sold cold water after ice cooling as drinking water. Manufactures and drives refrigeration equipment, refrigeration equipment, cooling equipment, etc. for household and commercial use, and supplies 52g of combustion gas-dissolved water after cold recovery to the seabed to grow seagrasses and phytoplankton And greatly increase seafood in the food chain.

  Referring to FIG. 3, the full-blade flywheel mercury turbine 8E8E will be described. The exhaust saturation temperature around 220 degrees is collected by the intake air 28a and compressed by the selected energy storage compressor 20A, and the mercury is set to a temperature of 500 to 1000 degrees compressed air 28a. The heat pump 1G that heats 1d and the water 52a, cools the air to around 300 degrees and recovers the compression heat more than once constitutes the heat pump 1G, and the final reduced diameter compression chamber mercury heat exchanger 2Z + water heat exchanger Fuel injection combustion in the process of heat exchange air cooling at 2Y, unlimited high pressure combustion heat exchange cooling combustion, divided into high pressure mercury such as 430 to 800 degrees, high pressure water such as 1374 degrees, high pressure combustion gas explosive power around 40 degrees In the process of preserving and driving the all-wheel impeller mercury turbine 8E, the mercury injection pump 6Z facilitates injection of 400 MPa and the like, and the vaporization explosion at the rear of the high-temperature mercury 1d traveling direction As the acceleration with the theoretical best acceleration in the vacuum direction directly below and the acceleration of gravity added in the vacuum, the large output of the blades was completely abolished and all blades were excluded from the calculation. Increase m / sec to 910,000 times * 13.5 * 28 = about 340 million times that of superheated steam, and 200 times rotation output with the same speed 1 / 1.7 million heat quantity mercury injection.

  Synchronize all blade impeller mercury turbine 8E8E with magnetic friction synchronizer 55, etc., and mesh and add vertically in multiple stages as shown in FIG. 4, or vertically provide outer box vertical portion 94A as shown in FIG. In order to maximize the use of gravitational acceleration of 9.8m / sec per second, the rotation output is generated in the process of rotating output, and the rotating output is generated with the minimum friction loss due to the rolling contact of high-temperature mercury 1d. Thus, the theoretical best maximum rotation output by mercury 1d having the maximum surface tension is provided, and the partition 11A is provided at a sufficient height in FIG. Cool to 100 degrees, for example, raise the vacuum by the air extractor 51 to eliminate any extracted vaporized mercury in the external air chamber 1A, and exhaust heat at a mercury exhaust temperature of around 220 degrees by the vaporized hot air recovery unit 2B. 5A is recovered by the intake air 28a, the intake air temperature is set to a maximum vacuum such as 60 to 100 degrees, the compressed air heat amount 28b or the combustion gas 49 heat amount is further recovered 200 degrees or more depending on the application, and the energy storage compressor 20X or Compressed multiple times with the existing compressor 20Y, the compressed air 28a temperature is set to 500-1000 degrees, etc. multiple times.

  As high-temperature mercury 1d compressed to a saturation pressure or higher by the mercury pump 1E, the high-temperature mercury 1d + water 52a is heated by the reduced-diameter compression chamber mercury heat exchanger 2Z compressed air 28a, and the compressed air 28a is cooled several times to 200 to 300 degrees. In the process of cooling the final compressed air, the mercury temperature is increased to 430 to 800 ° C. in the fuel injection combustion heat exchange and divided and used for combustion gas calorie output + combustion gas mass output. The vacuum is raised by the above, the injection of 400 MPa or the like is made very easy by the mercury injection pump 6Z, the uniform injection is expanded in the axial direction by the mercury injection nozzle 6b, the all-blade impeller mercury turbine 8E is driven, and the high temperature mercury 1d By setting the exhaust saturation temperature of the engine to a high vacuum of around 220 degrees, the vaporization explosive force is maximized, the rotational output is the maximum theoretical best engine, and it is connected to the horizontal crankshaft 16 etc. By Use in applications where the energy saving compressors 20A20X or existing compressor 20Y to the theoretical best thermal pump 1G, resources requires the most compact and lightweight high output and little mercury.

  The opposed series full blade impeller turbine 8K shown in FIG. 4 is provided with multiple turbines such as a full bucket impeller water turbine 8b8b opposed to each other in multiple stages perpendicular to the opposite series as shown in FIG. A gravitational acceleration of 9.8 m / sec / sec is efficiently utilized, and the turbine blade 8c and the measuring plate 8d of the selected turbine blade cross section 4X are provided with the all-wheel impeller turbine 8K in the outer box 77a at an optimum interval, A plurality of turbine blades 8c8c are arranged in the direction of the outer peripheral axis of each cylindrical body 8e8e by synchronizing with the magnetic friction synchronization devices 55, 55, etc. In the radial direction, the power generation turbine blades 8c are expanded and expanded in accordance with the application output, and the power generation turbine blades 8c are heated to about 1/10, and the heating reduction rolling contact of the high-temperature blade spring turbine water turbine 8b heating high temperature means 3B is made best. The atmospheric pressure, the same speed, and the same calorific power are 910,000 times that of using superheated steam, and experiments are necessary. The water turbine 8b8b is driven.

  In the process of generating rotational output, the pressure is increased to 24 MPa or the like by the water pump 1F, and the water is supplied to the hydrothermal exchanger 2Y to be 374 degree high-temperature water 52b. 8b8b is driven, the exhaust is cooled by alcohol cold heat 52e of the cold cooler 2A, etc., the saturated water temperature is 25 degrees or less, the vacuum maximum is stabilized, the gravitational acceleration additional maximum is stabilized, and the turbine blade 8c is most powerful. , Driving out the worst seawater temperature rise of existing power generation technology, preventing heavy rain wind speed 10 times increase due to abnormal weather, extracting air with air extractor 51, enabling maximum vacuum gravity acceleration maximum rotation output maximum Aiming at 200 times rotation output and heat, electricity and cold supply facilities of existing technology, various ships, airplanes, automobiles, and various rotation output drive devices, and heat and electricity during stoppage And used as a cold heat of the supply facilities, the existing rise of technology seawater temperature and CO2 emissions to 0, and then put off the human race extinction due to the rise, abnormal weather and food depleted sea surface temperature of 7 degrees by the existing power generation technology.

  5 is an all-blade propeller turbine mercury turbine 8E all-blade propeller vehicle water turbine 8b all-blade propeller vehicle gas turbine 8a vertically in multiple stages, respectively. It is possible to add a large output and efficiently add gravity acceleration in a vacuum, and the atmospheric pressure, the same speed, the same calorific power, kg weight m / second, 34,000,000 times all-wheel blade impeller mercury turbine 8E using superheated steam and large 910,000 times full blade impeller water turbine 8b using superheated steam at the same pressure and speed, and 100% pressure combustion gas injection full rotor blade gas turbine drive of existing gas turbine, 1000 times pressure combustion gas + superheat Steam is used as a combined engine injection unit 79K injection airplane drive, etc., and a bearing 80 and a thrust bearing 80a are provided according to the respective characteristics so that safe operation can be performed with high output, and each of them can be directly or existing transmission 55Y Shifted by the air friction transmission 55B and connected by the joint 80A, the left and right rotary shafts are connected to the output shaft, the generator shaft, the energy storage compressor 20X, etc., respectively, and the combined engine combustion unit 31X is driven to output rotational output and Generates jet propulsion output.

  In the process of generating rotational output, the rotational output is generated with a combustion gas explosive force of around 40 to 24 MPa, and the maximum rotational output is 100 times the pressure of the existing technology. In the exhaust process, aiming at the turbine 8a, the exhaust saturated combustion gas 49 temperature approaches -273 degrees in FIG. 2, FIG. 5 recovers cold energy by the cold heat recovery device 103 to produce alcohol cold heat 52e, and gas combustion by the upper gas extractor 51a The gas 49 is extracted to the external cold recovery unit 103, and the liquid or solid combustion gas 49 is selected and supplied to the external cold recovery unit 103 from the lower gas extractor 51a to recover the cold and generate an injection propulsion output. In this process, the whole moving blade propeller mercury turbine 8E and the whole moving blade propeller water turbine 8b are driven by a part of the combustion gas calorie output, and all of the combustion gas mass output + combustion gas heat. The remaining output is combustion gas 49 + superheated steam 50. Combustion gas 49 explosive power + superheated steam explosive power aiming 1000 times the pressure of existing jets is injected from the combined engine injection part 79K, and 10 times the speed of the existing jets. Etc.

  The series full blade impeller turbine 8L in FIG. 6 is a multistage arrangement of the full blade impeller mercury turbine 8E, the full blade impeller water turbine 8b, and the full bucket impeller gas turbine 8a in FIG. The turbine blade 8c and the side plate 8d are provided in the outer casing 77a of the all-blade pusher wheel turbine 8L at an optimum interval, for example, in order to efficiently use the gravitational acceleration of 9.8 m / second per second in a vacuum. At the same time, the turbine blades 8c having the turbine blade cross section 4X are arranged in multiple stages at an intensity size interval close to the outer box vertical portion 94A and matched to the injection mass, and matched to the application output in the direction of the outer peripheral axis of each cylindrical body 8e. Extending and expanding in the radial direction, the cross section is increased in proportion to the output in the radial direction, and there are multiple stages with the distance between the paragraphs exceeding the turbine outer diameter to maximize the addition of gravitational acceleration in a vacuum. In the all-wheel impeller gas turbine 8a, the combustion gas 49 injection pressure will be close to 100 times that of the existing gas turbine, aiming for 10 times the rotational output.

  In the process of driving the most efficient all-blade flywheel mercury turbine 8E, an experiment is necessary, but high-pressure high-temperature mercury such as 430 to 800 degrees 400 MPa, aiming for a 200-fold rotation output with 11.7 million calorific mercury injection of superheated steam. Using the 1d vaporization explosive force, the heat consumption of the same volume is reduced to 1/2 of the water, and the high output of all the moving blades that completely abolished the worst turbine blades of existing turbines was excluded from the calculation. The same calorific power, kg weight m / sec, is 910,000 times that of using superheated steam * 13.5 * 28 = about 34,000,000 times, and the all-wheel impeller mercury turbine 8E is driven in rolling contact to produce the theoretical best engine. Construct, aiming for 200 times rotation output of existing engine with the same speed 1 / 1.7 million calorie mercury injection, recovering mercury exhaust calorie with intake air 28a of vaporized hot air recovery device 2B in the exhaust process, mercury exhaust saturation temperature 220 degrees ago Is cooled to around 100 degrees, vaporized mercury is totally free of mercury pollution, intake air 28a temperature is set to 60 to 100 degrees, etc., air is extracted into the external air chamber 1A by the air extractor 51, and no mercury pollution is confirmed. Set the maximum rotation output to maximum.

  FIG. 7 shows an embodiment of the all blade combustor 32E and the vertical all blade water turbine 8B, except for the turbine, which is substantially the same as the above, with the energy storage compressor 20D directly driven by the crankshaft being opposed to the crankshaft. And the entire blade combustion section 32E that constitutes the energy storage compressor 20E is used, and the vibration is canceled out by the opposing reciprocating motion synchronization by the magnetic friction synchronizers 55, 55, etc., so that the water heat exchanger 2Y is respectively left and right and in the center. One or more cylinders other than the final stage are used as the pre-pressure hydrothermal exchanger 2Y to cancel the vibration, thereby enabling a large diameter of the double-headed enlarged piston 21 diameter. It is possible to drive in parallel, bend 90 degrees with a known gear joint, enable horizontal crankshafts 16 and 16, and have large diameter compression chambers 10a and 10a opposite to each other with simple structure to the limit. The pre-compression compression to final final compression is performed by the expanded diameter compression chamber 10a as the firing portion 32E, and the high-pressure combustion heat exchange cooling combustion is performed without limitation in the water heat exchanger 2Y, and high temperature water 52b such as 374 degrees 24 MPa vaporization explosive force +40 24 to 400 MPa combustion gas before and after the temperature is divided and used for 49 mass explosive force, and the vertical moving blade water turbine 8B is driven by high-temperature water 52b vaporizing explosive force such as 400 MPa of the water injection pump 6z, and the full blade combusting section 32E. Is driven by rotational force.

  Air in which a heat heat exchanger 2Y is provided on the left and right and in the center, and a pre-pressure water heat exchanger 2Y other than the final compression is used as the precompressed water heat exchanger 2Y. 28a is suction-compressed, finally compressed, and hot air 28a is supplied to the water heat exchanger 2Y. In the process of heat exchange cooling, the fuel injection ignition combustion is used as the all blade combustion part 32E. And the water heat exchanger 2Y is provided in the left and right final compression stages, the central final compression stage is the pre-pressure water heat exchanger 2Y, and the cooled air 28a is supplied to the left and right water heat exchangers 2Y, respectively. The whole blade combustion part 32F is the one that stirs air and injects and burns fuel. The final water heat exchanger 2Y is provided in the central final compression stage, the left and right final compression stages are pre-pressurized water heat exchangers 2Y, and cooled air 28a is supplied to the central water heat exchanger 2Y. The whole blade combustion part 32G is the one that stirs air and injects and burns fuel. Then, all the blade combustion parts 32A to 32H, which are selected and adopted, are combined into the whole blade combustion part 32X, which injects combustion gas mass explosive force + superheated steam 50 explosive force and sucks and injects forward air etc. As the engine injection part 79K, the water jet 79M is the one that sucks and injects water forward.

  The vertical all-blade water turbine 8B in FIG. 7 has an optimum interval between the inner blade group 60C of the inner shaft device 60A and the outer blade group 60D of the outer shaft device 60B, aiming for a small, simple and large output in the outer box 77a. The gravitational acceleration of 9.8 m / second per second is efficiently used in a vacuum, and the vertical all-blade water turbine 8B is driven by the high-temperature water 52b to reduce the amount of heat consumed by using superheated steam. The power output of all rotor blades, which have been abolished with the worst turbine blades of existing turbines, was excluded from the calculation, and the atmospheric pressure, the same speed, and the same calorific power were made 910,000 times that of using superheated steam, and the work rate was 910,000 times * 1/4000 calorie water injection = about 200 times rotation output, which can be used safely. The turbine blades 8c of the turbine blade cross section 4X are annularly arranged in each row at intervals of strength and magnitude according to the injection mass, and the inner shaft The device 60A and the outer shaft device 60B are integrally cast in an annular shape. The inner shaft device 60A and the outer shaft device 60B that rotate in the opposite directions by bolting the annular blade group are constructed, and the inner shaft device 60A, the outer shaft device 60B, and the outer box 77a are greatly reduced. A powerful bearing 80 and thrust bearing 80a are provided.

  Inner rotor blade group 60C and outer rotor blades rotating in opposite directions using high pressure combustion heat exchange cooling combustion without limitation in all rotor blade combustion section 32X, divided and used for combustion gas calorie explosive force + combustion gas mass explosive force The group 60D is driven strongly, the atmospheric pressure, the same speed, and the same caloric power are set to 910,000 times the existing technology, and the gravitational acceleration of the maximum acceleration in human history is added. Aiming at 200 times the rotational output of the technology, the vertical rotor blade water turbine 8B is driven most efficiently, and in the exhaust process, the hot water 52b exhaust is cooled by the alcohol cold heat 52e of the cold cooler 2A, etc. The air is extracted by 51, the maximum vacuum is the maximum output, the exhaust saturation temperature is around 25 degrees, etc., the hot water 52b is drained at a low temperature around 20 degrees, and the combustion gas 49 mass explosive power is made possible, Wing spring wheel The structure of the turbine and compact simple lightweight, others entirely above substantially similarly to improve the existing steam turbine power generation worst, to prevent global warming by inhibiting the human extinction as water temperatures rise 0CO2 exhaust 0 power.

  FIG. 8 shows an embodiment of a vertical all-blade gas turbine 8A that selectively uses the full-blade combustion section 32D. The full-blade combustion section 32D that selectively uses the energy storage compressor 20D in which the piston is directly driven to rotate by the crankshaft. Using a vertical all-blade water turbine 8B and a vertical all-blade gas turbine 8A to cope with mercury shortage, the hydrothermal exchanger 2Y has a 24-400 MPa combustion gas 49 explosive force around 40 degrees after heat exchange cooling, and a rotational output At maximum, the combustion gas control valve 24 is opened, the low-temperature combustion gas 49 is supplied to the annular combustion gas reservoir 95d many combustors 1Y, and the many fuel control valves 25b fuel injection valves 7 are opened and fuel injected, The maximum amount of fuel is combusted and the maximum pressure is injected from the combustion gas rocket nozzle 6M to maximize the rotational output of the vertical all-blade gas turbine 8A and reduce the amount of cold recovery. Various cold district heat, electricity and cold Offering The rotation output will occur such as equipment and various types of automobile class and various airplane acids and various ship class.

  The maximum amount of cold recovery is 24 to 400 MPa combustion gas 49 around 40 degrees, the combustion gas control valve 24 of the annular combustion gas reservoir 95d is opened, the low temperature combustion gas 49 is supplied to the combustor 1Y, and the combustion gas The maximum pressure and the minimum temperature are injected from the rocket nozzle 6M to drive the vertical all-blade gas turbine 8A to maximize the amount of cold recovery, and the turbine blade 8c is provided with a cold heat recovery means 3C and heated with dry ice with alcohol 1C or the like Preventing the sticking of water and water, recovering the cold, increasing the temperature rise volume of the combustion gas 49, maximizing the amount of cold recovery, driving the gas exhaust chamber 5c with the gas extractor 51a, Heat exchange with alcohol and compressed air is performed in the cold heat recovery devices 103 and 103 provided outside, the alcohol cold heat 52e and the compressed air cold heat 52e are close to -100 degrees and -210 degrees, and the ice cold heat 52e is Mass-produced and stored at low temperatures possible and sold in the tropics. Manufactured and operated various types of commercial and household refrigeration 52e drive equipment. Stored and used methane in cooled recovery liquid and gas at methane recovery facility. Combustion gas such as CO2 is sold and used for various purposes after cooling and cold recovery.

  FIG. 9 shows an embodiment of the full blade combustion part 32D and the vertical all blade mercury turbine 8H. The inner shaft device 60A and the outer shaft device 60B of the vertical blade dynamic turbine 8H are shown in FIG. As in the case of all rotor blade turbines, integrally cast and integrally processed bolts are connected in a ring-by-row manner to form an inner shaft device 60A and an outer shaft device 60B that rotate in opposite directions, and the mercury control valve 25d is controlled to be open to control the mercury reservoir 95D. The high-pressure high-temperature mercury 1d is jetted in the vertical downward vacuum direction by a plurality of mercury jet pumps 6Z as 430 to 800 degrees 400 MPa and the like, and the gravitational acceleration of 9.8 m / second per second is cyclically induced in the induction vacuum by the nozzle jet section 6b By further accelerating, the vertical all-blade mercury turbine 8H is driven by liquid high-temperature mercury 1d, the largest acceleration in human history, and the specific volumetric heat value is reduced to 13.5 * 28 of water. Abolished Exceeding the large output of the rotor blade, the atmospheric pressure, the same speed, and the same calorie power are 910,000 times * 13.5 * 28 = about 340 million times that of using superheated steam, and 11.7 million heat quantity mercury injection of superheated steam It aims at 200 times rotation output of the existing steam turbine.

  Between the inner shaft device 60A, the outer shaft device 60B, and the outer box 77a, the bearing 80, the thrust bearing 80a, the counter-rotating magnetic friction power transmission device 84, and the magnetic friction transmission device 55B can be safely used with a 200 times rotation output or the like. In the process of exhausting the vertical moving blade mercury turbine 8H by rolling and driving the inner moving blade group 60C and the outer moving blade group 60D, which rotate in opposite directions with the addition of gravitational acceleration being maximized, Heat recovery from the mercury exhaust saturation temperature around 220 ° C. with the intake air 28a of the vaporized hot air recovery device 2B, the temperature of the intake air 28a is set to 60 to 100 ° C., etc. The heat of gas 49 is recovered around 200 degrees, compressed by energy storage compressor 20X or existing compressor 20Y, compressed air temperature is heated several times to 500-1000 degrees, etc. with compressed mercury + water The heat pump 1G is configured to heat the mercury + water with the reduced-diameter compression chamber mercury heat exchanger 2Z + water heat exchanger 2Y, cool the compressed air 28a to around 200 degrees, and cool the final compressed air High pressure combustion heat exchange cooling combustion without limit fuel injection combustion in the process, divided into high temperature mercury 1d explosive force + high temperature water 52b explosive force + combustion gas mass explosive force.

  The all blade combustor 32D selected from the eight types of all blade combustors 32X uses an energy storage compressor 20D that omits the piston rod of an existing gasoline engine and is light and simple, and uses the cylinder head 15 and the check valve 97. The double-headed enlarged piston 21 is directly reciprocated by the rotation of the horizontal or vertical crankshaft 16 after being bent vertically or 90 degrees, and the energy storage compressor 20D of the expanded-compression chamber 10a having the simplest structure. By using multiple cylinders, the biston diameter and the piston stroke are appropriately expanded and reduced, and any gas fuel or the like is used for heat recovery compression heat recovery, and the counter rotating magnetic friction power transmission device 84 or counter rotating gear device 84Y is used. Etc., and through a magnetic friction transmission device 55B, a gear-type transmission 55Y, etc., the vertical rotor shaft mercury turbine 8H and the vertical crankshaft 16 are connected so as to be capable of shifting, and the water heat exchanger 2Y, etc. What was provided on the left and right, you have a Zendotsubasa combustion section 32D. And either left or right is the precompression compression chamber water heat exchanger 2Y, etc., and the cooling water is supplied to the other water heat exchanger 2Y, etc., and the one that burns with fuel injection ignition combustion is the full blade combustion part 30H.

  The series vertical all-blade turbine 8M in FIG. 10 includes a vertical all-blade mercury turbine 8H, a vertical all-blade water turbine 8B, and a vertical all-blade gas turbine 8A in the outer casing 77a. A vertical all-blade water turbine 8B and a vertical all-blade gas turbine 8A are vertically connected in series up to the top, and in the process of aiming for a small, simple and large output, Between the inner shaft device 60A + outer shaft device 60B and the outer casing 77a of the moving blade mercury turbine 8H, the vertical all moving blade water turbine 8B, the vertical all moving blade gas turbine 8A, or the vertical all moving blade water turbine 8B and the vertical type. A bearing 80, a thrust bearing 80a, a counter rotating magnetic frictional power transmission device 84 or a counter rotating gear device 84Y is provided between the inner shaft device 60A + outer shaft device 60B and the outer casing 77a of the whole rotor blade gas turbine 8A, and further on the inner side. Of the shaft device 60A and the outer shaft device 60B. The provided bearing 80 and a thrust bearing 80a also corresponds to 200 times the rotational output of the same amount of fuel existing engines.

  A vertical all-blade mercury turbine 8H, a vertical all-blade water turbine 8B, a vertical all-blade gas turbine 8A, etc. are connected to each other by shifting with a magnetic friction transmission 55B or a transmission 55Y. A bearing is formed between the rotary shaft 77a and the rotary shaft combustion unit 32X, such as a generator, and the like. Ensuring sufficient installation space for the cooler 2A, the cold energy recovery unit 103, etc., saving the site area of the building to be accommodated, facilitating high-rise buildings with 4th and 5th floors, folding 90 degrees on the selected floor and crankshaft And the generator shaft can be rotated, and the selected full blade combustion section 32X or full blade combustion section 32Y not shown in the figure is driven to drive the vertical all blade mercury turbine 8H or vertical all blade water turbine 8B or soot. Drives all type rotor blade gas turbine 8A.

  The contra-rotating magnetic frictional power transmission device 84 in FIG. 11 corrects the previous application, and the inner shaft device 60A and the outer shaft device 60B are coupled to each other by bearings 80, 80, 80 in the stationary outer box 94, A magnetized friction wheel 37a meshing with the magnetized friction wheel 37a of the support shaft 81 is fixed to the inner shaft device 60A, and thrust bearings 80a and 80a are provided between the inner shaft device 60A and the fixed outer case 94. In this case, a magnetized friction wheel 37a meshing with the inner magnetized friction wheel 37b fixed to the outer shaft device 60B is fixed, and the plurality of support shafts 81 magnetized friction wheels 37a are rotated counterclockwise by the right rotation of the inner shaft device 60A. The outer shaft device 60B to which the inner magnetized friction wheel 37b is fixed is rotated counterclockwise, and the outer shaft device 60B and the inner shaft device 60A are rotated in directions opposite to each other. Drives blade water turbine 8B and vertical all blade air turbine 8A It is. Similarly, correct the magnetic friction transmission 55B and magnetic friction synchronizer 55.

  In the magnetized friction wheel 37a and the inner magnetized friction wheel 37b, the meshing portion of the existing gear and the internal gear becomes large, and the power transmission surface increases in friction loss due to sliding contact and generates frictional heat. In high-speed use such as the reverse magnetic friction power transmission device 84 and the magnetic friction transmission device 55B, the meshing portion is reduced as much as possible to reduce the sliding contact of the rotor blade transmission surface, and the sliding contact is reduced as much as possible by the attractive force of the magnet. It is close to rolling contact, reduces friction loss, and can be used for ultra-high speed rotating parts. Therefore, it approaches the gear at low speed, and the meshing part of the magnetized friction wheel 37a shrinks at high speed. Also used as a water pump for cooling frictional heat, like the existing gear pump, a water supply path 96A is provided in the water compression section, and a water absorption path 95A is provided in the water suction section. 84, the magnetic friction synchronization device 55, the gear type synchronization device 55, the magnetic friction transmission device 55B, and the gear type transmission device 55Y are similarly used for the water pump / magnetic friction synchronization device 55, the water pump / gear type synchronization device 55, The pump and magnetic friction transmission 55B and the water pump and gear transmission 55Y are used.

  The generation of the air suction / injection propulsion output of the various jets in FIG. 12 uses the reduced diameter compression chamber mercury heat exchanger 2Z to cool the combustion gas 49 temperature and the compressed air temperature, the high temperature mercury 1d temperature, the high temperature water 52b temperature, At the superheated steam 50 temperature, the combined engine injection part 79K is separated from the whole blade combustion part 32X and simplified, and the combustion gas 49 and superheated steam 50 are used in the whole blade combustion part 32X depending on the flight speed. The temperature of the combustion gas 49 is easily increased by high-temperature and high-pressure air, the combustion gas control valve 24 is opened, and the combustion gas 49 explosive force with a large amount of oxygen remaining is supplied to the combustion gas reservoir 95a at around 40 to 24 to 400 MPa. In the process of driving the combined engine injection unit 79K with combustion gas 49 explosive force + combustor 1Y fuel injection combustion + superheated steam 50 explosive force The low-temperature combustion gas 49 is supplied to the combustor 1Y, the fuel 1b is supplied to the plurality of fuel control valves 25b open fuel reservoir 95B, the fuel 1b is burned at the maximum amount by the fuel injection pump 1D, and the outer peripheral superheated steam reservoir is burned. 95c superheated steam 50 is heated to the highest temperature, and superheated steam 50 cooled by cooling fin 5B is used for high-temperature and high-pressure injection and injected from combustion gas injection rocket nozzle 6Y + superheated steam rocket nozzle 6A.

  The superheated steam 50 is supplied to the superheated steam reservoir 95c on the outer periphery of the combustor 1Y, and the cooling fin 5B is provided in parallel on the outer periphery to enable high-temperature injection of the air-cooled superheated steam, thereby heating the low-temperature combustion gas injection and the peripheral superheated steam. This enables high-temperature mass combustion of the combustor 1Y, increases the air suction / injection propulsion output of the superheated steam 50 + combustion gas 49, and injects from the superheated steam rocket nozzle 6A + combustion gas injection rocket nozzle 6Y. The theoretical best combined engine injection unit 79K that maximizes output easily, reduces friction loss with a rocket nozzle, makes high-speed injection, and streamlined combined engine injection unit 79K aims at 10 times the recoil of existing jets, outside the combined engine injection unit Combined with the cylindrical rotating part 77G of the box 77F, the magnetic friction power unit 55 provided on the flying wing 38b and the flying tail 38c, and the publicly known technology. The jet outer box 77F can be rotated 90 to 180 degrees or more according to the application, allowing vertical ascent, vertical descent, and reverse injection to be an airfield that can depart and land anywhere on the rooftop of the building, the moon, stars, etc. Mach 32's escape speed and the speed of light to reach the speed of light as much as possible. Air suction / injection output is generated by various air suction / injection drive devices such as ships and various ultra-high-speed battle ships.

  13 The generation of the air suction / injection output of the combined engine airplane 38A is achieved by using the reduced diameter compression chamber mercury heat exchanger 2Z as the precompression diameter compression chamber mercury heat exchanger 2Z, and using a vertical all blade mercury turbine 8H + 竪The full rotor blade combustion section 32X is driven by the type full rotor blade turbine 8B, the combined engine injection section 79K is driven by the combustion gas 49 mass output + superheated steam 50 explosive force, and the combined engine injection section 79K is driven by the flying blade 38b or Divided equipment on the left and right of the flying tail 38c, and the combined engine combustion part 31X or the whole moving blade combustion part 32X are divided and installed on the vertical blades 38d to 38d, and the combined engine injection part 79K in FIG. The fuel injection pump 1D injects and burns a large amount of low-temperature combustion gas 49 close to compressed air close to, and heats the superheated steam 50 in the superheated steam reservoir 95c around the combustor 1Y in the process of increasing the fuel amount, Cooling fin 5B provided on the periphery cools the superheated steam to enable high-temperature superheated steam and high-temperature combustion gas injection, and injection from superheated steam rocket nozzle 6A + combustion gas injection rocket nozzle 6Y enables high-temperature high-pressure mass combustion injection By increasing the injection propulsion output to generate the best theoretical simple injection propulsion output, the air and vacuum ahead are sucked and injected to increase the injection propulsion output of the same fuel amount to 10 times that of existing jets.

  When flying in the air, high-speed and high-pressure dynamic pressure air is sucked from the blade leading edge center 38e of the flying blade 38b or the flying tail blade 38c, and is selected from the intake valve 28 of the selected combined engine combustion unit 31X or all blade combustion unit 32X. Inhalation, pre-compression compression and main pressure compression, high-pressure combustion heat exchange cooling combustion without limit by reduced diameter compression chamber mercury heat exchanger 2Z, high temperature mercury 1d vaporization explosive force + superheated steam 50 explosive force + combustion gas 49 mass explosion It is divided and stored in the power, each can be stored in large quantities, and can be used for out-of-fuel and space shuttles. It flies in a vacuum at an altitude of 100 km or more without fuel, and instantly supersonic Mach 23-28 As a space velocity, it enables day trips anywhere on the earth, and various rocket fuels are loaded to make the universe a high-speed target that approaches the speed of light over Mach 48, returning to the earth at a flight speed such as the flight wing 38b and the flight tail 38c. The water 52a tube, superheated steam 50 tube, high-temperature mercury 1d tube, or combustion gas tube, which has been reduced in weight to high pressure with carbon fiber, carbon nanotubes, etc., is connected to all the parts that become hot, and the high-pressure lightweight container is made up of heat. Collected and used as a facility for supplying heat, electricity, and cold energy during shutdown, and used as a facility for preventing the extinction of mankind along with ground facilities.

  The water 52a tube or superheated steam 50 tube or high-temperature mercury 1d tube or combustion gas tube in a high-pressure lightweight container made of carbon fiber or the like is used to collect the fireball temperature according to the flight speed and make each explosive force. Used as the main energy, the flight trunk 38a and the flight wing 38b are provided with a cockpit 10b, a control room 10c and a cabin 10d, and the control room 10c is equipped with a general control device 20 to control the whole with existing technology. . In the overall control process, the combined engine injection unit 79K provided on the left and right sides of the flying wing 38b and the flying tail 38c is controlled to rotate 90 to 180 degrees by the cylindrical rotating unit 77G, so that vertical ascent, vertical descent and reverse injection are performed. It is possible to use liquid oxygen for spacecraft, and various supersonic jets and supersonic jet fighters aiming for 10 times the speed of existing technology, various jets and various jet fighters, , The air generated by various air suction / injection drive equipment that sucks and injects air and vacuum from various space return passenger aircraft, etc., and allows vertical descent and vertical ascent on the airfield, the moon and various stars, etc. anywhere on the roof of the building, etc. It is also used as wing stability or no wing than levitation by.

  14 The air suction injection output of the air-injected ship 38B is generated by using the combined engine combustion unit 31X or the full blade combustion unit 32X selected according to the type A or the like of FIGS. 1 to 3 or 4 to 11. , Separated from the combined engine injection unit 79K and appropriately provided in the hull. Air 28a is sucked from the leading edge center 38e of the flying wing 38b, and the air 28a is sucked to collect and compress various amounts of heat as described above. Then, compression heat recovery is performed a plurality of times in the reduced-diameter compression chamber mercury heat exchanger 2Z water heat exchanger 2Y, and high-temperature mercury 1d vaporization explosive power of 430 to 800 degrees saturation pressure or higher + high temperature water 52b vaporization of about 374 degrees saturation pressure or higher Explosive power + Superheated steam 50 Explosive power + Around 40 degrees Celsius 24-400MPa Combustion gas mass Explosive power is divided and used to drive the combined engine combustion section 31X or all blade combustion section 32X, and vertical all blade mercury Turbine 8H or all blade impeller It generates silver turbine 8E, vertical all-blade water turbine 8B, or all-blade bouncing water turbine water turbine 8b drive rotation output, injection propulsion by 400MP superheated steam 50 explosive force + around 40 degrees 24-400MPa combustion gas mass explosive force Generate output.

  In the process of injection propulsion aiming at a ship close to the speed of sound, the entire low-temperature combustion gas 49 is supplied to the combustor 1Y, and the one or more combustors 1Y are heated with the superheated steam 50 in the fuel injection combustion outer periphery superheated steam reservoir 95c, The combined engine injection unit 79K is driven at the maximum fuel combustion amount and the maximum combustion temperature to maximize the air suction injection propulsion output, and one or more combined engine injection units 79K in FIG. 12 are optimally provided at the front or rear of the hull. Air in front of the hull is sucked and sprayed backwards in the enclosure at the bottom of the hull, and sprayed to the rear of the front levitation plate 9A, the front of the rear levitation plate 9B, and the parallel vertical plate 9c. The most of the bottom of the ship, which was lifted by the combustion gas 49 injection pressure or the same pressure superheated steam 50 injection pressure, and expanded by the parallel vertical plate 9c, was the theoretically best hull pressure speed levitation to minimize friction loss, and the air nozzle at the rear of the hull Air jet from 9D etc. The injection rate with an increase in the speed and natural increases in, and theoretically the best of air suction injection marine propulsion output.

  During the jet propulsion process, the rudder 40A of the air nozzle 9D and the rudder 40A of the vertical wing 38d are driven and controlled, and vehicles, fighter planes, etc., which are significantly heavier than existing airplanes, are intended for transportation at ultra-high speeds at regular intervals. The flying wing 38b and the flying tail 38c are integrally or appropriately divided and controlled by up-and-down control using existing technology, the maximum speed is made close to the sound speed, and the distance from the water is kept constant. The cockpit 10b, the cabin 10d, the control room 10c, and the cargo room 10e are provided. The control room 10c is equipped with a general control device 20 to control the whole with existing technology, and vaporization and explosion of high temperature water 52b such as 374 degrees Celsius and 400 MPa. Power + 24 degrees Celsius around 40 degrees Celsius Combustion gas explosive force + About 400 degrees Celsius 24-400 MPa superheated steam is stored and steered by the flight wing 38b and flight tail 38c, aiming at the speed of sound Cruise ships and various ferry boats and various cargo ships and various aircraft carriers and various combat ships, etc., and a variety of air suction injection drive equipment, are stopped and then used as a supply facility of heat and electricity and cold.

  15 The water suction / injection propulsion output of the water injection vessel 38C is generated by separating the selected combined engine combustion unit 31X or all blade combustion unit 32X from the water jet 79M, and the water heat exchanger 2Y has an unlimited high pressure. Combustion heat exchange cooling combustion, water injection pump 6z injection 374 degrees 400 MPa high temperature water 52b vaporization explosive force + around 500 degrees 400 MPa superheated steam explosive force + around 40 degrees around 24 to 400 MPa combustion gas explosive force, 400 MPa water vaporization explosive force The combined engine combustion unit 31X or the entire rotor blade combustion unit 32X is driven in total, and the water injection pump 6z similarly accelerates and injects the high-temperature water 52b in the vertical downward vacuum direction in the same manner as described above, and the atmospheric pressure, the same speed, and the same amount of heat work. The rate is 910,000 times that of superheated steam, and all blade blade turbines are driven. All combustion gas mass explosive power and combustor 1Y fuel injection combustion + superheat Vapor explosive force Te drives the water jet 79M, superheating the steam pressure speed + combustion gas pressure speed and injection from the ship's bottom Earth direction 囲内 to the rear, and the ship's bottom friction loss reduction driven by the combustion gas bubbles to propel floating the hull.

  Driven by the low temperature combustion gas mass explosive force and the combustor 1Y fuel injection combustion + superheated steam explosive force, the water jet 79M shown in FIG. Injecting at an optimum angle at the rear of the direction, driving and steering a rudder 40A provided at the rear of the ship bottom in the course of injection propulsion, and having a water wing 38g that can be raised and lowered, moved to an optimal position by a plurality of hydraulic cylinders 48a, Curved or bent in front of the water jet 79M to make the injection at the foremost optimal position 1 or more, with the water pressure water pressure + superheated steam pressure speed + combustion gas pressure speed bubble of the diagonally lower rear injection and the water pressure of the upper wing 38g by the hull speed As a water suction injection propulsion that lifts a large hull, the friction loss at the bottom of the parallel vertical plate 9C, which is vast due to the bubbles injected with a large amount of combustion gas, is minimized. Supplying food such as plant frankton such as CO2, oxygen and oxygen, etc. Propulsion of ultra-high speed near the same weight as an existing cargo ship, a cockpit 10b and a cabin 10d are provided in the upper part, and a cargo compartment 10e and a control room are provided in the cabin 10A. 10c is installed, and is controlled overall by the general control device 20 by the general control device 20, and various water suction injection drives such as various ships, various ferry boats, various cargo ships, various aircraft carriers, various battle ships, etc. aiming at 20 times the speed of the existing cargo ship It is used as equipment to supply heat, electricity, and cold energy during outages, and as a power generation to prevent human extinction. .

  The water jet 79M in FIG. 16 is separated from, for example, the whole blade combustion part 32X and simplified to the limit, and the high pressure combustion heat exchange cooling combustion is performed without limitation in the whole blade combustion part 32X. Other than the above, a 40-400 MPa combustion gas 49 explosive power around 40 degrees + a 400 MPa superheated steam explosive power around 400 degrees combusts a large amount of combustion gas 49 with a small amount of fuel combustion and close to compressed air in the process of driving the water jet 79M The fuel is supplied from the gas control valve 24 to the combustion gas reservoir 95a, the fuel 1b is supplied from one or more fuel control valves 25b to the fuel reservoir 95B, and fuel is injected into the combustor 1Y by the fuel injection pump 1D. In the combustion process, the superheated steam 50 of the combustor 1Y outer peripheral superheated steam reservoir 95c is heated and the cooling fin 5B provided on the outer periphery. The hot steam is cooled to enable high-temperature superheated steam and high-temperature combustion gas injection, and the maximum speed injection is performed from the superheated steam rocket nozzle 6A + combustion gas injection rocket nozzle 6Y. Supplying food enables the maximum frictional propulsion water suction jet propulsion output.

  One or more fuel injection pumps 1D are provided in the combustor 1Y, the fuel gas 49 is ignited and burned by combustion, and the superheated steam 50 in the peripheral superheated steam reservoir 95c is heated by the high-temperature and high-pressure combustion of the combustor 1Y. High-temperature high-pressure injection and high-temperature high-pressure combustion injection of combustion gas are made possible to increase the injection propulsion output and water cooling with cooling fins 5B, etc., and after injection, seawater directly cooled combustion gas dissolution such as combustion gas 49 bubble CO2 The water supply power is further increased by the supply of food such as phytoplankton and the volume reduction suction force, and the water stream injection propulsion output is maximized by the streamlined water jet 79M, which is 20 times the speed of existing cargo ships. Aiming, etc., a water jet outer box 77D is provided at the front of the bottom of the ship and bent or bent in front of the water jet 79M to make an injection at the front optimum position 1 or more. Fixed at an angle, the front water 52a is sucked and accelerated, the most efficient water suction jet hull is ascended to the maximum extent, various high-speed ships, various high-speed battle ships, various aircraft carriers, various high-speed water transportation mobile devices, etc. It is a combined energy storage cycle engine that drives water suction and jet drive equipment.

  By dividing and using combustion gas calorific value explosive force + combustion gas mass explosive force, and making all rotor blade water turbines drive vaporization explosive force of water, the vaporizing explosive force is concentrated in the low pressure part downstream in the direction of travel, the theoretical best The fuel consumption is reduced to 1/539, and the acceleration of gravity injection in the vacuum vertically is added 9.8m / second per second for water injection acceleration. Exceeding the large output, the atmospheric pressure, the same speed, and the same calorific power, kg weight m / sec, are 1700 times * 539 times that of the existing steam turbine, approximately 910,000 times, and the existing steam injection of 1/4000 calorie water is used. As a 200 times rotation output of the steam turbine, there is a possibility that all power plants, ships and airplanes in the existing world will be completely abolished and all blades water turbine + all blades gas turbine driven.

  Divided and used for combustion gas calorific power + combustion gas mass explosive power, and using all blade water turbine + all blade gas turbine drive, the power generation amount is 200 times that of the existing steam turbine, There is a possibility that the nuclear power plant will be completely abolished, the seawater temperature will rise 0 and CO2 emissions will be 0.

  Divided and used for combustion gas calorific value explosive force + combustion gas mass explosive force, all moving blade water turbine + all moving blade gas turbine drive, electricity rate is 1/10 etc., all automobiles in the world are driven by storage battery, There is a possibility that various propeller ships, various rotational force driven mechanical devices, etc. are driven by storage batteries to reduce CO2 exhaust to zero.

  Divided and stored into combustion gas calorie explosive force + combustion gas mass explosive force, driving all moving blade mercury turbine + all moving blade water turbine + all moving blade gas turbine, the same pressure at the same atmospheric pressure of all moving blade mercury turbine Calorific power kg weight m / sec is 910,000 times * 13.5 * 28 = 34,000,000 times that of existing steam turbine, and 11.7 million heat quantity mercury injection of superheated steam is used as 200 times rotation output of existing steam turbine. The superheated steam + oxygen-rich combustion gas + fuel + combined engine injection unit 79K increases the injection propulsion output by 10 times, etc. But there is a possibility of a day trip.

  Divided and used for combustion gas calorie explosive force + combustion gas mass explosive force, driving all blade mercury turbine + all blade water turbine + all blade gas turbine, and rotating output closer to 200 times that of existing steam turbine , Superheated steam + oxygen-rich combustion gas + fuel + combined engine injection unit 79K increases injection propulsion output by 10 times, etc., and accelerates without limit by the space shuttle, bringing the universe closer to the speed of light more than Mach 48 , There is a possibility to make space travel prime.

  Rotational output increased by 200 times Injection propulsion output increased by 10 times, etc., so there is a possibility that the speed of various ships will approach sonic speed due to high-temperature and high-pressure injection of combustion gas, and various supersonic jets and various supersonic jets Fighters, various ultra-high-speed ships, various ultra-high-speed battle ships, various ultra-high-speed aircraft carriers, various space return passenger aircraft, various space return aircraft, various air transport mobile devices and various water transport mobile devices , Etc., may be used as a facility for supplying CO2 exhaust 0 heat, electricity, and cold heat when the engine is stopped.

  Combustion gas exhaust that approaches the absolute 0 degree of all rotor blade gas turbines by collecting compressed air heat amount and other heat amounts recovered by various heat amounts, repeatedly compressing heat recovery, endlessly high pressure combustion heat exchange cooling combustion There is a possibility that the entire heat exchange can be used with a huge amount of cold heat, and all the remaining combustion gases such as CO2 are dissolved in water to form combustion gas-dissolved water, which is then supplied to the seabed to greatly increase seagrasses and phytoplanktons. It can proliferate and proliferate human food such as fish through the food chain.

  Combustion gas exhaust that approaches the absolute 0 degree of all rotor blade gas turbines by collecting compressed air heat amount and other heat amounts that have been recovered and recovered, and repeatedly compressing heat recovery and endlessly high-pressure combustion heat exchange cooling combustion Compressed air cooling, alcohol cooling, and ice cooling as combustion gas cooling, and enter and create various cooling applications such as direct cooling, refrigeration, ice making, and methane hydrate cooling and recovery there is a possibility.

  Combustion gas exhaust that approaches the absolute 0 degree of all rotor blade gas turbines by collecting compressed air heat amount and other heat amounts recovered by various heat amounts, repeatedly compressing heat recovery, endlessly high pressure combustion heat exchange cooling combustion The heat exchange storage of all of them as compressed air cold, alcohol cold or ice cold, and sell them to the consumer and heat exchange customers in the summer, aiming for 1/10 power consumption, etc. Manufactures and sells various types of household refrigeration equipment, various refrigeration equipment, various air conditioning equipment, various ice making equipment, various heating and cooling piping buildings, etc. There is a possibility of cooling the whole and turning the heat island phenomenon into a cold summer city.

  Heat, electricity, and cold heat supply equipment whose rotational output is close to 200 times that of existing steam turbines, etc., because the amount equivalent to the amount of supplied heat is surplus for exclusive use of rotational output, so the surplus heat amount is superheated steam temperature 52d such as 400 degrees Celsius or glycerin temperature 52d or water temperature / heat 52d, and use by water / heat 52d as a by-product of power generation, aiming for power consumption of 1/10, etc. Various commercial and household heating equipment, various cooking equipment and various hot water There is a possibility of manufacturing and selling equipment, various dishwashers, various washing and drying machines, and various seawater desalination equipment.

  Heat, electricity, and cold power supply equipment whose rotational output is close to 200 times that of existing steam turbines, etc., because the amount equivalent to the amount of supplied heat is surplus for exclusive use of rotational output, so the superheated steam temperature 52d such as 300 degrees Celsius or water temperature heat There is a possibility to enter 52 methane recovery business by injecting it into methane hydrate or permafrost methane.

  The combustion gas 49 heat quantity or the compressed air heat quantity 28b is recovered by the intake air 28a, and the compressed heat exchange cooling heat recovery is performed by the heat pump 1G + water heat exchanger 2Y of the energy storage compressor, and high temperature water 52b such as 374 degrees 24-400 MPa. And the entire blade turbine is driven by vaporization explosive force to reduce the heat consumption to 1/539 of that of the existing steam turbine, to a gravitational acceleration of 9.8 m / sec. There is a possibility that a heat, electricity and cold supply facility is used, and cold cooling is performed in the exhaust process, resulting in 0 CO2 exhaust gas + 0 seawater temperature rise.

Example of cross section of united engine combustion section 31A and various turbine blades (Example 1) Sectional view of driving of all blade gas turbine 8a and all blade water turbine 8b (Example 2) Cross-sectional view of all-rotor impeller turbine and combined engine combustion section 31A (Example 3) Cross section of opposed series full blade impeller turbine 8K gravity acceleration utilization (Example 4) Front sectional view of gravity acceleration using series full blade impeller turbine (Example 5) Side cross-sectional view using gravity acceleration in series all blade impeller turbine 8L (Example 6) Cross-sectional view of vertical rotor blade water turbine 8B and rotor blade combustion section 32E (Example 7) Vertical sectional blade gas turbine 8A and full blade combustion section 32D sectional view (Eighth embodiment) Cross section of vertical all blade mercury turbine 8H and all blade combustion section 32D (Example 9) Sectional view of series vertical type all blade turbine 8M (Example 10) Cross-sectional view of counter-rotating magnetic frictional power transmission device 84 (Example 11) Sectional drawing which shows union engine injection part 79K (Example 12) Explanatory drawing which shows united engine airplane 39A (Example 13) Sectional drawing which shows air injection ship 39B (Example 14) Sectional drawing which shows water-injection ship 39C (Example 15) Sectional view showing water jet 79M (Example 16)

Explanation of symbols

  1A: External air chamber, 1C: Alcohol, 1D: Fuel injection pump, 1E: Mercury pump, 1F: Water pump, 1G: Heat pump (heat recovery with intake air and compression with gas compressor) 1Y: Combustor 1Z: Combustion chamber, 1a: Combustion section, 1b: Fuel, 1d: High-temperature mercury, 1e: Coated steel ball, 2A: Cold heat cooler, 2B: Vaporized hot air recovery device, 2C: Compression heat recovery device, 2Y: Water Heat exchanger, 2Z: Shrinkage compression chamber mercury heat exchanger, 2a: Condenser, 3A: Water repellent effect (means for reducing friction loss with water) 3B: Heating high temperature means (electric resistance or high temperature for electromagnetic heating) 3C: Cold heat recovery means, 3G: Water repellent action (means for reducing friction loss with mercury) 4A: Turbine blade cross section (existing cross section) 4B: Turbine blade cross section (output surface curved small cross section) 4C: Turbine blade cross section (output surface straight line) Cross section) 4D: Ta Bin blade cross section (output opposite surface linear cross section) 4E: Turbine blade cross section (output opposite surface curved small cross section) 4F: Turbine blade cross section (existing opposite cross section) 4X: Turbine blade cross section (selected cross section from 4A to 4F) 4a: Outside Compressor blade group, 4b: Inner compressor blade group, 5A: Exhaust heat quantity, 5B: Cooling fin, 5c: Gas exhaust chamber, 6: Nozzle, 6a: Nozzle injection section, 6b: Nozzle injection section, 6d: Nozzle injection section 6Z: Water injection pump, 6A: Superheated steam rocket nozzle, 6M: Combustion gas rocket nozzle, 6Y: Combustion gas injection rocket nozzle, 6Z: Mercury injection pump (improved from all fuel injection pumps, gear pumps, etc.), 7: Fuel Injection valve, 8a: Full bucket blade wheel gas turbine (full blade gas turbine), 8b: Full bucket blade wheel water turbine (full blade water turbine), 8c: -Bin blade, 8d: side plate, 8e: cylindrical body, 8A: vertical all-blade gas turbine (full blade air turbine), 8B: vertical all-blade water turbine (full blade air turbine), 8E: full motion 8H: vertical all-blade mercury turbine, 8K: opposed series all-blade turbine, 8L: series all-blade turbine, 8M: Series vertical all-blade turbine, 8X: all-blade turbine (all-blade mercury turbine + all-blade water turbine + all-blade gas turbine), 9: one-way air flow heat exchanger (for exhaust heat recovery) 9A: Front levitation plate, 9B: Rear levitation plate, 9C: Parallel vertical plate, 9D: Air injection port, 10A: Cabin, 10a: Expanded compression chamber, 10b: Pilot room, 10c: Control room, 10d : Guest room, 10e: Cargo compartment 11A: partition wall, 11B: mercury chamber, 11B: water chamber, 11C: air chamber, 15: cylinder head, 16: crankshaft, 16A: crank, 20A: energy storage compressor, 20B: energy storage compressor, 20C: energy Storage compressor, 20D: energy storage compressor, 20E: energy storage compressor, 20F: energy storage compressor, 20G: energy storage compressor, 20H: energy storage compressor, 20X: energy storage compressor (from 20A to 20H) 20Y: Existing compressor (compressor selected from existing gas compressors) 21: Expanded piston, 24: Combustion gas control valve, 25: Superheated steam control valve, 25b: Fuel control valve, 25d : Mercury control valve, 25B: High temperature water control valve, 28: Intake valve, 28a: Air, 28b: Compressed air 29: Various energy conservation cycle coalescing engines (various rockets, various reciprocating engines, steam turbines, gas turbines and energy conservation cycle engines are merged), 31: Power transmission surface, 31A: Coalition engine combustion section (combined engine combustion with 20A) Part), 31B: coalescence engine combustion part (with 20B), 31C: coalescence engine combustion part (with 20C), 31D: coalescence engine combustion part (with 20D), 31E: coalescence engine combustion part (with 20E), 31F: coalescence Engine combustion section (20F equipped), 31G: Combined engine combustion section (20G equipped), 31H: Combined engine combustion section (20H equipped), 31X: Combined engine combustion section (20X equipped), 31Y: Combined engine combustion section (20Y equipped) Combined engine combustion section), 32A: All blade combustion section (20A equipped all blade combustion section), 32B: All blade combustion section (20B equipped), 3 2C: All blade combustion part (with 20C), 32D: All blade combustion part (with 20D), 32E: All blade combustion part (with 20E), 32F: All blade combustion part (with 20F), 32G: All blade combustion part (20G equipped), 32H: All blade combustion part (20H equipped), 32X: All blade combustion part (20X equipped), 32Y: All blade combustion part (20Y equipped all blade combustion part) 33: Bar magnet, 34: Electromagnet, 35: Direction of rotation, 37: Double-headed enlarged piston, 37a: Magnetized friction wheel (including gears), 37b: Inner magnetized friction wheel (including internal gears) 38A: Combined Engine airplane, 38B: Air-injection ship, 38C: Water-injection ship, 38a: Flight trunk, 38b: Flight wing, 38c: Flight tail, 38d: Vertical wing, 38e: Wing leading edge inlet, 38g: Water wing, 39: Fixing groove, 39A: united Kanto Airplane, 39B: Air-injected ship, 39C: Water-injected ship, 40: Drive tool, 40A: Rudder, 40a: Pendulum arm, 46: Magnet part, 47: York, 48a: Hydraulic cylinder, 49: Combustion gas, 49A: Internally magnetized friction wheel device 49a: Combustion gas stirring plate 50: Superheated steam 51: Air extractor 51A: Magnetized friction wheel device 51a: Gas extractor 52a: Water 52b: Hot water 52d: Mercury temperature, 52d: Water temperature, 52d: Superheated steam temperature, 52d: Glycerin temperature, 52e: Ice cooling temperature, 52e: Water cooling temperature, 52e: Alcohol cooling temperature, 52e: Compressed air cooling temperature, 52g: Combustion gas dissolved water, 52h: Cold water 55: Magnetic friction synchronizer (including gear type and water pump combined use), 55: Gear type synchronizer, 55B: Magnetic friction transmission ( 55Y: Gear type transmission (selected from existing transmission) 60A: Inner shaft device, 60B: Outer shaft device, 60C: Inner blade group, 60D: Outer blade group, 77 : Outer box, 77a: Turbine outer box, 77b: Cylindrical outer box, 77C: Jet engine outer box, 77D: Water jet outer box, 77F: Combined engine injection part outer box, 77G: Cylindrical rotating part, 78K: Combined engine Injection unit, 78M: Water jet, 79K: Combined engine injection unit, 79M: Water jet, 80: Bearing, 80a: Thrust bearing, 80A: Joint, 81: Support shaft, 81a: Support point, 84: Counter reversal magnetic friction power Transmission device (including gear type and water pump) 84Y: Counter-rotating gear device (created by existing technology), 88: Known fuel injection valve, 94: Outer box, 94A: Vertical portion of outer box, 95: High temperature water reservoir, 95A: Water absorption path, 95B: Fuel reservoir, 95D: Mercury reservoir, 95a: Combustion gas reservoir, 95c: Superheated steam reservoir, 95d: Combustion gas reservoir, 96 : Stroke, 96A: Water supply path, 97: Check valve, 98: Valve seat, 99: Valve body, 103: Cold energy recovery device (cold energy recovery with alcohol)

Claims (5000)

  A turbine blade section (4F) having a tabine blade (8c) and an all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Energy conservation cycle coalescence engine.   A turbine blade section (4F) having a tabine blade (8c) and an all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Energy conservation cycle coalescence engine.   Various energy storage as hydroelectric power storage battery driven various rotary output drive equipment equipped with a turbine blade section (4F) and a combined engine combustion section (31X) that performs hydroelectric power generation with a turbine blade turbine (8F) and a turbine blade turbine. Cycle coalescence engine.   Various energy storage as hydroelectric power storage battery driven various rotary output drive equipment equipped with a combined turbine combustion section (31Y) that performs hydroelectric power generation with a turbine blade cross section (4F) and a turbine blade turbine (8C) that makes a turbine blade cross section (4F) Cycle coalescence engine.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade impeller water turbine heating high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation and various rotations driven by hydroelectric storage battery Various energy storage cycle coalescence engine as output drive equipment.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade impeller water turbine with heating high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation and various rotations driven by hydroelectric storage battery Various energy storage cycle coalescing engines as output drive devices.   Turbine blade (8c) of power generation technology with turbine blade cross-section (4E), and all blade combustion section (32X) for hydroelectric power generation by heating high temperature means (3B) with vertical type all blade water turbine, driving hydroelectric storage battery Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade (8c) of power generation technology with turbine blade cross-section (4E), and all blade combustion section (32Y) for hydroelectric power generation with heating high temperature means (3B) using vertical all blade water turbine, driving hydroelectric storage battery Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, various rotating output drive equipment driven by hydroelectric storage battery Various energy conservation cycle coalescing engines.   Turbine blades (8c) of the power generation technology with the turbine blade cross section (4E) and all rotor blade combustion section (32Y) that performs hydroelectric power generation with a vertical all blade water turbine, various rotating output drive devices driven by hydroelectric storage batteries Various energy conservation cycle coalescing engines.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31X) for hydroelectric power generation with a water turbine with all-wheel impellers, and various rotational output drive devices driven by a hydroelectric storage battery Various energy conservation cycle coalescence engine.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) that performs hydroelectric power generation with a water turbine with all-wheel impellers, and various rotational output drive devices driven by a hydropower storage battery Various energy conservation cycle coalescence engine.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and combined rotor combustion unit (31X) for hydroelectric power generation with reduced friction loss by all blade impeller water turbines and various rotational output drive devices driven by hydroelectric storage battery A variety of energy conservation cycle coalescing engines.   Turbine blade (8c) of power generation technology with turbine blade cross section (4E) and combined engine combustion section (31Y) for hydroelectric power generation with reduced friction loss with all blade impeller water turbines and various rotary output drive devices driven by hydroelectric storage battery A variety of energy conservation cycle coalescing engines.   A turbine blade section (4F) having a tabine blade (8c) and an all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Energy conservation cycle coalescence engine.   A turbine blade section (4F) having a tabine blade (8c) and an all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Energy conservation cycle coalescence engine.   Various energy storage as hydroelectric power storage battery driven various rotary output drive equipment equipped with a turbine blade section (4F) and a combined engine combustion section (31X) that performs hydroelectric power generation with a turbine blade turbine (8F) and a turbine blade turbine. Cycle coalescence engine.   Various energy storage as hydroelectric power storage battery driven various rotary output drive equipment equipped with a combined turbine combustion section (31Y) that performs hydroelectric power generation with a turbine blade cross section (4F) and a turbine blade turbine (8C) that makes a turbine blade cross section (4F) Cycle coalescence engine.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade impeller water turbine heating high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation and various rotations driven by hydroelectric storage battery Various energy storage cycle coalescence engine as output drive equipment.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade impeller water turbine with heating high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation and various rotations driven by hydroelectric storage battery Various energy storage cycle coalescing engines as output drive devices.   Turbine blade (8c) of power generation technology with turbine blade cross-section (4E), and all blade combustion section (32X) for hydroelectric power generation by heating high temperature means (3B) with vertical type all blade water turbine, driving hydroelectric storage battery Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade (8c) of power generation technology with turbine blade cross-section (4E), and all blade combustion section (32Y) for hydroelectric power generation with heating high temperature means (3B) using vertical all blade water turbine, driving hydroelectric storage battery Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, various rotating output drive equipment driven by hydroelectric storage battery Various energy conservation cycle coalescing engines.   Turbine blades (8c) of the power generation technology with the turbine blade cross section (4E) and all rotor blade combustion section (32Y) that performs hydroelectric power generation with a vertical all blade water turbine, various rotating output drive devices driven by hydroelectric storage batteries Various energy conservation cycle coalescing engines.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31X) for hydroelectric power generation with a water turbine with all-wheel impellers, and various rotational output drive devices driven by a hydroelectric storage battery Various energy conservation cycle coalescence engine.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) that performs hydroelectric power generation with a water turbine with all-wheel impellers, and various rotational output drive devices driven by a hydropower storage battery Various energy conservation cycle coalescence engine.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and combined rotor combustion unit (31X) for hydroelectric power generation with reduced friction loss by all blade impeller water turbines and various rotational output drive devices driven by hydroelectric storage battery A variety of energy conservation cycle coalescing engines.   Turbine blade (8c) of power generation technology with turbine blade cross section (4E) and combined engine combustion section (31Y) for hydroelectric power generation with reduced friction loss with all blade impeller water turbines and various rotary output drive devices driven by hydroelectric storage battery A variety of energy conservation cycle coalescing engines.   A hydropower storage battery drive that includes a turbine blade cross section (4F) and a turbine blade combustion section (32X) that performs hydroelectric power generation using a vertical all blade water turbine with a turbine blade cross section (4F) and includes various types of heating equipment. Various energy storage cycle coalescing engines as various rotational output drive devices.   A hydroelectric storage battery drive that includes a turbine blade section (4F) and a turbine blade combustion section (32Y) that generates hydroelectric power using a vertical all-blade water turbine with a turbine blade cross section (4F) and includes various types of heating equipment. Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross section (4F) tabine blade (8c) and all-compartment blade bouncing water turbine combined unit combustion unit (31X) for hydroelectric power generation and various rotations driven by hydroelectric storage batteries including various heating equipment Various energy storage cycle coalescence engine as output drive equipment.   Turbine blade cross section (4F) with tabine blade (8c) and a combined engine combustion section (31Y) for hydroelectric power generation with all blade impeller water turbines and various rotations driven by hydroelectric storage batteries including various heating equipment Various energy storage cycle coalescence engine as output drive equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) for generating hydroelectric power by heating high temperature means (3B) with all blade impeller water turbines and various heating equipment using heat Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for heating and heating means (3B) hydroelectric power generation with a fully moving blade propeller water turbine, and various heating equipment using warm heat Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a all-blade combustion section (32X) for hydroelectric power generation with heating high-temperature means (3B) by a vertical all-blade water turbine, and various heating using warm heat Various energy storage cycle coalescing engines, which are driven by hydroelectric storage batteries and various rotational output drive devices including equipment.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E), and a full-blade combustion unit (32Y) for hydroelectric power generation with heating high-temperature means (3B) by a vertical all-blade water turbine, and various heating using warm heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices including equipment.   Water including a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine, including various types of heating equipment using heat. Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Water including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, including various heating equipment using warm heat Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   A hydroelectric storage battery comprising a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) that performs hydroelectric power generation with an all-wheel impeller water turbine and various heating equipments using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   A hydroelectric storage battery comprising a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation using a water turbine with all rotor blades, and including various types of heating equipment. Various energy storage cycle coalescing engines as various rotational output drive devices.   Includes turbine blade (8c) with power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31X) for hydrodynamic power generation with reduced friction loss by all blade impeller water turbine, including various heating equipment using heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes turbine blade (8c) with power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31Y) for hydrodynamic power generation with reduced friction loss with all blade impeller water turbine, and includes various heating equipment using heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   A hydropower storage battery drive that includes a turbine blade cross section (4F) and a turbine blade combustion section (32X) that performs hydroelectric power generation using a vertical all blade water turbine with a turbine blade cross section (4F) and includes various types of heating equipment. Various energy storage cycle coalescing engines as various rotational output drive devices.   A hydroelectric storage battery drive that includes a turbine blade section (4F) and a turbine blade combustion section (32Y) that generates hydroelectric power using a vertical all-blade water turbine with a turbine blade cross section (4F) and includes various types of heating equipment. Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross section (4F) tabine blade (8c) and all-compartment blade bouncing water turbine combined unit combustion unit (31X) for hydroelectric power generation and various rotations driven by hydroelectric storage batteries including various heating equipment Various energy storage cycle coalescence engine as output drive equipment.   Turbine blade cross section (4F) with tabine blade (8c) and a combined engine combustion section (31Y) for hydroelectric power generation with all blade impeller water turbines and various rotations driven by hydroelectric storage batteries including various heating equipment Various energy storage cycle coalescence engine as output drive equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) for generating hydroelectric power by heating high temperature means (3B) with all blade impeller water turbines and various heating equipment using heat Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for heating and heating means (3B) hydroelectric power generation with a fully moving blade propeller water turbine, and various heating equipment using warm heat Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a all-blade combustion section (32X) for hydroelectric power generation with heating high-temperature means (3B) by a vertical all-blade water turbine, and various heating using warm heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices including equipment.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E), and a full-blade combustion unit (32Y) for hydroelectric power generation with heating high-temperature means (3B) by a vertical all-blade water turbine, and various heating using warm heat Various energy storage cycle coalescing engines, which are driven by hydroelectric storage batteries and various rotational output drive devices including equipment.   Water including a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine, including various types of heating equipment using heat. Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Water including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, including various heating equipment using warm heat Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   A hydroelectric storage battery comprising a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) that performs hydroelectric power generation with an all-wheel impeller water turbine and various heating equipments using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   A hydroelectric storage battery comprising a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation using a water turbine with all rotor blades, and including various types of heating equipment. Various energy storage cycle coalescing engines as various rotational output drive devices.   Includes turbine blade (8c) with power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31X) for hydrodynamic power generation with reduced friction loss by all blade impeller water turbine, including various heating equipment using heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes turbine blade (8c) with power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31Y) for hydrodynamic power generation with reduced friction loss with all blade impeller water turbine, and includes various heating equipment using heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Driven by a hydroelectric storage battery, which has a turbine blade cross section (4F) and a turbine blade combustion section (32X) for hydroelectric power generation by a vertical all-blade water turbine, including various cooking equipments using heat. Various energy storage cycle coalescing engines as various rotational output drive devices.   Driven by a hydroelectric power storage battery, which has a turbine blade cross section (4F) and a turbine blade combustion section (32Y) for hydroelectric power generation by a vertical all blade water turbine with a turbine blade cross section (4F) and includes various types of cooking equipment using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross section (4F) tabine blade (8c) and all-wheel blade impeller water turbine combined unit combustion unit (31X) with hydroelectric power storage battery driven various rotations including various cooking equipment using heat Various energy storage cycle coalescence engine as output drive equipment.   Turbine blade cross section (4F) with tabine blade (8c) and a combined engine combustion section (31Y) for hydroelectric power generation with all blade impeller water turbines and various rotations driven by hydroelectric storage batteries including various cooking equipments using heat Various energy storage cycle coalescence engine as output drive equipment.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and all blade impeller water turbine heating high temperature means (3B) coalescence engine combustion unit (31X) for hydroelectric power generation and various cooking equipment using heat Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   Turbine blade cross section (4E) power generation technology turbine blade (8c) and all blade impeller water turbine heating high temperature means (3B) coalescence engine combustion section (31Y) for hydroelectric power generation and various cooking equipment using heat Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade (8c) of power generation technology with a turbine blade cross-section (4E) and a whole blade combustion section (32X) for heating and heating means (3B) hydroelectric power generation with a vertical all blade water turbine, and various cooking using heat Various energy storage cycle coalescing engines, which are driven by hydroelectric storage batteries and various rotational output drive devices including equipment.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and vertical all blade water turbine with heating high temperature means (3B) all blade combustion section (32Y) for hydroelectric power generation Various energy storage cycle coalescing engines, which are driven by hydroelectric storage batteries and various rotational output drive devices including equipment.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine and water including various cooking equipment using heat Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Water including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, including various cooking equipment and equipment using heat Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Hydroelectric power storage battery comprising various cooking equipment and equipment using thermal energy, comprising a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) that performs hydroelectric power generation using a fully moving blade impeller water turbine Various energy storage cycle coalescing engines as various rotational output drive devices.   A hydroelectric storage battery comprising a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation using a water turbine with all rotor blades, including various cooking equipments using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Includes turbine blade (8c) with power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31X) for hydrodynamic power generation with reduced friction loss by all blade impeller water turbine, and includes various cooking equipment equipment using heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes turbine blade (8c) with power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31Y) for reducing friction loss with all blade impeller water turbine, and includes various cooking equipment using heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Driven by a hydroelectric storage battery, which has a turbine blade cross section (4F) and a turbine blade combustion section (32X) for hydroelectric power generation by a vertical all-blade water turbine, including various cooking equipments using heat. Various energy storage cycle coalescing engines as various rotational output drive devices.   Driven by a hydroelectric power storage battery, which has a turbine blade cross section (4F) and a turbine blade combustion section (32Y) for hydroelectric power generation by a vertical all blade water turbine with a turbine blade cross section (4F) and includes various types of cooking equipment using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross section (4F) tabine blade (8c) and all-wheel blade impeller water turbine combined unit combustion unit (31X) with hydroelectric power storage battery driven various rotations including various cooking equipment using heat Various energy storage cycle coalescence engine as output drive equipment.   Turbine blade cross section (4F) with tabine blade (8c) and a combined engine combustion section (31Y) for hydroelectric power generation with all blade impeller water turbines and various rotations driven by hydroelectric storage batteries including various cooking equipments using heat Various energy storage cycle coalescence engine as output drive equipment.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and all blade impeller water turbine heating high temperature means (3B) coalescence engine combustion unit (31X) for hydroelectric power generation and various cooking equipment using heat Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   Turbine blade cross section (4E) power generation technology turbine blade (8c) and all blade impeller water turbine heating high temperature means (3B) coalescence engine combustion section (31Y) for hydroelectric power generation and various cooking equipment using heat Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade (8c) of power generation technology with a turbine blade cross-section (4E) and a whole blade combustion section (32X) for heating and heating means (3B) hydroelectric power generation with a vertical all blade water turbine, and various cooking using heat Various energy storage cycle coalescing engines, which are driven by hydroelectric storage batteries and various rotational output drive devices including equipment.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and vertical all blade water turbine with heating high temperature means (3B) all blade combustion section (32Y) for hydroelectric power generation Various energy storage cycle coalescing engines, which are driven by hydroelectric storage batteries and various rotational output drive devices including equipment.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine and water including various cooking equipment using heat Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Water including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, including various cooking equipment and equipment using heat Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Includes turbine blade (8c) with power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31X) for hydrodynamic power generation with reduced friction loss by all blade impeller water turbine, and includes various cooking equipment equipment using heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes turbine blade (8c) with power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31Y) for reducing friction loss with all blade impeller water turbine, and includes various cooking equipment using heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Driven by a hydroelectric power storage battery, including a turbine blade cross section (4F) and a turbine blade combustion section (32X) for hydroelectric power generation by a vertical all blade water turbine with a turbine blade cross section (4F) and various types of hot water equipment Various energy storage cycle coalescing engines as various rotational output drive devices.   A hydropower storage battery drive that includes a turbine blade section (4F) and a turbine blade combustion section (32Y) that generates hydroelectric power using a vertical all blade water turbine with a turbine blade cross section (4F) and includes various types of hot water equipment. Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross section (4F) with tabine blade (8c) and a combined engine combustion section (31X) for hydroelectric power generation with all blade impeller water turbines and various rotations driven by hydroelectric storage batteries including various hot water equipment Various energy storage cycle coalescence engine as output drive equipment.   Turbine blade cross section (4F) with tabine blade (8c) and a combined engine combustion unit (31Y) for hydroelectric power generation with all blade impeller water turbines and various rotations driven by hydroelectric storage batteries including various hot water equipment Various energy storage cycle coalescence engine as output drive equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) that generates hydroelectric power by heating high temperature means (3B) with all blade impeller water turbine. Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for heating and heating means (3B) hydroelectric power generation with all blade impeller water turbines, and various hot water equipment using warm heat Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a hot blade high temperature means (3B) with a vertical blade moving water turbine and a whole blade burning section (32X) for hydroelectric power generation. Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices including equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a heating blade high temperature means (3B) all blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, and various hot water using warm heat Various energy storage cycle coalescing engines, which are driven by hydroelectric storage batteries and various rotational output drive devices including equipment.   Water including a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32X) that performs hydroelectric power generation using a vertical all blade water turbine, including various types of hot water equipment. Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Water including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, including various types of hot water equipment. Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Hydroelectric power storage battery comprising a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) for hydroelectric power generation using a fully-rotor impeller water turbine and various types of hot water equipment. Various energy storage cycle coalescing engines as various rotational output drive devices.   A hydroelectric storage battery including a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation using a fully-rotor impeller water turbine and various types of hot water equipment. Various energy storage cycle coalescing engines as various rotational output drive devices.   Includes turbine blade (8c) of power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31X) for reducing friction loss water generation with all blade impeller water turbine, and includes various hot water facility equipment using heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes a turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31Y) for reducing friction loss water generation with all blade impeller water turbines, including various hot water hot water equipment. Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Driven by a hydroelectric power storage battery, including a turbine blade cross section (4F) and a turbine blade combustion section (32X) for hydroelectric power generation by a vertical all blade water turbine with a turbine blade cross section (4F) and various types of hot water equipment Various energy storage cycle coalescing engines as various rotational output drive devices.   A hydropower storage battery drive that includes a turbine blade section (4F) and a turbine blade combustion section (32Y) that generates hydroelectric power using a vertical all blade water turbine with a turbine blade cross section (4F) and includes various types of hot water equipment. Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross section (4F) with tabine blade (8c) and a combined engine combustion section (31X) for hydroelectric power generation with all blade impeller water turbines and various rotations driven by hydroelectric storage batteries including various hot water equipment Various energy storage cycle coalescence engine as output drive equipment.   Turbine blade cross section (4F) with tabine blade (8c) and a combined engine combustion unit (31Y) for hydroelectric power generation with all blade impeller water turbines and various rotations driven by hydroelectric storage batteries including various hot water equipment Various energy storage cycle coalescence engine as output drive equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) that generates hydroelectric power by heating high temperature means (3B) with all blade impeller water turbine. Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for heating and heating means (3B) hydroelectric power generation with all blade impeller water turbines, and various hot water equipment using warm heat Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a hot blade high temperature means (3B) with a vertical blade moving water turbine and a whole blade burning section (32X) for hydroelectric power generation. Various energy storage cycle coalescing engines, which are driven by hydroelectric storage batteries and various rotational output drive devices including equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a heating blade high temperature means (3B) all blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, and various hot water using warm heat Various energy storage cycle coalescing engines, which are driven by hydroelectric storage batteries and various rotational output drive devices including equipment.   Water including a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32X) that performs hydroelectric power generation using a vertical all blade water turbine, including various types of hot water equipment. Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Water including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, including various types of hot water equipment. Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Hydroelectric power storage battery comprising a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) for hydroelectric power generation using a fully-rotor impeller water turbine and various types of hot water equipment. Various energy storage cycle coalescing engines as various rotational output drive devices.   A hydroelectric storage battery including a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation using a fully-rotor impeller water turbine and various types of hot water equipment. Various energy storage cycle coalescing engines as various rotational output drive devices.   Includes turbine blade (8c) of power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31X) for reducing friction loss water generation with all blade impeller water turbine, and includes various hot water facility equipment using heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes a turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31Y) for reducing friction loss water generation with all blade impeller water turbines, including various hot water hot water equipment. Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   A variety of hydropower storage battery drives including various dishwashers using thermal energy, equipped with a turbine blade section (4F) and a turbine blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine with a turbine blade cross section (4F) Various energy storage cycle coalescing engines as rotary output drive equipment.   A variety of water-powered storage battery drives, including various dishwashers, using a turbine blade section (4F) and a turbine blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines as rotary output drive equipment.   Turbine blade cross section (4F) with tabine blade (8c) and a combined engine combustion section (31X) for hydroelectric power generation with all blade impeller water turbines and various rotational outputs driven by hydroelectric storage batteries including various dishwashers using heat Various energy storage cycle coalescing engines as driving equipment.   Turbine blade cross section (4F) tabine blade (8c) and all-compartment blade bobbin water turbine combined unit combustion unit (31Y) for hydroelectric power generation and various rotational outputs driven by hydroelectric storage battery including various dishwashers using heat Various energy storage cycle coalescing engines as driving equipment.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and all blade impeller water turbine heating high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation, various dishwashers using heat Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and all blade impeller water turbine heating high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation, various dishwashers using heat Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and vertical bladed water turbine heating high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation and various dishwashing using heat Various energy storage cycle coalescing engines for various rotating output drive devices driven by hydroelectric storage batteries including machinery.   Turbine blade cross section (4E), turbine blade (8c) of power generation technology and vertical blade-type all blade water turbine, heating high temperature means (3B) all blade combustion section (32Y) for hydroelectric power generation, and various dishwashing using heat Various energy storage cycle coalescing engines for various rotating output drive devices driven by hydroelectric storage batteries including machinery.   Hydroelectric power generation including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32X) for hydroelectric power generation using a vertical all blade water turbine, including various dishwashers using heat Various energy storage cycle coalescing engine as storage battery driven various rotational output drive equipment.   Hydroelectric power generation including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a full blade combustion section (32Y) for hydroelectric power generation using a vertical all blade water turbine, including various dishwashers using heat Various energy storage cycle coalescing engine as storage battery driven various rotational output drive equipment.   Driven by hydroelectric power storage batteries, including a turbine blade (8c) of power generation technology with a turbine blade cross-section (4E) and a combined engine combustion section (31X) for hydroelectric power generation with a water turbine with all rotor blades, including various dishwashers using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Driven by a hydroelectric storage battery with a turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31Y) that performs hydroelectric power generation with a water turbine with all rotor blades, including various dishwashers using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all-combined blade impeller water turbine with coalescence engine combustion section (31X) for reducing friction loss and water including various dishwashers using heat Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Water including a turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion section (31Y) for generating friction loss hydroelectric power by a fully moving blade propeller water turbine and including various dishwashers using heat Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   A variety of hydropower storage battery drives including various dishwashers using thermal energy, equipped with a turbine blade section (4F) and a turbine blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine with a turbine blade cross section (4F) Various energy storage cycle coalescing engines as rotary output drive equipment.   A variety of water-powered storage battery drives, including various dishwashers, using a turbine blade section (4F) and a turbine blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines as rotary output drive equipment.   Turbine blade cross section (4F) with tabine blade (8c) and a combined engine combustion section (31X) for hydroelectric power generation with all blade impeller water turbines and various rotational outputs driven by hydroelectric storage batteries including various dishwashers using heat Various energy storage cycle coalescing engines as driving equipment.   Turbine blade cross section (4F) tabine blade (8c) and all-compartment blade bobbin water turbine combined unit combustion unit (31Y) for hydroelectric power generation and various rotational outputs driven by hydroelectric storage battery including various dishwashers using heat Various energy storage cycle coalescing engines as driving equipment.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and all blade impeller water turbine heating high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation, various dishwashers using heat Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and all blade impeller water turbine heating high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation, various dishwashers using heat Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and vertical bladed water turbine heating high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation and various dishwashing using heat Various energy storage cycle coalescing engines for various rotating output drive devices driven by hydroelectric storage batteries including machinery.   Turbine blade cross section (4E), turbine blade (8c) of power generation technology and vertical blade-type all blade water turbine, heating high temperature means (3B) all blade combustion section (32Y) for hydroelectric power generation, and various dishwashing using heat Various energy storage cycle coalescing engines for various rotating output drive devices driven by hydroelectric storage batteries including machinery.   Hydroelectric power generation including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32X) for hydroelectric power generation using a vertical all blade water turbine, including various dishwashers using heat Various energy storage cycle coalescing engine as storage battery driven various rotational output drive equipment.   Hydroelectric power generation including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a full blade combustion section (32Y) for hydroelectric power generation using a vertical all blade water turbine, including various dishwashers using heat Various energy storage cycle coalescing engine as storage battery driven various rotational output drive equipment.   Driven by hydroelectric power storage batteries, including a turbine blade (8c) of power generation technology with a turbine blade cross-section (4E) and a combined engine combustion section (31X) for hydroelectric power generation with a water turbine with all rotor blades, including various dishwashers using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Hydroelectric power storage battery drive including various dishwashers using heat, equipped with turbine blade (8c) of power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31Y) for hydroelectric power generation with all blade impeller water turbine Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all-combined blade impeller water turbine with coalescence engine combustion section (31X) for reducing friction loss and water including various dishwashers using heat Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Water including a turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion section (31Y) for generating friction loss hydroelectric power by a fully moving blade propeller water turbine and including various dishwashers using heat Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Driven by a hydroelectric storage battery including a turbine blade cross section (4F) and a turbine blade combustion section (32X) for hydroelectric power generation by a vertical all blade water turbine with a blade section (4F) and various types of washing dryers using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Driven by a hydroelectric storage battery with a turbine blade cross section (4F) and a turbine blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, including various washing dryers using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross section (4F) with tabine blade (8c) and a combined engine combustion section (31X) for hydroelectric power generation with all blade impeller water turbines and various rotations driven by hydroelectric storage batteries including various washing dryers using heat Various energy storage cycle coalescence engine as output drive equipment.   Turbine blade cross section (4F) with tabine blades (8c) and a combined engine combustion unit (31Y) for hydroelectric power generation with all blade impeller water turbines and various rotations driven by hydroelectric storage batteries including various washing dryers using heat Various energy storage cycle coalescence engine as output drive equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined moving unit (31X) for heating and heating means (3B) hydroelectric power generation with a water turbine impeller water turbine. Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation with a heating blade high speed turbine (3B) with all blade impeller water turbines, and various washing dryers using heat Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a full-blade combustion section (32X) for hydroelectric power generation by a heating high-temperature means (3B) by a vertical all-blade water turbine Various energy storage cycle coalescing engines that are driven by hydroelectric storage batteries, including dryers, and various rotational output drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32Y) for hydroelectric power generation with a high temperature heating means (3B) with a vertical all blade water turbine, and various washing using heat Various energy storage cycle coalescing engines that are driven by hydroelectric storage batteries, including dryers, and various rotational output drive devices.   Water including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine, including various washing dryers using heat Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Water including a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, including various washing and drying machines using heat. Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   A hydroelectric storage battery comprising a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) for hydroelectric power generation using a water turbine with all-wheel impeller, and various types of washing dryers using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   A hydroelectric storage battery comprising a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation using a water turbine with all rotor blades, including various types of washing dryers using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Includes turbine blade (8c) with power generation technology with turbine blade cross section (4E) and combined engine combustion section (31X) that generates hydrodynamic power with reduced friction loss with all blade impeller water turbine, and includes various washing dryers using heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes turbine blade (8c) of power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31Y) that reduces friction loss with all blade impeller water turbine and includes various washing dryers using heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Driven by a hydroelectric storage battery including a turbine blade cross section (4F) and a turbine blade combustion section (32X) for hydroelectric power generation by a vertical all blade water turbine with a blade section (4F) and various types of washing dryers using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Driven by a hydroelectric storage battery with a turbine blade cross section (4F) and a turbine blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, including various washing dryers using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross section (4F) with tabine blade (8c) and a combined engine combustion section (31X) for hydroelectric power generation with all blade impeller water turbines and various rotations driven by hydroelectric storage batteries including various washing dryers using heat Various energy storage cycle coalescence engine as output drive equipment.   Turbine blade cross section (4F) with tabine blades (8c) and a combined engine combustion unit (31Y) for hydroelectric power generation with all blade impeller water turbines and various rotations driven by hydroelectric storage batteries including various washing dryers using heat Various energy storage cycle coalescence engine as output drive equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined moving unit (31X) for heating and heating means (3B) hydroelectric power generation with a water turbine impeller water turbine. Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation with a heating blade high speed turbine (3B) with all blade impeller water turbines, and various washing dryers using heat Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a full-blade combustion section (32X) for hydroelectric power generation by a heating high-temperature means (3B) by a vertical all-blade water turbine Various energy storage cycle coalescing engines that are driven by hydroelectric storage batteries, including dryers, and various rotational output drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32Y) for hydroelectric power generation with a high temperature heating means (3B) with a vertical all blade water turbine, and various washing using heat Various energy storage cycle coalescing engines that are driven by hydroelectric storage batteries, including dryers, and various rotational output drive devices.   Water including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine, including various washing dryers using heat Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Water including a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, including various washing and drying machines using heat. Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   A hydroelectric storage battery comprising a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) for hydroelectric power generation using a water turbine with all-wheel impeller, and various types of washing dryers using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   A hydroelectric storage battery comprising a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation using a water turbine with all rotor blades, including various types of washing dryers using heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Includes turbine blade (8c) with power generation technology with turbine blade cross section (4E) and combined engine combustion section (31X) that generates hydrodynamic power with reduced friction loss with all blade impeller water turbine, and includes various washing dryers using heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes turbine blade (8c) of power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31Y) that reduces friction loss with all blade impeller water turbine and includes various washing dryers using heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   A variety of hydroelectric storage battery drives including various hot water piping buildings with a turbine blade cross section (4F), a tabine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation using a vertical all blade water turbine Various energy storage cycle coalescing engines as rotary output drive equipment.   A variety of hydroelectric storage battery drives including various hot water piping buildings with a turbine blade cross section (4F) and a turbine blade combustion section (32Y) for hydroelectric power generation by a vertical all blade water turbine with a turbine blade cross section (4F) Various energy storage cycle coalescing engines as rotary output drive equipment.   Turbine blade cross section (4F) with tabine blade (8c) and a combined engine combustion section (31X) for hydroelectric power generation with all blade impeller water turbines and various rotational outputs driven by hydroelectric storage batteries including various hot water piping buildings Various energy storage cycle coalescing engines as driving equipment.   Turbine blade cross section (4F) with tabine blade (8c) and a combined engine combustion unit (31Y) for hydroelectric power generation with all-wheel impeller water turbines and various rotational outputs driven by hydroelectric storage batteries including various hot water piping buildings Various energy storage cycle coalescing engines as driving equipment.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31X) for hydroelectric power generation with a heating blade high-speed turbine (3B) with all blade impeller water turbines and various hot water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation by a heating high temperature means (3B) with all blade impeller water turbines and various hot water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Turbine blade (8c) of power generation technology with turbine blade cross section (4E) and heating blade high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, and various hot water pipes Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries including buildings.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a heating blade high temperature means (3B) all blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, and various hot water pipes Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries including buildings.   Hydroelectric power generation including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a full blade combustion section (32Y) for hydroelectric power generation using a vertical all blade water turbine and including various hot water piping buildings Various energy storage cycle coalescing engine as storage battery driven various rotational output drive equipment.   Hydroelectric power generation including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a full blade combustion section (32Y) for hydroelectric power generation using a vertical all blade water turbine and including various hot water piping buildings Various energy storage cycle coalescing engine as storage battery driven various rotational output drive equipment.   Driven by a hydroelectric power storage battery with various hot water piping buildings, equipped with a turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation with a fully moving impeller water turbine Various energy storage cycle coalescing engines as various rotational output drive devices.   Driven by a hydroelectric power storage battery with various hot water piping buildings, equipped with a turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation with a fully moving impeller water turbine Various energy storage cycle coalescing engines as various rotational output drive devices.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) that generates friction loss reduced hydroelectric power with a fully moving blade propeller water turbine and water including various hot water piping buildings Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for generating friction loss water power with a full bucket blade water turbine water turbine, including various hot water piping buildings Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   A variety of hydroelectric storage battery drives including various hot water piping buildings with a turbine blade cross section (4F), a tabine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation using a vertical all blade water turbine Various energy storage cycle coalescing engines as rotary output drive equipment.   A variety of hydroelectric storage battery drives including various hot water piping buildings with a turbine blade cross section (4F) and a turbine blade combustion section (32Y) for hydroelectric power generation by a vertical all blade water turbine with a turbine blade cross section (4F) Various energy storage cycle coalescing engines as rotary output drive equipment.   Turbine blade cross section (4F) with tabine blade (8c) and a combined engine combustion section (31X) for hydroelectric power generation with all blade impeller water turbines and various rotational outputs driven by hydroelectric storage batteries including various hot water piping buildings Various energy storage cycle coalescing engines as driving equipment.   Turbine blade cross section (4F) with tabine blade (8c) and a combined engine combustion unit (31Y) for hydroelectric power generation with all-wheel impeller water turbines and various rotational outputs driven by hydroelectric storage batteries including various hot water piping buildings Various energy storage cycle coalescing engines as driving equipment.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31X) for hydroelectric power generation with a heating blade high-speed turbine (3B) with all blade impeller water turbines and various hot water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation by a heating high temperature means (3B) with all blade impeller water turbines and various hot water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Turbine blade (8c) of power generation technology with turbine blade cross section (4E) and heating blade high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, and various hot water pipes Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries including buildings.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a heating blade high temperature means (3B) all blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, and various hot water pipes Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries including buildings.   Hydroelectric power generation including turbine blades (8c) of power generation technology with turbine blade cross section (4E) and full blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, including various hot water piping buildings Various energy storage cycle coalescing engine as storage battery driven various rotational output drive equipment.   Hydroelectric power generation including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a full blade combustion section (32Y) for hydroelectric power generation using a vertical all blade water turbine and including various hot water piping buildings Various energy storage cycle coalescing engine as storage battery driven various rotational output drive equipment.   Hydroelectric power storage battery drive including various hot water piping buildings with a turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31X) for hydroelectric power generation with a fully moving blade impeller water turbine Various energy storage cycle coalescing engines as various rotational output drive devices.   Driven by a hydroelectric power storage battery with various hot water piping buildings, equipped with a turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation with a fully moving impeller water turbine Various energy storage cycle coalescing engines as various rotational output drive devices.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) that generates friction loss reduced hydroelectric power with a fully moving blade propeller water turbine and water including various hot water piping buildings Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for generating friction loss water power with a full bucket blade water turbine water turbine, including various hot water piping buildings Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Driven by a hydroelectric power storage battery, including a turbine blade (8c) having a turbine blade cross section (4F) and a whole blade combustion section (32X) for hydroelectric power generation using a vertical all blade water turbine, including various types of cooling equipment using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   A hydroelectric storage battery drive including a turbine blade (8c) having a turbine blade cross section (4F) and an all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine and including various cooling facility equipment Various energy storage cycle coalescing engines as various rotational output drive devices.   A turbine blade (8c) with a turbine blade cross section (4F) and a combined engine combustion section (31X) for hydroelectric power generation with a fully moving blade propeller water turbine. Various energy storage cycle coalescence engine as output drive equipment.   Turbine blades (8c) with a turbine blade cross section (4F) and a combined engine combustion unit (31Y) for hydroelectric power generation with all-wheel impeller water turbines, various rotations driven by hydroelectric storage batteries including various cooling facility equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31X) for hydroelectric power generation with a high temperature heating means (3B) with all blade impeller water turbines and various cooling equipment using cold heat Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation with a moving blade impeller water turbine, and various cooling equipment using cold heat Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a all-blade combustion section (32X) for hydroelectric power generation with a high temperature heating means (3B) with a vertical all blade water turbine, and various cooling using cold energy Various energy storage cycle coalescing engines, which are driven by hydroelectric storage batteries and various rotational output drive devices including equipment.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and an all-blade combustion section (32Y) for hydroelectric power generation with heating high-temperature means (3B) by a vertical all-blade water turbine and various cooling utilizing cold heat Various energy storage cycle coalescing engines, which are driven by hydroelectric storage batteries and various rotational output drive devices including equipment.   Water including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine, including various cooling equipment using cold energy Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Water including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32Y) for hydroelectric power generation using a vertical all blade water turbine, including various cooling equipment using cold energy Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   A hydroelectric storage battery comprising a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) for hydroelectric power generation using a water turbine with all-wheel impeller, and including various cooling equipment using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   A hydroelectric storage battery including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation using a fully-rotor impeller water turbine and various cooling equipment using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   Includes a turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31X) that reduces friction loss with all-rotor impeller water turbines and includes various cooling equipment using cold energy Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes turbine blade (8c) of power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31Y) that reduces friction loss with all rotor blade propeller water turbine and includes various cooling facility equipment using cold heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   A hydroelectric storage battery drive that includes a turbine blade cross section (4F) and a turbine blade combustion section (32X) that performs hydroelectric power generation with a vertical all-blade water turbine and includes various types of cooling equipment using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   Driven by a hydroelectric power storage battery, including a turbine blade cross section (4F) and a turbine blade combustion section (32Y) for hydroelectric power generation by a vertical all blade water turbine with a turbine blade cross section (4F) and various types of cooling equipment. Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross section (4F) with tabine blade (8c) and all-compartment blade propeller water turbine combined unit combustion section (31X) with hydroelectric power storage battery driven various rotations including various cooling facility equipment Various energy storage cycle coalescence engine as output drive equipment.   Turbine blade cross section (4F) tabine blade (8c) and all-wheel blade impeller water turbine combined unit combustion unit (31Y) for hydroelectric power generation and various types of hydroelectric storage battery driven rotation including various cooling equipment Various energy storage cycle coalescence engine as output drive equipment.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation with a moving blade impeller water turbine, and various cooling equipment using cold heat Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation with a moving blade impeller water turbine, and various cooling equipment using cold heat Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a all-blade combustion section (32X) for hydroelectric power generation with a high temperature heating means (3B) with a vertical all blade water turbine, and various cooling using cold energy Various energy storage cycle coalescing engines, which are driven by hydroelectric storage batteries and various rotational output drive devices including equipment.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and an all-blade combustion section (32Y) for hydroelectric power generation with heating high-temperature means (3B) by a vertical all-blade water turbine and various cooling utilizing cold heat Various energy storage cycle coalescing engines, which are driven by hydroelectric storage batteries and various rotational output drive devices including equipment.   Water including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine, including various cooling equipment using cold energy Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Water including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32Y) for hydroelectric power generation using a vertical all blade water turbine, including various cooling equipment using cold energy Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   A hydroelectric storage battery comprising a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) for hydroelectric power generation using a water turbine with all-wheel impeller, and including various cooling equipment using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   A hydroelectric storage battery including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation using a fully-rotor impeller water turbine and various cooling equipment using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   Includes a turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31X) that reduces friction loss with all-rotor impeller water turbines and includes various cooling equipment using cold energy Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes turbine blade (8c) of power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31Y) that reduces friction loss with all rotor blade propeller water turbine and includes various cooling facility equipment using cold heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Turbine blade cross section (4F) tabine blade (8c) and all blade combustion unit (32X) for hydroelectric power generation with vertical all blade water turbine, and various rotational outputs driven by hydroelectric storage battery including various generators Various energy storage cycle coalescing engines as driving equipment.   Turbine blades (8c) with turbine blade cross section (4F) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine and various rotational outputs driven by hydroelectric storage battery including various generators Various energy storage cycle coalescing engines as driving equipment.   Turbine blade cross section (4F) with tabine blade (8c) and a combined engine combustion section (31X) for hydroelectric power generation with all-wheel impeller water turbines and various rotational output drive devices driven by hydroelectric storage batteries including various generators A variety of energy conservation cycle coalescence engine.   Turbine blade cross section (4F) tabine blade (8c) and all-wheel blade bouncing water turbine combined unit combustion unit (31Y) for hydroelectric power generation, and various rotational output drive devices driven by hydroelectric storage batteries including various generators A variety of energy conservation cycle coalescence engine.   Includes turbine blade (8c) of power generation technology with turbine blade cross-section (4E) and combined engine combustion section (31X) for hydroelectric power generation by heating high temperature means (3B) with all blade impeller water turbine and various generators Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade impeller water turbine with heating high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation, including various generators Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Various generators equipped with a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32X) for hydroelectric power generation by heating high temperature means (3B) with a vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Various generators equipped with a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32Y) for hydroelectric power generation by heating high temperature means (3B) with a vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Turbine blade (8c) with power generation technology with turbine blade cross section (4E) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, driven by hydroelectric storage battery including various generators Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blades (8c) of power generation technology with a turbine blade cross section (4E) and a hydrodynamic power storage battery drive including various generators with a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and a combined engine combustion section (31X) that performs hydroelectric power generation with all-wheel impeller water turbines and various rotations driven by hydroelectric storage batteries including various generators Various energy storage cycle coalescence engine as output drive equipment.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and a combined engine combustion section (31Y) that performs hydroelectric power generation with all blade impeller water turbines and various rotations driven by hydroelectric storage batteries including various generators Various energy storage cycle coalescence engine as output drive equipment.   Turbine blades (8c) of power generation technology with a turbine blade cross section (4E) and a combined-engine combustion section (31X) for reducing friction loss with all blade impeller water turbines and hydroelectric power storage batteries including various generators Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31Y) for reducing friction loss hydroelectric power generation with all blade impeller water turbines, and a hydroelectric storage battery including various generators Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross section (4F) tabine blade (8c) and all blade combustion unit (32X) for hydroelectric power generation with vertical all blade water turbine, and various rotational outputs driven by hydroelectric storage battery including various generators Various energy storage cycle coalescing engines as driving equipment.   Turbine blades (8c) with turbine blade cross section (4F) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine and various rotational outputs driven by hydroelectric storage battery including various generators Various energy storage cycle coalescing engines as driving equipment.   Turbine blade cross section (4F) with tabine blade (8c) and a combined engine combustion section (31X) for hydroelectric power generation with all-wheel impeller water turbines and various rotational output drive devices driven by hydroelectric storage batteries including various generators A variety of energy conservation cycle coalescence engine.   Turbine blade cross section (4F) tabine blade (8c) and all-wheel blade bouncing water turbine combined unit combustion unit (31Y) for hydroelectric power generation, and various rotational output drive devices driven by hydroelectric storage batteries including various generators A variety of energy conservation cycle coalescence engine.   Includes turbine blade (8c) of power generation technology with turbine blade cross-section (4E) and combined engine combustion section (31X) for hydroelectric power generation by heating high temperature means (3B) with all blade impeller water turbine and various generators Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade impeller water turbine with heating high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation, including various generators Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Various generators equipped with a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32X) for hydroelectric power generation by heating high temperature means (3B) with a vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Various generators equipped with a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32Y) for hydroelectric power generation by heating high temperature means (3B) with a vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Turbine blade (8c) with power generation technology with turbine blade cross section (4E) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, driven by hydroelectric storage battery including various generators Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blades (8c) of power generation technology with a turbine blade cross section (4E) and a hydrodynamic power storage battery drive including various generators with a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and a combined engine combustion section (31X) that performs hydroelectric power generation with all-wheel impeller water turbines and various rotations driven by hydroelectric storage batteries including various generators Various energy storage cycle coalescence engine as output drive equipment.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and a combined engine combustion section (31Y) that performs hydroelectric power generation with all blade impeller water turbines and various rotations driven by hydroelectric storage batteries including various generators Various energy storage cycle coalescence engine as output drive equipment.   Turbine blades (8c) of power generation technology with a turbine blade cross section (4E) and a combined-engine combustion section (31X) for reducing friction loss with all blade impeller water turbines and hydroelectric power storage batteries including various generators Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31Y) for reducing friction loss hydroelectric power generation with all blade impeller water turbines, and a hydroelectric storage battery including various generators Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross section (4F) with tabine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as equipment.   A turbine blade cross section (4F) with a tabine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation with a saddle type all blade water turbine. Various energy storage cycle coalescing engines as equipment.   Turbine blade cross section (4F) tabine blade (8c) and all-rotor blade bouncing water turbine combined unit combustion unit (31X) for hydroelectric power generation and various types of rotating power drive devices including various electric motors Various energy conservation cycle coalescing engines.   Turbine blade cross section (4F) tabine blade (8c) and all-wheel blade bobbin water turbine combined unit combustion unit (31Y) for hydroelectric power generation and various types of rotating power drive devices including various electric motors Various energy conservation cycle coalescing engines.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion section (31X) for hydroelectric power generation by a heating blade high speed turbine (3B) with all blade impeller water turbines and water including various electric motors Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation with a heating high-temperature means (3B) water turbine with all blade impeller water turbines, including various electric motors Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32X) for hydroelectric power generation with heating high temperature means (3B) with a vertical all blade water turbine, and various motors Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32Y) for hydroelectric power generation with heating high temperature means (3B) with a vertical all blade water turbine, and various electric motors Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   Turbine blades (8c) with power generation technology with turbine blade cross section (4E) and all blades combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, and various types of hydroelectric storage battery drive including various motors Various energy storage cycle coalescing engines as rotary output drive equipment.   A variety of hydroelectric storage battery drives including various motors, including a turbine blade (8c) of the power generation technology with a turbine blade cross section (4E) and a full blade combustion section (32Y) that performs hydroelectric power generation with a vertical all blade water turbine Various energy storage cycle coalescing engines as rotary output drive equipment.   Turbine blade cross section (4E), turbine blade (8c) of power generation technology, and combined engine combustion section (31X) for hydroelectric power generation with all blade impeller water turbine, various rotational outputs of hydroelectric storage battery drive including various motors Various energy storage cycle coalescing engines as driving equipment.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and a combined engine combustion section (31Y) for hydroelectric power generation with all blade impeller water turbines and various rotational outputs driven by hydroelectric storage batteries including various motors Various energy storage cycle coalescing engines as driving equipment.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and a combined-engine combustion unit (31X) for reducing friction loss hydroelectric power generation with all blade impeller water turbines and driving a hydropower storage battery including various motors Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and a combined engine combustion section (31Y) for reducing friction loss hydroelectric power generation with all blade impeller water turbines and driving a hydroelectric storage battery including various motors Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross section (4F) with tabine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as equipment.   A turbine blade cross section (4F) with a tabine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation with a saddle type all blade water turbine. Various energy storage cycle coalescing engines as equipment.   Turbine blade cross section (4F) tabine blade (8c) and all-rotor blade bouncing water turbine combined unit combustion unit (31X) for hydroelectric power generation and various types of rotating power drive devices including various electric motors Various energy conservation cycle coalescing engines.   Turbine blade cross section (4F) tabine blade (8c) and all-wheel blade bobbin water turbine combined unit combustion unit (31Y) for hydroelectric power generation and various types of rotating power drive devices including various electric motors Various energy conservation cycle coalescing engines.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion section (31X) for hydroelectric power generation by a heating blade high speed turbine (3B) with all blade impeller water turbines and water including various electric motors Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation with a heating high-temperature means (3B) water turbine with all blade impeller water turbines, including various electric motors Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32X) for hydroelectric power generation with heating high temperature means (3B) with a vertical all blade water turbine, and various motors Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32Y) for hydroelectric power generation with heating high temperature means (3B) with a vertical all blade water turbine, and various electric motors Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   Turbine blades (8c) with power generation technology with turbine blade cross section (4E) and all blades combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, and various types of hydroelectric storage battery drive including various motors Various energy storage cycle coalescing engines as rotary output drive equipment.   A variety of hydroelectric storage battery drives including various motors, including a turbine blade (8c) of the power generation technology with a turbine blade cross section (4E) and a full blade combustion section (32Y) that performs hydroelectric power generation with a vertical all blade water turbine Various energy storage cycle coalescing engines as rotary output drive equipment.   Turbine blade cross section (4E), turbine blade (8c) of power generation technology, and combined engine combustion section (31X) for hydroelectric power generation with all blade impeller water turbine, various rotational outputs of hydroelectric storage battery drive including various motors Various energy storage cycle coalescing engines as driving equipment.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and a combined engine combustion section (31Y) for hydroelectric power generation with all blade impeller water turbines and various rotational outputs driven by hydroelectric storage batteries including various motors Various energy storage cycle coalescing engines as driving equipment.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and a combined-engine combustion unit (31X) for reducing friction loss hydroelectric power generation with all blade impeller water turbines and driving a hydropower storage battery including various motors Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and a combined engine combustion section (31Y) for reducing friction loss hydroelectric power generation with all blade impeller water turbines and driving a hydroelectric storage battery including various motors Various energy storage cycle coalescing engines as various rotational output drive devices.   A variety of hydroelectric storage battery drives including various hot water piping greenhouses with a turbine blade cross section (4F) and a turbine blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine with a turbine blade cross section (4F) Various energy storage cycle coalescing engines as rotary output drive equipment.   A variety of hydroelectric storage battery drives including various hot water piping greenhouses, equipped with a turbine blade section (4F) and a turbine blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine with a turbine blade cross section (4F) Various energy storage cycle coalescing engines as rotary output drive equipment.   Turbine blade cross section (4F) tabine blade (8c) and all-combined blade impeller water turbine combined unit combustion unit (31X) with hydroelectric power storage battery driven various rotating outputs including hot water piping greenhouses Various energy storage cycle coalescing engines as driving equipment.   Turbine blade cross section (4F) with tabine blade (8c) and a combined engine combustion unit (31Y) for hydroelectric power generation with all blade impeller water turbines and various rotational outputs driven by hydroelectric storage batteries including various hot water piping greenhouses Various energy storage cycle coalescing engines as driving equipment.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade impeller water turbine, heating high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation, various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion unit (31Y) for hydroelectric power generation with a heating high temperature means (3B) with all blade impeller water turbines and various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Turbine blade (8c) of power generation technology with turbine blade cross section (4E) and heating blade high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, and various hot water pipes Various energy storage cycle coalescing engines for various rotating output drive devices driven by hydroelectric storage batteries including greenhouses.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a heating blade high temperature means (3B) all blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, and various hot water pipes Various energy storage cycle coalescing engines for various rotating output drive devices driven by hydroelectric storage batteries including greenhouses.   Hydroelectric power generation including turbine blades (8c) of power generation technology with turbine blade cross section (4E) and full blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, including various hot water piping greenhouses Various energy storage cycle coalescing engine as storage battery driven various rotational output drive equipment.   Hydroelectric power generation including turbine blades (8c) of the power generation technology with turbine blade cross section (4E) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, including various hot water piping greenhouses Various energy storage cycle coalescing engine as storage battery driven various rotational output drive equipment.   Hydroelectric power storage battery drive including various hot water piping greenhouses, equipped with turbine blade (8c) of power generation technology with turbine blade cross section (4E) and combined engine combustion section (31X) for hydroelectric power generation with all blade impeller water turbine Various energy storage cycle coalescing engines as various rotational output drive devices.   Hydroelectric power storage battery drive including various hot water piping greenhouses, equipped with turbine blade (8c) of power generation technology with turbine blade cross section (4E) and combined engine combustion section (31Y) for hydroelectric power generation with all blade impeller water turbine Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade (8c) with power generation technology with turbine blade cross section (4E) and combined engine combustion section (31Y) for reducing friction loss with all blade impeller water turbine and water including various hot water piping greenhouses Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Turbine blade (8c) with power generation technology with turbine blade cross section (4E) and combined engine combustion section (31Y) for reducing friction loss with all blade impeller water turbine and water including various hot water piping greenhouses Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   A variety of hydroelectric storage battery drives including various hot water piping greenhouses with a turbine blade cross section (4F) and a turbine blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine with a turbine blade cross section (4F) Various energy storage cycle coalescing engines as rotary output drive equipment.   A variety of hydroelectric storage battery drives including various hot water piping greenhouses, equipped with a turbine blade section (4F) and a turbine blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine with a turbine blade cross section (4F) Various energy storage cycle coalescing engines as rotary output drive equipment.   Turbine blade cross section (4F) tabine blade (8c) and all-combined blade impeller water turbine combined unit combustion unit (31X) with hydroelectric power storage battery driven various rotating outputs including hot water piping greenhouses Various energy storage cycle coalescing engines as driving equipment.   Turbine blade cross section (4F) with tabine blade (8c) and a combined engine combustion unit (31Y) for hydroelectric power generation with all blade impeller water turbines and various rotational outputs driven by hydroelectric storage batteries including various hot water piping greenhouses Various energy storage cycle coalescing engines as driving equipment.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade impeller water turbine, heating high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation, various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion unit (31Y) for hydroelectric power generation with a heating high temperature means (3B) with all blade impeller water turbines and various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined high temperature means (3B) combined engine combustion section (32A) for hydroelectric power generation with a vertical all blade water turbine, and various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined high temperature means (3B) combined engine combustion section (32B) for hydroelectric power generation with a vertical all blade water turbine, and various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   Hydroelectric power generation including turbine blades (8c) of power generation technology with turbine blade cross section (4E) and full blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, including various hot water piping greenhouses Various energy storage cycle coalescing engine as storage battery driven various rotational output drive equipment.   Hydroelectric power generation including turbine blades (8c) of the power generation technology with turbine blade cross section (4E) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, including various hot water piping greenhouses Various energy storage cycle coalescing engine as storage battery driven various rotational output drive equipment.   Hydroelectric power storage battery drive including various hot water piping greenhouses, equipped with turbine blade (8c) of power generation technology with turbine blade cross section (4E) and combined engine combustion section (31X) for hydroelectric power generation with all blade impeller water turbine Various energy storage cycle coalescing engines as various rotational output drive devices.   Hydroelectric power storage battery drive including various hot water piping greenhouses, equipped with turbine blade (8c) of power generation technology with turbine blade cross section (4E) and combined engine combustion section (31Y) for hydroelectric power generation with all blade impeller water turbine Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and all-combined blade impeller water turbine combined coal combustion combustion part (31X) for reducing friction loss hydroelectric power, including various hot water piping greenhouses Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Turbine blade (8c) with power generation technology with turbine blade cross section (4E) and combined engine combustion section (31Y) for reducing friction loss with all blade impeller water turbine and water including various hot water piping greenhouses Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   A hydropower storage battery drive including various hot water storage equipment, including a turbine blade cross section (4F), a tabine blade (8c), and a full blade combustion section (32X) for hydroelectric power generation using a vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices.   A hydropower storage battery drive including various hot water storage facilities equipment, including a turbine blade cross section (4F) and a turbine blade combustion section (32Y) for hydroelectric power generation by a vertical all blade water turbine with a turbine blade cross section (4F) Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross section (4F) tabine blade (8c) and all-wheel blade bouncing water turbine combined unit combustion unit (31Y) that performs hydroelectric power generation and various rotations driven by hydroelectric storage battery including various hot water storage equipment Various energy storage cycle coalescence engine as output drive equipment.   Turbine blade cross section (4F) tabine blade (8c) and all-wheel blade bouncing water turbine combined unit combustion unit (31Y) that performs hydroelectric power generation and various rotations driven by hydroelectric storage battery including various hot water storage equipment Various energy storage cycle coalescence engine as output drive equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) for hydroelectric power generation with a heating high-temperature means (3B) with all blade impeller water turbines and various hot water storage equipment Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E), and a combined engine combustion section (31Y) for hydroelectric power generation with a heating high temperature means (3B) with all blade impeller water turbines and various hot water storage equipment Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a full blade combustion section (32Y) for generating hydrothermal power by a high temperature heating means (3B) with a vertical all blade water turbine and various hot water storage Various energy storage cycle coalescing engines, which are driven by hydroelectric storage batteries and various rotational output drive devices including equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a full blade combustion section (32Y) for generating hydrothermal power by a high temperature heating means (3B) with a vertical all blade water turbine and various hot water storage Various energy storage cycle coalescing engines, which are driven by hydroelectric storage batteries and various rotational output drive devices including equipment.   A turbine blade (8c) having a power generation technology with a turbine blade cross section (4E) and a whole blade combustion section (32X) that performs hydroelectric power generation with a vertical all blade water turbine and water including various hot water storage equipment. Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Water including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, including various hot water storage equipment. Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Hydroelectric power storage battery comprising a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) that performs hydroelectric power generation using a fully moving blade impeller water turbine and including various types of hot water storage equipment Various energy storage cycle coalescing engines as various rotational output drive devices.   Hydroelectric power storage battery comprising a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) that performs hydroelectric power generation using a fully moving blade impeller water turbine and including various types of hot water storage equipment Various energy storage cycle coalescing engines as various rotational output drive devices.   Includes turbine blade (8c) with power generation technology with turbine blade cross section (4E) and combined engine combustion section (31X) for generating friction loss reduced water power with all blade impeller water turbines and various hot water storage equipment Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes turbine blade (8c) of power generation technology with turbine blade cross-section (4E) and coalescence engine combustion section (31Y) for reducing friction loss hydroelectric power generation with all blade impeller water turbine, including various hot water storage equipment Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   A hydropower storage battery drive including various hot water storage equipment, including a turbine blade cross section (4F), a tabine blade (8c), and a full blade combustion section (32X) for hydroelectric power generation using a vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices.   A hydropower storage battery drive including various hot water storage facilities equipment, including a turbine blade cross section (4F) and a turbine blade combustion section (32Y) for hydroelectric power generation by a vertical all blade water turbine with a turbine blade cross section (4F) Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross section (4F) tabine blade (8c) and all-compartment blade propeller water turbine combined unit combustion unit (31X) with hydroelectric power generation and various hot water storage battery driven rotations including various hot water storage equipment Various energy storage cycle coalescence engine as output drive equipment.   Turbine blade cross section (4F) tabine blade (8c) and all-wheel blade bouncing water turbine combined unit combustion unit (31Y) that performs hydroelectric power generation and various rotations driven by hydroelectric storage battery including various hot water storage equipment Various energy storage cycle coalescence engine as output drive equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) for hydroelectric power generation with a heating high-temperature means (3B) with all blade impeller water turbines and various hot water storage equipment Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E), and a combined engine combustion section (31Y) for hydroelectric power generation with a heating high temperature means (3B) with all blade impeller water turbines and various hot water storage equipment Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a hot blade high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine, and various hot water storage Various energy storage cycle coalescing engines, which are driven by hydroelectric storage batteries and various rotational output drive devices including equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a full blade combustion section (32Y) for generating hydrothermal power by a high temperature heating means (3B) with a vertical all blade water turbine and various hot water storage Various energy storage cycle coalescing engines, which are driven by hydroelectric storage batteries and various rotational output drive devices including equipment.   A turbine blade (8c) having a power generation technology with a turbine blade cross section (4E) and a whole blade combustion section (32X) that performs hydroelectric power generation with a vertical all blade water turbine and water including various hot water storage equipment. Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Water including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, including various hot water storage equipment. Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Hydroelectric power storage battery comprising a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) that performs hydroelectric power generation using a fully moving blade impeller water turbine and including various types of hot water storage equipment Various energy storage cycle coalescing engines as various rotational output drive devices.   Hydroelectric power storage battery comprising a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) that performs hydroelectric power generation using a fully moving blade impeller water turbine and including various types of hot water storage equipment Various energy storage cycle coalescing engines as various rotational output drive devices.   Includes turbine blade (8c) with power generation technology with turbine blade cross section (4E) and combined engine combustion section (31X) for generating friction loss reduced water power with all blade impeller water turbines and various hot water storage equipment Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes turbine blade (8c) of power generation technology with turbine blade cross-section (4E) and coalescence engine combustion section (31Y) for reducing friction loss hydroelectric power generation with all blade impeller water turbine, including various hot water storage equipment Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   A hydropower storage battery drive including various hot water piping facilities equipment, equipped with a turbine blade cross section (4F) and a turbine blade combustion section (32X) for hydropower generation with a vertical all blade water turbine with a turbine blade cross section (4F) Various energy storage cycle coalescing engines as various rotational output drive devices.   A hydroelectric storage battery drive including various hot water piping facilities and equipment with a turbine blade cross section (4F) and a turbine blade combustion section (32Y) for hydroelectric power generation by a vertical all blade water turbine with a turbine blade cross section (4F) Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross section (4F) tabine blade (8c) and a combined engine combustion unit (31X) for hydroelectric power generation with all-wheel impeller water turbines, various rotations driven by hydroelectric storage batteries including various hot water piping equipment Various energy storage cycle coalescence engine as output drive equipment.   Turbine blade cross section (4F) tabine blade (8c) and all-wheel blade bobbin water turbine combined unit combustion unit (31Y) for hydroelectric power generation and various hot water storage battery driven various rotations including hot water piping equipment Various energy storage cycle coalescence engine as output drive equipment.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and all blade impeller water turbine with heating high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation and various hot water piping equipment Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation with a heating blade high speed turbine (3B) with all blade impeller water turbines and various hot water piping equipment Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   Turbine blade (8c) of power generation technology with turbine blade cross section (4E) and heating blade high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, and various hot water pipes Various energy storage cycle coalescing engines, which are driven by hydroelectric storage batteries and various rotational output drive devices including equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a heating blade high temperature means (3B) all blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, and various hot water pipes Various energy storage cycle coalescing engines, which are driven by hydroelectric storage batteries and various rotational output drive devices including equipment.   A turbine blade (8c) having a power generation technology with a turbine blade cross section (4E) and a whole blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine and water including various hot water piping equipment. Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Water including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, including various hot water piping equipment. Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Hydroelectric power storage battery comprising a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) for hydroelectric power generation with a fully-rotor impeller water turbine, and including various hot water piping equipment Various energy storage cycle coalescing engines as various rotational output drive devices.   A hydroelectric storage battery including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation using a water turbine with all rotor blades, including various types of hot water piping equipment Various energy storage cycle coalescing engines as various rotational output drive devices.   Includes turbine blades (8c) of power generation technology with turbine blade cross section (4E) and coalescence engine combustion part (31X) for reducing friction loss water generation with all blade impeller water turbines, including various hot water piping equipment Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes turbine blade (8c) of power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31Y) for reducing friction loss hydroelectric power generation with all blade impeller water turbine, including various hot water piping equipment Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   A hydropower storage battery drive including various hot water piping facilities equipment, equipped with a turbine blade cross section (4F) and a turbine blade combustion section (32X) for hydropower generation with a vertical all blade water turbine with a turbine blade cross section (4F) Various energy storage cycle coalescing engines as various rotational output drive devices.   A hydroelectric storage battery drive including various hot water piping facilities and equipment with a turbine blade cross section (4F) and a turbine blade combustion section (32Y) for hydroelectric power generation by a vertical all blade water turbine with a turbine blade cross section (4F) Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross section (4F) tabine blade (8c) and a combined engine combustion unit (31X) for hydroelectric power generation with all-wheel impeller water turbines, various rotations driven by hydroelectric storage batteries including various hot water piping equipment Various energy storage cycle coalescence engine as output drive equipment.   Turbine blade cross section (4F) tabine blade (8c) and all-wheel blade bobbin water turbine combined unit combustion unit (31Y) for hydroelectric power generation and various hot water storage battery driven various rotations including hot water piping equipment Various energy storage cycle coalescence engine as output drive equipment.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and all blade impeller water turbine with heating high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation and various hot water piping equipment Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation with a heating blade high speed turbine (3B) with all blade impeller water turbines and various hot water piping equipment Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   Turbine blade (8c) of power generation technology with turbine blade cross section (4E) and heating blade high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, and various hot water pipes Various energy storage cycle coalescing engines, which are driven by hydroelectric storage batteries and various rotational output drive devices including equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a heating blade high temperature means (3B) all blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, and various hot water pipes Various energy storage cycle coalescing engines, which are driven by hydroelectric storage batteries and various rotational output drive devices including equipment.   A turbine blade (8c) having a power generation technology with a turbine blade cross section (4E) and a whole blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine and water including various hot water piping equipment. Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Water including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, including various hot water piping equipment. Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Hydroelectric power storage battery comprising a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) for hydroelectric power generation with a fully-rotor impeller water turbine, and including various hot water piping equipment Various energy storage cycle coalescing engines as various rotational output drive devices.   A hydroelectric storage battery including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation using a water turbine with all rotor blades, including various types of hot water piping equipment Various energy storage cycle coalescing engines as various rotational output drive devices.   Includes turbine blades (8c) of power generation technology with turbine blade cross section (4E) and coalescence engine combustion part (31X) for reducing friction loss water generation with all blade impeller water turbines, including various hot water piping equipment Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes turbine blade (8c) of power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31Y) for reducing friction loss hydroelectric power generation with all blade impeller water turbine, including various hot water piping equipment Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   A variety of hydroelectric storage battery drives including various cold and hot water pipe buildings with a turbine blade cross section (4F) and a turbine blade combustion section (32X) for hydroelectric power generation by a vertical all blade water turbine with a turbine blade cross section (4F) Various energy storage cycle coalescing engines as rotary output drive equipment.   A variety of hydropower storage battery drives including various cold and hot water piping buildings with a turbine blade cross section (4F) and a turbine blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine with a turbine blade cross section (4F) Various energy storage cycle coalescing engines as rotary output drive equipment.   Turbine blade cross section (4F) with tabine blade (8c) and a combined engine combustion section (31X) for hydroelectric power generation with all blade impeller water turbines and various rotational outputs driven by hydroelectric storage batteries including various cold water piping buildings Various energy storage cycle coalescing engines as driving equipment.   Turbine blade cross section (4F) tabine blade (8c) and all-wheel blade bouncing water turbine combined unit combustion unit (31Y) for hydroelectric power generation, and various rotational output of hydroelectric storage battery drive including various cold water piping buildings Various energy storage cycle coalescing engines as driving equipment.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E), and a combined engine combustion section (31X) for hydroelectric power generation with a heating blade high speed turbine (3B) with all blade impeller water turbine, and various cold water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation with a heating blade high speed turbine (3B) with all blade impeller water turbines and various cold and hot water pipe buildings Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a hot blade high temperature means (3B) with a vertical rotor blade water turbine and a whole rotor blade combustion section (32X) for hydroelectric power generation, and various cold water pipes Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries including buildings.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E), and a all-blade combustion section (32Y) for hydroelectric power generation by a heating high temperature means (3B) by a vertical all blade water turbine, and various cold and hot water pipes Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries including buildings.   Hydroelectric power generation including turbine blade (8c) of power generation technology with turbine blade cross section (4E) and full blade combustion section (32X) for hydroelectric power generation using vertical all blade water turbine, including various cold water piping buildings Various energy storage cycle coalescing engine as storage battery driven various rotational output drive equipment.   Hydroelectric power generation including turbine blades (8c) of power generation technology having a turbine blade cross section (4E) and a total blade combustion section (32Y) that performs hydroelectric power generation using a vertical all blade water turbine and including various cold water piping buildings Various energy storage cycle coalescing engine as storage battery driven various rotational output drive equipment.   Hydroelectric power storage battery drive including various cold and hot water pipe buildings with a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) that performs hydroelectric power generation with a water turbine with all rotor blades Various energy storage cycle coalescing engines as various rotational output drive devices.   Driven by a hydroelectric power storage battery that includes a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) that performs hydroelectric power generation using a water turbine with all rotor blades, including various cold water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and a combined engine combustion section (31X) for generating friction loss reduced water power with all blade impeller water turbines and water including various cold water piping buildings Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Water including a turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion section (31Y) that generates friction loss hydroelectric power by all-wheel impeller water turbines and including various cold water piping buildings Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   A variety of hydroelectric storage battery drives including various cold and hot water pipe buildings with a turbine blade cross section (4F) and a turbine blade combustion section (32X) for hydroelectric power generation by a vertical all blade water turbine with a turbine blade cross section (4F) Various energy storage cycle coalescing engines as rotary output drive equipment.   A variety of hydropower storage battery drives including various cold and hot water piping buildings with a turbine blade cross section (4F) and a turbine blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine with a turbine blade cross section (4F) Various energy storage cycle coalescing engines as rotary output drive equipment.   Turbine blade cross section (4F) with tabine blade (8c) and a combined engine combustion section (31X) for hydroelectric power generation with all blade impeller water turbines and various rotational outputs driven by hydroelectric storage batteries including various cold water piping buildings Various energy storage cycle coalescing engines as driving equipment.   Turbine blade cross section (4F) tabine blade (8c) and all-wheel blade bouncing water turbine combined unit combustion unit (31Y) for hydroelectric power generation, and various rotational output of hydroelectric storage battery drive including various cold water piping buildings Various energy storage cycle coalescing engines as driving equipment.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E), and a combined engine combustion section (31X) for hydroelectric power generation with a heating blade high speed turbine (3B) with all blade impeller water turbine, and various cold water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation with a heating blade high speed turbine (3B) with all blade impeller water turbines and various cold and hot water pipe buildings Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a hot blade high temperature means (3B) with a vertical rotor blade water turbine and a whole rotor blade combustion section (32X) for hydroelectric power generation, and various cold water pipes Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries including buildings.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E), and a all-blade combustion section (32Y) for hydroelectric power generation by a heating high temperature means (3B) by a vertical all blade water turbine, and various cold and hot water pipes Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries including buildings.   Hydroelectric power generation including turbine blade (8c) of power generation technology with turbine blade cross section (4E) and full blade combustion section (32X) for hydroelectric power generation using vertical all blade water turbine, including various cold water piping buildings Various energy storage cycle coalescing engine as storage battery driven various rotational output drive equipment.   Hydroelectric power generation including turbine blades (8c) of power generation technology having a turbine blade cross section (4E) and a total blade combustion section (32Y) that performs hydroelectric power generation using a vertical all blade water turbine and including various cold water piping buildings Various energy storage cycle coalescing engine as storage battery driven various rotational output drive equipment.   Hydroelectric power storage battery drive including various cold and hot water pipe buildings with a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) that performs hydroelectric power generation with a water turbine with all rotor blades Various energy storage cycle coalescing engines as various rotational output drive devices.   Driven by a hydroelectric power storage battery that includes a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) that performs hydroelectric power generation using a water turbine with all rotor blades, including various cold water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and a combined engine combustion section (31X) for generating friction loss reduced water power with all blade impeller water turbines and water including various cold water piping buildings Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Water including a turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion section (31Y) that generates friction loss hydroelectric power by all-wheel impeller water turbines and including various cold water piping buildings Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Driven by a hydroelectric power storage battery, which has a turbine blade cross section (4F) and a turbine blade combustion section (32X) for hydroelectric power generation by a vertical all blade water turbine with a turbine blade cross section (4F) and various refrigeration equipment using cold heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Driven by a hydroelectric storage battery including a turbine blade section (4F) and a turbine blade combustion section (32Y) for hydroelectric power generation by a vertical all blade water turbine with a turbine blade cross section (4F) and various refrigeration equipment using cold heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross section (4F) tabine blade (8c) and all-wheel blade bouncing water turbine combined unit combustion unit (31X) for hydroelectric power generation and various rotations driven by hydroelectric storage batteries including various refrigeration equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   Turbine blade cross section (4F) tabine vane (8c) and all-wheel impeller sprocket water turbine combined unit combustion unit (31Y) for hydroelectric power generation and various types of hydroelectric storage battery driven rotation including various refrigeration equipment Various energy storage cycle coalescence engine as output drive equipment.   Various refrigeration equipment using cold heat, comprising a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller water turbine Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   Various refrigeration equipment using cold heat, comprising a turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade (8c) of a power generation technology having a turbine blade cross-section (4E) and a full-blade combustion section (32X) for hydroelectric power generation with heating high temperature means (3B) by a vertical all blade water turbine and various refrigeration utilizing cold heat Various energy storage cycle coalescing engines, which are driven by hydroelectric storage batteries and various rotational output drive devices including equipment.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32Y) for hydroelectric power generation by a high temperature heating means (3B) with a vertical all blade water turbine and various refrigeration utilizing cold heat Various energy storage cycle coalescing engines, which are driven by hydroelectric storage batteries and various rotational output drive devices including equipment.   Various refrigeration equipment using cold heat, comprising a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a full-blade combustion section (32Y) for hydroelectric power generation equipped with a well-known heating high temperature means in a vertical blade-type all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries including devices.   Water including a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32X) for hydroelectric power generation using a vertical all blade water turbine, including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Water including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine and including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   A hydroelectric storage battery comprising a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) for hydroelectric power generation using a full-rotor impeller water turbine and various refrigeration equipment utilizing cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   A hydroelectric storage battery comprising a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation using a water turbine with all rotor blades, and various refrigeration equipment utilizing cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   Includes a turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31X) that reduces friction loss with all blade impeller water turbines and includes various refrigeration equipment using cold heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes turbine blade (8c) with power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31Y) for reducing friction loss with all blade impeller water turbine, and includes various refrigeration equipment using cold energy Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Driven by a hydroelectric power storage battery, which has a turbine blade cross section (4F) and a turbine blade combustion section (32X) for hydroelectric power generation by a vertical all blade water turbine with a turbine blade cross section (4F) and various refrigeration equipment using cold heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Driven by a hydroelectric storage battery including a turbine blade section (4F) and a turbine blade combustion section (32Y) for hydroelectric power generation by a vertical all blade water turbine with a turbine blade cross section (4F) and various refrigeration equipment using cold heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross section (4F) tabine blade (8c) and all-wheel blade bouncing water turbine combined unit combustion unit (31X) for hydroelectric power generation and various rotations driven by hydroelectric storage batteries including various refrigeration equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   Turbine blade cross section (4F) tabine vane (8c) and all-wheel impeller sprocket water turbine combined unit combustion unit (31Y) for hydroelectric power generation and various types of hydroelectric storage battery driven rotation including various refrigeration equipment Various energy storage cycle coalescence engine as output drive equipment.   Various refrigeration equipment using cold heat, comprising a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller water turbine Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   Various refrigeration equipment using cold heat, comprising a turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade (8c) of a power generation technology having a turbine blade cross-section (4E) and a full-blade combustion section (32X) for hydroelectric power generation with heating high temperature means (3B) by a vertical all blade water turbine and various refrigeration utilizing cold heat Various energy storage cycle coalescing engines, which are driven by hydroelectric storage batteries and various rotational output drive devices including equipment.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32Y) for hydroelectric power generation by a high temperature heating means (3B) with a vertical all blade water turbine and various refrigeration utilizing cold heat Various energy storage cycle coalescing engines, which are driven by hydroelectric storage batteries and various rotational output drive devices including equipment.   Water including a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32X) for hydroelectric power generation using a vertical all blade water turbine, including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Water including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine and including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   A hydroelectric storage battery comprising a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) for hydroelectric power generation using a full-rotor impeller water turbine and various refrigeration equipment utilizing cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   A hydroelectric storage battery comprising a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation using a water turbine with all rotor blades, and various refrigeration equipment utilizing cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   Includes a turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31X) that reduces friction loss with all blade impeller water turbines and includes various refrigeration equipment using cold heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes turbine blade (8c) with power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31Y) for reducing friction loss with all blade impeller water turbine, and includes various refrigeration equipment using cold energy Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Various energy storage cycles including various water suction / injection drive equipment including a turbine blade cross section (4F), a tabine blade (8c), and a full blade combustion section (32X) for hydroelectric power generation using a vertical all blade water turbine. Combined organization.   Various energy storage cycles including various water suction / injection drive equipment including a turbine blade section (4F) and a turbine blade section (8c) having a turbine blade cross section (4F) and an all blade combustion section (32Y) for hydroelectric power generation using a vertical all blade water turbine. Combined organization.   Various energy storage cycle coalescence engines with various water suction / injection drive equipment including a turbine blade section (4F) and a combined engine combustion section (31X) for hydroelectric power generation with a water turbine with a turbine blade cross section (4F) .   Various energy storage cycle combined engines including a turbine blade section (4c) and a combined engine combustion section (31Y) that performs hydroelectric power generation using a water turbine with a turbine blade cross section (4F) and various water suction injection drive devices. .   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31X) for hydroelectric power generation with a heating high temperature means (3B) with all blade impeller water turbines and various water suction injection drive devices A variety of energy conservation cycle coalescence engine.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation with a heating high-temperature means (3B) by a full-rotor impeller water turbine and various water suction and injection drive devices A variety of energy conservation cycle coalescence engine.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E), and a full-blade combustion section (32X) for hydroelectric power generation with heating high temperature means (3B) by a vertical all blade water turbine, and various water suction jets Various energy storage cycle coalescing engines as driving equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a full blade combustion unit (32Y) for hydroelectric power generation with a heating high temperature means (3B) by a vertical all blade water turbine and various water suction injections Various energy storage cycle coalescing engines as driving equipment.   Various types of water suction / injection drive devices including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine. Energy conservation cycle coalescence engine.   Various types of water suction / injection drive devices including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine. Energy conservation cycle coalescence engine.   Various types of energy storage, including a turbine blade (8c) of power generation technology with a turbine blade cross-section (4E) and a combined engine combustion section (31X) that performs hydroelectric power generation with a fully moving impeller water turbine and various water suction and injection drive devices Cycle coalescence engine.   Various energy storages including various water suction / injection drive equipment including turbine blade (8c) of power generation technology with turbine blade cross section (4E) and combined engine combustion section (31Y) for hydroelectric power generation with all-wheel impeller water turbine Cycle coalescence engine.   A turbine blade (8c) of the power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31X) for reducing friction loss water power with all blade impeller water turbines and various water suction injection drive devices Various energy conservation cycle coalescence engine.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for reducing friction loss water generation with a fully moving blade propeller water turbine and various water suction injection drive devices. Various energy conservation cycle coalescence engine.   Various energy storage cycles including various water suction / injection drive equipment including a turbine blade cross section (4F), a tabine blade (8c), and a full blade combustion section (32X) for hydroelectric power generation using a vertical all blade water turbine. Combined organization.   Various energy storage cycles including various water suction / injection drive equipment including a turbine blade section (4F) and a turbine blade section (8c) having a turbine blade cross section (4F) and an all blade combustion section (32Y) for hydroelectric power generation using a vertical all blade water turbine. Combined organization.   Various energy storage cycle coalescence engines with various water suction / injection drive equipment including a turbine blade section (4F) and a combined engine combustion section (31X) for hydroelectric power generation with a water turbine with a turbine blade cross section (4F) .   Various energy storage cycle combined engines including a turbine blade section (4c) and a combined engine combustion section (31Y) that performs hydroelectric power generation using a water turbine with a turbine blade cross section (4F) and various water suction injection drive devices. .   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31X) for hydroelectric power generation with a heating high temperature means (3B) with all blade impeller water turbines and various water suction injection drive devices A variety of energy conservation cycle coalescence engine.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation with a heating high-temperature means (3B) by a full-rotor impeller water turbine and various water suction and injection drive devices A variety of energy conservation cycle coalescence engine.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E), and a full-blade combustion section (32X) for hydroelectric power generation with heating high temperature means (3B) by a vertical all blade water turbine, and various water suction jets Various energy storage cycle coalescing engines as driving equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a full blade combustion unit (32Y) for hydroelectric power generation with a heating high temperature means (3B) by a vertical all blade water turbine and various water suction injections Various energy storage cycle coalescing engines as driving equipment.   Various types of water suction / injection drive devices including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine. Energy conservation cycle coalescence engine.   Various types of water suction / injection drive devices including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine. Energy conservation cycle coalescence engine.   Various types of energy storage, including a turbine blade (8c) of power generation technology with a turbine blade cross-section (4E) and a combined engine combustion section (31X) that performs hydroelectric power generation with a fully moving impeller water turbine and various water suction and injection drive devices Cycle coalescence engine.   Various energy storages including various water suction / injection drive equipment including turbine blade (8c) of power generation technology with turbine blade cross section (4E) and combined engine combustion section (31Y) for hydroelectric power generation with all-wheel impeller water turbine Cycle coalescence engine.   A turbine blade (8c) of the power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31X) for reducing friction loss water power with all blade impeller water turbines and various water suction injection drive devices Various energy conservation cycle coalescence engine.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for reducing friction loss water generation with a fully moving blade propeller water turbine and various water suction injection drive devices. Various energy conservation cycle coalescence engine.   Various water suction jets including various heating equipment using thermal energy, with a turbine blade section (4F) and a turbine blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine. Various energy storage cycle coalescing engines as driving equipment.   Various water suction jets including various heating equipment and components using thermal heating, with a turbine blade cross section (4F) and a tabine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine Various energy storage cycle coalescing engines as driving equipment.   Various water suction / injection drive devices including various heating facility devices using thermal energy, including a turbine blade section (4F) and a combined engine combustion section (31X) for hydroelectric power generation using a turbine blade turbine (8F) with a turbine blade cross section (4F) A variety of energy conservation cycle coalescence engine.   Various water suction / injection drive devices including various heating equipment using thermal energy, including a turbine blade section (4F) and a combined engine combustion section (31Y) for hydroelectric power generation using a turbine blade turbine (8F) with a turbine blade cross section (4F) A variety of energy conservation cycle coalescence engine.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) for generating hydroelectric power by heating high temperature means (3B) with all blade impeller water turbines and various heating equipment using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for heating and heating means (3B) hydroelectric power generation with a fully moving blade propeller water turbine, and various heating equipment using warm heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a all-blade combustion section (32X) for hydroelectric power generation with heating high-temperature means (3B) by a vertical all-blade water turbine, and various heating using warm heat Various energy storage cycle coalescing engines as various water suction / injection drive devices including equipment.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E), and a full-blade combustion unit (32Y) for hydroelectric power generation with heating high-temperature means (3B) by a vertical all-blade water turbine, and various heating using warm heat Various energy storage cycle coalescing engines as various water suction / injection drive devices including equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine, and various types of heating equipment using warm heat Various energy storage cycle coalescing engine as water suction jet drive equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and an all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, and various types of heating equipment using various heat sources Various energy storage cycle coalescing engine as water suction jet drive equipment.   A variety of water suction including various heating equipment and components using thermal energy, including a turbine blade (8c) of a power generation technology having a turbine blade cross-section (4E) and a combined engine combustion section (31X) for hydroelectric power generation using a water turbine with all rotor blades Various energy storage cycle coalescing engines as injection drive devices.   A variety of water suction including various heating equipment using thermal energy, including a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation using a water turbine with all rotor blades Various energy storage cycle coalescing engines as injection drive devices.   Includes turbine blade (8c) with power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31X) for hydrodynamic power generation with reduced friction loss by all blade impeller water turbine, including various heating equipment using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Includes turbine blade (8c) with power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31Y) for hydrodynamic power generation with reduced friction loss with all blade impeller water turbine, and includes various heating equipment using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Various water suction jets including various heating equipment using thermal energy, with a turbine blade section (4F) and a turbine blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine. Various energy storage cycle coalescing engines as driving equipment.   Various water suction jets including various heating equipment and components using thermal heating, with a turbine blade cross section (4F) and a tabine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine Various energy storage cycle coalescing engines as driving equipment.   Various water suction / injection drive devices including various heating facility devices using thermal energy, including a turbine blade section (4F) and a combined engine combustion section (31X) for hydroelectric power generation using a turbine blade turbine (8F) with a turbine blade cross section (4F) A variety of energy conservation cycle coalescence engine.   Various water suction / injection drive devices including various heating equipment using thermal energy, including a turbine blade section (4F) and a combined engine combustion section (31Y) for hydroelectric power generation using a turbine blade turbine (8F) with a turbine blade cross section (4F) A variety of energy conservation cycle coalescence engine.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) for generating hydroelectric power by heating high temperature means (3B) with all blade impeller water turbines and various heating equipment using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for heating and heating means (3B) hydroelectric power generation with a fully moving blade propeller water turbine, and various heating equipment using warm heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a all-blade combustion section (32X) for hydroelectric power generation with heating high-temperature means (3B) by a vertical all-blade water turbine, and various heating using warm heat Various energy storage cycle coalescing engines as various water suction / injection drive devices including equipment.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E), and a full-blade combustion unit (32Y) for hydroelectric power generation with heating high-temperature means (3B) by a vertical all-blade water turbine, and various heating using warm heat Various energy storage cycle coalescing engines as various water suction / injection drive devices including equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine, and various types of heating equipment using warm heat Various energy storage cycle coalescing engine as water suction jet drive equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and an all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, and various types of heating equipment using various heat sources Various energy storage cycle coalescing engine as water suction jet drive equipment.   A variety of water suction including various heating equipment and components using thermal energy, including a turbine blade (8c) of a power generation technology having a turbine blade cross-section (4E) and a combined engine combustion section (31X) for hydroelectric power generation using a water turbine with all rotor blades Various energy storage cycle coalescing engines as injection drive devices.   A variety of water suction including various heating equipment using thermal energy, including a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation using a water turbine with all rotor blades Various energy storage cycle coalescing engines as injection drive devices.   Includes turbine blade (8c) with power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31X) for hydrodynamic power generation with reduced friction loss by all blade impeller water turbine, including various heating equipment using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Includes turbine blade (8c) with power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31Y) for hydrodynamic power generation with reduced friction loss with all blade impeller water turbine, and includes various heating equipment using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Turbine blade cross section (4F) tabine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section (79K) various air suction injection drive equipment A variety of energy conservation cycle coalescence engine.   Turbine blade cross section (4F) tabine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section (79K) various air suction injection drive equipment A variety of energy conservation cycle coalescence engine.   The turbine blade cross section (4F) has a tabine blade (8c) and a combined engine combustion section (31X) for hydroelectric power generation using a fully moving impeller turbine, and a combined engine injection section (79K), various air suction injection drive devices, Various energy conservation cycle coalescence engine.   The turbine blade section (4F) has a tabine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation with a fully moving blade spring turbine water turbine, and a combined engine injection section (79K) with various air suction injection drive devices, Various energy conservation cycle coalescence engine.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion unit (31X) for hydroelectric power generation by a heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection unit (79K) ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation by heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection section (79K) ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and vertical all blade water turbine heating high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a heating and high-temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and all blade combustion section (32X) generating hydroelectric power with vertical all blade water turbine, combined engine injection section (79K) various air suction Various energy storage cycle coalescing engines as injection drive devices.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section (79K) various air suction Various energy storage cycle coalescing engines as injection drive devices.   The turbine blade cross section (4E) has a turbine blade (8c) of power generation technology and a combined engine combustion section (31X) that performs hydroelectric power generation with a fully-rotor impeller water turbine, and includes a combined engine injection section (79K) and various air suction injection drives Various energy storage cycle coalescing engines as equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion unit (31Y) that performs hydroelectric power generation with a fully-rotated blade impeller water turbine and a combined engine injection unit (79K) various air suction injection drives Various energy storage cycle coalescing engines as equipment.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and a combined engine combustion section (31X) that generates friction loss reduced water generation with all blade impeller water turbines, combined engine injection section (79K) various air Various energy storage cycle coalescing engines as suction injection drive devices.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all-combined blade impeller water turbine with combined engine combustion section (31Y) for reducing friction loss hydroelectric power and combined engine injection section (79K) various air Various energy storage cycle coalescing engines as suction injection drive devices.   Turbine blade cross section (4F) tabine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section (79K) various air suction injection drive equipment A variety of energy conservation cycle coalescence engine.   Turbine blade cross section (4F) tabine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section (79K) various air suction injection drive equipment A variety of energy conservation cycle coalescence engine.   The turbine blade cross section (4F) has a tabine blade (8c) and a combined engine combustion section (31X) for hydroelectric power generation using a fully moving impeller turbine, and a combined engine injection section (79K), various air suction injection drive devices, Various energy conservation cycle coalescence engine.   The turbine blade section (4F) has a tabine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation with a fully moving blade spring turbine water turbine, and a combined engine injection section (79K) with various air suction injection drive devices, Various energy conservation cycle coalescence engine.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion unit (31X) for hydroelectric power generation by a heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection unit (79K) ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation by heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection section (79K) ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and vertical all blade water turbine heating high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a heating and high-temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and all blade combustion section (32X) generating hydroelectric power with vertical all blade water turbine, combined engine injection section (79K) various air suction Various energy storage cycle coalescing engines as injection drive devices.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section (79K) various air suction Various energy storage cycle coalescing engines as injection drive devices.   The turbine blade cross section (4E) has a turbine blade (8c) of power generation technology and a combined engine combustion section (31X) that performs hydroelectric power generation with a fully-rotor impeller water turbine, and includes a combined engine injection section (79K) and various air suction injection drives Various energy storage cycle coalescing engines as equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion unit (31Y) that performs hydroelectric power generation with a fully-rotated blade impeller water turbine and a combined engine injection unit (79K) various air suction injection drives Various energy storage cycle coalescing engines as equipment.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and a combined engine combustion section (31X) that generates friction loss reduced water generation with all blade impeller water turbines, combined engine injection section (79K) various air Various energy storage cycle coalescing engines as suction injection drive devices.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all-combined blade impeller water turbine with combined engine combustion section (31Y) for reducing friction loss hydroelectric power and combined engine injection section (79K) various air Various energy storage cycle coalescing engines as suction injection drive devices.   Turbine blade cross section (4F) tabine blade (8c) and all blade combustion unit (32X) for hydroelectric power generation with vertical all blade water turbine, and combined engine injection section including various heating equipment (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4F) with a turbine blade (8c) and an all-blade combustion section (32Y) for hydroelectric power generation using a vertical all-blade water turbine, and a combined engine injection section including various types of heating equipment using heat (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section (79K) that includes a turbine blade cross section (4F) and a combined engine combustion section (31X) that generates hydroelectric power with a turbine blade turbine and a turbine blade turbine (31K), and includes various types of heating equipment. ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Combined engine injection part (79K) including various heating equipment using thermal energy, comprising a turbine blade section (4F) and a combined engine combustion part (31Y) for hydroelectric power generation using a turbine blade turbine (8F) and a turbine blade turbine. ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) for generating hydroelectric power by heating high temperature means (3B) with all blade impeller water turbines and various heating equipment using heat Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for heating and heating means (3B) hydroelectric power generation with a fully moving blade propeller water turbine, and various heating equipment using warm heat Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a all-blade combustion section (32X) for hydroelectric power generation with heating high-temperature means (3B) by a vertical all-blade water turbine, and various heating using warm heat Combined engine injection unit (79K) including equipment and equipment Various energy storage cycle combined engines as various air suction injection drive equipment.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E), and a full-blade combustion unit (32Y) for hydroelectric power generation with heating high-temperature means (3B) by a vertical all-blade water turbine, and various heating using warm heat Combined engine injection unit (79K) including equipment and equipment Various energy storage cycle combined engines as various air suction injection drive equipment.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, combined with various heating equipment using heat Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blade (8c) of power generation technology with turbine blade cross section (4E) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, combined with various heating equipment using heat Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) that performs hydroelectric power generation with a fully moving blade impeller water turbine, including various types of heating equipment using heat (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation with a full-rotor impeller water turbine, including various heating equipments using heat (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Includes turbine blade (8c) with power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31X) for hydrodynamic power generation with reduced friction loss by all blade impeller water turbine, including various heating equipment using heat Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Includes turbine blade (8c) with power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31Y) for hydrodynamic power generation with reduced friction loss with all blade impeller water turbine, and includes various heating equipment using heat Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross section (4F) tabine blade (8c) and all blade combustion unit (32X) for hydroelectric power generation with vertical all blade water turbine, and combined engine injection section including various heating equipment (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4F) with a turbine blade (8c) and an all-blade combustion section (32Y) for hydroelectric power generation using a vertical all-blade water turbine, and a combined engine injection section including various types of heating equipment using heat (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section (79K) that includes a turbine blade cross section (4F) and a combined engine combustion section (31X) that generates hydroelectric power with a turbine blade turbine and a turbine blade turbine (31K), and includes various types of heating equipment. ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Combined engine injection part (79K) including various heating equipment using thermal energy, comprising a turbine blade section (4F) and a combined engine combustion part (31Y) for hydroelectric power generation using a turbine blade turbine (8F) and a turbine blade turbine. ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) for generating hydroelectric power by heating high temperature means (3B) with all blade impeller water turbines and various heating equipment using heat Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for heating and heating means (3B) hydroelectric power generation with a fully moving blade propeller water turbine, and various heating equipment using warm heat Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a all-blade combustion section (32X) for hydroelectric power generation with heating high-temperature means (3B) by a vertical all-blade water turbine, and various heating using warm heat Combined engine injection unit (79K) including equipment and equipment Various energy storage cycle combined engines as various air suction injection drive equipment.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E), and a full-blade combustion unit (32Y) for hydroelectric power generation with heating high-temperature means (3B) by a vertical all-blade water turbine, and various heating using warm heat Combined engine injection unit (79K) including equipment and equipment Various energy storage cycle combined engines as various air suction injection drive equipment.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, combined with various heating equipment using heat Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blade (8c) of power generation technology with turbine blade cross section (4E) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, combined with various heating equipment using heat Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) that performs hydroelectric power generation with a fully moving blade impeller water turbine, including various types of heating equipment using heat (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation with a full-rotor impeller water turbine, including various heating equipments using heat (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Includes turbine blade (8c) with power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31X) for hydrodynamic power generation with reduced friction loss by all blade impeller water turbine, including various heating equipment using heat Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Includes turbine blade (8c) with power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31Y) for hydrodynamic power generation with reduced friction loss with all blade impeller water turbine, and includes various heating equipment using heat Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Combined engine injection section (79K) including a turbine blade section (4F) and a turbine blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine, including various generators Various energy storage cycle coalescing engines as various air suction jet drive devices.   Combined engine injection section (79K) including a turbine blade section (4F) and a turbine blade combustion section (32Y) for hydroelectric power generation by a vertical all blade water turbine with a turbine blade cross section (4F) and including various generators Various energy storage cycle coalescing engines as various air suction jet drive devices.   Combined engine injection section (79K) with various generators, including a combined engine combustion section (31X) for hydroelectric power generation with a turbine blade cross section (4F) and a turbine blade turbine (8C) and a turbine blade turbine. Various energy storage cycle coalescing engines as suction injection drive devices.   Combined engine injection unit (79K) with various generators including a combined engine combustion unit (31Y) for hydroelectric power generation with a turbine blade cross section (4F) and a turbine blade turbine (8c) and a full blade impeller water turbine Various energy storage cycle coalescing engines as suction injection drive devices.   Includes turbine blade (8c) of power generation technology with turbine blade cross-section (4E) and combined engine combustion section (31X) for hydroelectric power generation by heating high temperature means (3B) with all blade impeller water turbine and various generators Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade impeller water turbine with heating high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation, including various generators Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Various generators equipped with a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32X) for hydroelectric power generation by heating high temperature means (3B) with a vertical all blade water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Various generators equipped with a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32Y) for hydroelectric power generation by heating high temperature means (3B) with a vertical all blade water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blades (8c) of power generation technology having a turbine blade cross section (4E) and a full blade combustion unit (32X) for hydroelectric power generation with a vertical all blade water turbine, and a combined engine injection unit including various generators (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and full blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section including various generators (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection unit (79K) including various generators, including a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined engine combustion unit (31X) for hydroelectric power generation with a fully moving blade impeller water turbine ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Combined engine injection unit (79K) including various generators, including a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined engine combustion unit (31Y) for hydroelectric power generation with a fully-rotor impeller water turbine ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Combined engine injection including various generators with a turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31X) for reducing friction loss hydroelectric power generation with all blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including various generators with a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for reducing friction loss hydroelectric power generation with all blade impeller water turbines (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section (79K) including a turbine blade section (4F) and a turbine blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine, including various generators Various energy storage cycle coalescing engines as various air suction jet drive devices.   Combined engine injection section (79K) including a turbine blade section (4F) and a turbine blade combustion section (32Y) for hydroelectric power generation by a vertical all blade water turbine with a turbine blade cross section (4F) and including various generators Various energy storage cycle coalescing engines as various air suction jet drive devices.   Combined engine injection section (79K) with various generators, including a combined engine combustion section (31X) for hydroelectric power generation with a turbine blade cross section (4F) and a turbine blade turbine (8C) and a turbine blade turbine. Various energy storage cycle coalescing engines as suction injection drive devices.   Combined engine injection unit (79K) with various generators including a combined engine combustion unit (31Y) for hydroelectric power generation with a turbine blade cross section (4F) and a turbine blade turbine (8c) and a full blade impeller water turbine Various energy storage cycle coalescing engines as suction injection drive devices.   Includes turbine blade (8c) of power generation technology with turbine blade cross-section (4E) and combined engine combustion section (31X) for hydroelectric power generation by heating high temperature means (3B) with all blade impeller water turbine and various generators Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade impeller water turbine with heating high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation, including various generators Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Various generators equipped with a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32X) for hydroelectric power generation by heating high temperature means (3B) with a vertical all blade water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Various generators equipped with a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32Y) for hydroelectric power generation by heating high temperature means (3B) with a vertical all blade water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blades (8c) of power generation technology having a turbine blade cross section (4E) and a full blade combustion unit (32X) for hydroelectric power generation with a vertical all blade water turbine, and a combined engine injection unit including various generators (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and full blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section including various generators (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection unit (79K) including various generators, including a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined engine combustion unit (31X) for hydroelectric power generation with a fully moving blade impeller water turbine ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Combined engine injection unit (79K) including various generators, including a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined engine combustion unit (31Y) for hydroelectric power generation with a fully-rotor impeller water turbine ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Combined engine injection including various generators with a turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31X) for reducing friction loss hydroelectric power generation with all blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including various generators with a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for reducing friction loss hydroelectric power generation with all blade impeller water turbines (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Various types of combined engine injection parts (79K) including various electric motors having a turbine blade cross section (4F), a tabine blade (8c) and a whole blade combustion part (32X) for hydroelectric power generation using a vertical all-blade water turbine Various energy storage cycle coalescing engine as air suction jet drive equipment.   Various types of combined engine injection parts (79K) including various electric motors including a turbine blade cross section (4F), a tabine blade (8c) and a whole blade combustion section (32Y) for hydroelectric power generation using a vertical all-blade water turbine Various energy storage cycle coalescing engine as air suction jet drive equipment.   Combined engine injection unit (79K) with various motors equipped with combined engine combustion unit (31X) for hydroelectric power generation with turbine blade cross section (4F) and turbine blade turbine (8c) and all blade impeller water turbine Various energy storage cycle coalescing engines as injection drive devices.   Combined engine injection unit (79K) with various motors equipped with a combined engine combustion unit (31Y) for hydroelectric power generation with a turbine blade cross section (4F) and a turbine blade turbine (8c) and hydrodynamic power generation with all turbine blades Various energy storage cycle coalescing engines as injection drive devices.   Turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) for generating hydroelectric power by heating high temperature means (3B) with all blade impeller water turbines and combining various motors Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation by a heating high temperature means (3B) water turbine with all blade impeller water turbines, including various electric motors Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32X) for hydroelectric power generation with heating high temperature means (3B) with a vertical all blade water turbine, and various motors Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32Y) for hydroelectric power generation with heating high temperature means (3B) with a vertical all blade water turbine, and various electric motors Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross section (4E) and a turbine blade (8c) of power generation technology and a full blade combustion portion (32X) for hydroelectric power generation using a vertical all blade water turbine, and a combined engine injection section including various motors ( 79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4E) and a turbine blade (8c) of a power generation technology and a full blade combustion portion (32Y) for hydroelectric power generation with a vertical all blade water turbine, and a combined engine injection section including various motors ( 79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section (79K) including various electric motors, including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) that performs hydroelectric power generation with a fully moving impeller water turbine Various energy storage cycle coalescing engines as various air suction jet drive devices.   Combined engine injection unit (79K) including various electric motors, including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion unit (31Y) for hydroelectric power generation with a fully moving blade impeller water turbine Various energy storage cycle coalescing engines as various air suction jet drive devices.   Combined engine injection unit including various motors, including a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined engine combustion unit (31X) for reducing friction loss water generation with a full-rotor impeller water turbine. (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section including various electric motors, including a turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion section (31Y) for reducing friction loss water generation with a fully-rotor impeller water turbine. (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Various types of combined engine injection parts (79K) including various electric motors having a turbine blade cross section (4F), a tabine blade (8c) and a whole blade combustion part (32X) for hydroelectric power generation using a vertical all-blade water turbine Various energy storage cycle coalescing engine as air suction jet drive equipment.   Various types of combined engine injection parts (79K) including various electric motors including a turbine blade cross section (4F), a tabine blade (8c) and a whole blade combustion section (32Y) for hydroelectric power generation using a vertical all-blade water turbine Various energy storage cycle coalescing engine as air suction jet drive equipment.   Combined engine injection unit (79K) with various motors equipped with combined engine combustion unit (31X) for hydroelectric power generation with turbine blade cross section (4F) and turbine blade turbine (8c) and all blade impeller water turbine Various energy storage cycle coalescing engines as injection drive devices.   Combined engine injection unit (79K) with various motors equipped with a combined engine combustion unit (31Y) for hydroelectric power generation with a turbine blade cross section (4F) and a turbine blade turbine (8c) and hydrodynamic power generation with all turbine blades Various energy storage cycle coalescing engines as injection drive devices.   Turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) for generating hydroelectric power by heating high temperature means (3B) with all blade impeller water turbines and combining various motors Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation by a heating high temperature means (3B) water turbine with all blade impeller water turbines, including various electric motors Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32X) for hydroelectric power generation with heating high temperature means (3B) with a vertical all blade water turbine, and various motors Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32Y) for hydroelectric power generation with heating high temperature means (3B) with a vertical all blade water turbine, and various electric motors Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross section (4E) and a turbine blade (8c) of power generation technology and a full blade combustion portion (32X) for hydroelectric power generation using a vertical all blade water turbine, and a combined engine injection section including various motors ( 79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4E) and a turbine blade (8c) of a power generation technology and a full blade combustion portion (32Y) for hydroelectric power generation with a vertical all blade water turbine, and a combined engine injection section including various motors ( 79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section (79K) including various electric motors, including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) that performs hydroelectric power generation with a fully moving impeller water turbine Various energy storage cycle coalescing engines as various air suction jet drive devices.   Combined engine injection unit (79K) including various electric motors, including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion unit (31Y) for hydroelectric power generation with a fully moving blade impeller water turbine Various energy storage cycle coalescing engines as various air suction jet drive devices.   Combined engine injection unit including various motors, including a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined engine combustion unit (31X) for reducing friction loss water generation with a full-rotor impeller water turbine. (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section including various electric motors, including a turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion section (31Y) for reducing friction loss water generation with a fully-rotor impeller water turbine. (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4F) tabine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section including various hot water storage equipment (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4F) with a turbine blade (8c) and an all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine and a combined engine injection section including various types of hot water storage equipment (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection unit (79K) including various hot water storage facilities and equipment, including a combined turbine combustion unit (31X) for hydropower generation with a turbine blade cross section (4F) and a turbine blade turbine 8 ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Combined engine injection unit (79K) including various hot water storage facilities and equipment, including a combined turbine combustion unit (31Y) for hydroelectric power generation using a turbine blade cross section (4F) and a turbine blade blade (8c) and an all blade impeller water turbine ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) for hydroelectric power generation with a heating high-temperature means (3B) with all blade impeller water turbines and various hot water storage equipment Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E), and a combined engine combustion section (31Y) for hydroelectric power generation with a heating high temperature means (3B) with all blade impeller water turbines and various hot water storage equipment Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a hot blade high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine, and various hot water storage Combined engine injection unit (79K) including equipment and equipment Various energy storage cycle combined engines as various air suction injection drive equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a full blade combustion section (32Y) for generating hydrothermal power by a high temperature heating means (3B) with a vertical all blade water turbine and various hot water storage Combined engine injection unit (79K) including equipment and equipment Various energy storage cycle combined engines as various air suction injection drive equipment.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, combined with various hot water storage equipment Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and all blade combustion section (32Y) that performs hydroelectric power generation with vertical all blade water turbine, including various hot water storage equipment Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) for hydroelectric power generation with a fully moving impeller water turbine, including various hot water storage equipment (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation with a fully moving impeller water turbine, including various hot water storage equipment (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Includes turbine blade (8c) with power generation technology with turbine blade cross section (4E) and combined engine combustion section (31X) for generating friction loss reduced water power with all blade impeller water turbines and various hot water storage equipment Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Includes turbine blade (8c) of power generation technology with turbine blade cross-section (4E) and coalescence engine combustion section (31Y) for reducing friction loss hydroelectric power generation with all blade impeller water turbine, including various hot water storage equipment Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross section (4F) tabine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section including various hot water storage equipment (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4F) with a turbine blade (8c) and an all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine and a combined engine injection section including various types of hot water storage equipment (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection unit (79K) including various hot water storage facilities and equipment, including a combined turbine combustion unit (31X) for hydropower generation with a turbine blade cross section (4F) and a turbine blade turbine 8 ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Combined engine injection unit (79K) including various hot water storage facilities and equipment, including a combined turbine combustion unit (31Y) for hydroelectric power generation using a turbine blade cross section (4F) and a turbine blade blade (8c) and an all blade impeller water turbine ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) for hydroelectric power generation with a heating high-temperature means (3B) with all blade impeller water turbines and various hot water storage equipment Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E), and a combined engine combustion section (31Y) for hydroelectric power generation with a heating high temperature means (3B) with all blade impeller water turbines and various hot water storage equipment Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a hot blade high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine, and various hot water storage Combined engine injection unit (79K) including equipment and equipment Various energy storage cycle combined engines as various air suction injection drive equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a full blade combustion section (32Y) for generating hydrothermal power by a high temperature heating means (3B) with a vertical all blade water turbine and various hot water storage Combined engine injection unit (79K) including equipment and equipment Various energy storage cycle combined engines as various air suction injection drive equipment.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, combined with various hot water storage equipment Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and all blade combustion section (32Y) that performs hydroelectric power generation with vertical all blade water turbine, including various hot water storage equipment Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) for hydroelectric power generation with a fully moving impeller water turbine, including various hot water storage equipment (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation with a fully moving impeller water turbine, including various hot water storage equipment (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Includes turbine blade (8c) with power generation technology with turbine blade cross section (4E) and combined engine combustion section (31X) for generating friction loss reduced water power with all blade impeller water turbines and various hot water storage equipment Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Includes turbine blade (8c) of power generation technology with turbine blade cross-section (4E) and coalescence engine combustion section (31Y) for reducing friction loss hydroelectric power generation with all blade impeller water turbine, including various hot water storage equipment Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross section (4F) tabine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section including flying around Mach 28 in space (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection part including a turbine blade cross section (4F) and a turbine blade combustion part (32Y) for hydroelectric power generation by a vertical all-blade water turbine with a turbine blade cross section (4F) and including flying around the Mach 28 (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   A combined engine injection section (79K) including a turbine blade section (4F) and a combined engine combustion section (31X) for hydroelectric power generation with a turbine blade turbine water turbine with a turbine blade cross section (4F) and flying around the Mach 28 ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Combined engine injection unit (79K) including a turbine blade cross section (4F) and a combined engine combustion unit (31Y) for hydroelectric power generation with a full turbine impeller water turbine with a turbine blade cross section (4F) including flying around the Mach 28 ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller water turbine, and the space around Mach 28 Combined engine injection unit including flight (79K) Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine, and the universe around Mach 28 Combined engine injection unit including flight (79K) Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a full blade combustion unit (32X) for hydroelectric power generation with a heating high temperature means (3B) by a vertical all blade water turbine, and Mach 28 Combined engine injection part (79K) including flying before and after various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a full-blade combustion section (32Y) for hydroelectric power generation using a vertical all-blade water turbine and a high temperature heating means (3B) hydroelectric power is provided. Combined engine injection part (79K) including flying before and after various energy storage cycle combined engine as various air suction injection drive devices.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all-blade water turbine, including space flight around Mach 28 Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, including spacecraft flying around Mach 28 Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection including a turbine blade (8c) of the power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31X) that hydroelectrically generates power with a full moving blade impeller water turbine, including flying around the Mach 28 in space. (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including a turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation with a fully moving blade impeller water turbine, including flight in and around Mach 28 (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Includes a turbine blade (8c) of power generation technology with a turbine blade cross-section (4E) and a combined engine combustion section (31X) that reduces friction loss with a fully moving blade impeller water turbine and includes flying around the universe around Mach 28 Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Includes a turbine blade (8c) of power generation technology with a turbine blade cross-section (4E) and a combined engine combustion section (31Y) that reduces friction loss with all-rotor impeller water turbines and includes a flight around Mach 28 in space. Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross section (4F) tabine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section including flying around Mach 28 in space (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection part including a turbine blade cross section (4F) and a turbine blade combustion part (32Y) for hydroelectric power generation by a vertical all-blade water turbine with a turbine blade cross section (4F) and including flying around the Mach 28 (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   A combined engine injection section (79K) including a turbine blade section (4F) and a combined engine combustion section (31X) for hydroelectric power generation with a turbine blade turbine water turbine with a turbine blade cross section (4F) and flying around the Mach 28 ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Combined engine injection unit (79K) including a turbine blade cross section (4F) and a combined engine combustion unit (31Y) for hydroelectric power generation with a full turbine impeller water turbine with a turbine blade cross section (4F) including flying around the Mach 28 ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller water turbine, and the space around Mach 28 Combined engine injection unit including flight (79K) Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine, and the universe around Mach 28 Combined engine injection unit including flight (79K) Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a full blade combustion unit (32X) for hydroelectric power generation with a heating high temperature means (3B) by a vertical all blade water turbine, and Mach 28 Combined engine injection part (79K) including flying before and after various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a full-blade combustion section (32Y) for hydroelectric power generation using a vertical all-blade water turbine and a high temperature heating means (3B) hydroelectric power is provided. Combined engine injection part (79K) including flying before and after various energy storage cycle combined engine as various air suction injection drive devices.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all-blade water turbine, including space flight around Mach 28 Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, including spacecraft flying around Mach 28 Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection including a turbine blade (8c) of the power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31X) that hydroelectrically generates power with a full moving blade impeller water turbine, including flying around the Mach 28 in space. (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including a turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation with a fully moving blade impeller water turbine, including flight in and around Mach 28 (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Includes a turbine blade (8c) of power generation technology with a turbine blade cross-section (4E) and a combined engine combustion section (31X) that reduces friction loss with a fully moving blade impeller water turbine and includes flying around the universe around Mach 28 Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Includes a turbine blade (8c) of power generation technology with a turbine blade cross-section (4E) and a combined engine combustion section (31Y) that reduces friction loss with all-rotor impeller water turbines and includes a flight around Mach 28 in space. Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross section (4F) tabine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section including various cold storage equipment (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4F) tabine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section including various refrigeration equipment using cold energy (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section (79K) including a turbine blade section (4F) and a combined engine combustion section (31X) for hydroelectric power generation using a turbine blade turbine with a turbine blade cross section (4F) and various refrigeration equipment using cold heat ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Combined engine injection unit (79K) that includes a turbine blade cross section (4F) and a combined engine combustion unit (31Y) that generates hydroelectric power with a turbine blade turbine and a turbine blade turbine (31Y) and includes various refrigeration equipment using cold energy ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation with all-wheel impeller water turbines and various refrigeration equipment utilizing cold energy Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation with a fully moving blade impeller water turbine, and various refrigeration equipment using cold energy Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32X) for hydroelectric power generation with heating high temperature means (3B) by a vertical all blade water turbine, and various cold storage using cold energy Combined engine injection unit (79K) including equipment and equipment Various energy storage cycle combined engines as various air suction injection drive equipment.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a all-blade combustion section (32Y) for hydroelectric power generation by a high temperature heating means (3B) with a vertical all blade water turbine and various cold storage using cold energy Combined engine injection unit (79K) including equipment and equipment Various energy storage cycle combined engines as various air suction injection drive equipment.   Combined with a turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine, including various refrigeration equipment using cold energy Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined with a turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, including various refrigeration equipment using cold energy Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection including a turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31X) for hydroelectric power generation with a fully-rotor impeller water turbine, including various refrigeration equipment using cold energy (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation with a fully-rotor impeller water turbine and including various refrigeration equipment using cold energy (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Includes turbine blade (8c) with power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31X) for hydrodynamic power generation with reduced friction loss with all blade impeller water turbine, including various refrigeration equipment using cold energy Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Includes turbine blade (8c) with power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31Y) for reducing friction loss with all blade impeller water turbines and including various refrigeration equipment using cold energy Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross section (4F) tabine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section including various cold storage equipment (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4F) tabine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section including various refrigeration equipment using cold energy (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section (79K) including a turbine blade section (4F) and a combined engine combustion section (31X) for hydroelectric power generation using a turbine blade turbine with a turbine blade cross section (4F) and various refrigeration equipment using cold heat ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Combined engine injection unit (79K) that includes a turbine blade cross section (4F) and a combined engine combustion unit (31Y) that generates hydroelectric power with a turbine blade turbine and a turbine blade turbine (31Y) and includes various refrigeration equipment using cold energy ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation with all-wheel impeller water turbines and various refrigeration equipment utilizing cold energy Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation with a fully moving blade impeller water turbine, and various refrigeration equipment using cold energy Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32X) for hydroelectric power generation with heating high temperature means (3B) by a vertical all blade water turbine, and various cold storage using cold energy Combined engine injection unit (79K) including equipment and equipment Various energy storage cycle combined engines as various air suction injection drive equipment.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a all-blade combustion section (32Y) for hydroelectric power generation by a high temperature heating means (3B) with a vertical all blade water turbine and various cold storage using cold energy Combined engine injection unit (79K) including equipment and equipment Various energy storage cycle combined engines as various air suction injection drive equipment.   Combined with a turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine, including various refrigeration equipment using cold energy Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined with a turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, including various refrigeration equipment using cold energy Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection including a turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31X) for hydroelectric power generation with a fully-rotor impeller water turbine, including various refrigeration equipment using cold energy (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation with a fully-rotor impeller water turbine and including various refrigeration equipment using cold energy (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Includes turbine blade (8c) with power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31X) for hydrodynamic power generation with reduced friction loss with all blade impeller water turbine, including various refrigeration equipment using cold energy Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Includes turbine blade (8c) with power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31Y) for reducing friction loss with all blade impeller water turbines and including various refrigeration equipment using cold energy Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross section (4F) tabine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section including various hot water piping equipment (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4F) tabine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section including various hot water piping equipment (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection unit (79K) including various hot water piping facilities and equipment including a combined turbine combustion unit (31X) for hydroelectric power generation with a turbine blade cross section (4F) and a turbine blade turbine 8 ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Combined engine injection unit (79K) including various hot water piping facilities and equipment including a combined turbine combustion unit (31Y) for hydroelectric power generation with a turbine blade cross section (4F) and a turbine blade turbine (8F) and a turbine blade turbine ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and all blade impeller water turbine with heating high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation and various hot water piping equipment Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation with a heating blade high speed turbine (3B) with all blade impeller water turbines and various hot water piping equipment Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   Turbine blade (8c) of power generation technology with turbine blade cross section (4E) and heating blade high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, and various hot water pipes Combined engine injection unit (79K) including equipment and equipment Various energy storage cycle combined engines as various air suction injection drive equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a heating blade high temperature means (3B) all blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, and various hot water pipes Combined engine injection unit (79K) including equipment and equipment Various energy storage cycle combined engines as various air suction injection drive equipment.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, combined with various hot water piping equipment Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blades (8c) of power generation technology with turbine blade cross section (4E) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, combined with various hot water piping equipment Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection including a turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31X) for hydroelectric power generation with a fully-rotor impeller water turbine, including various hot water piping equipment (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation with a fully-rotor impeller water turbine, including various hot water piping equipment (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Includes turbine blades (8c) of power generation technology with turbine blade cross section (4E) and coalescence engine combustion part (31X) for reducing friction loss water generation with all blade impeller water turbines, including various hot water piping equipment Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Includes turbine blade (8c) of power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31Y) for reducing friction loss hydroelectric power generation with all blade impeller water turbine, including various hot water piping equipment Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross section (4F) tabine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section including various hot water piping equipment (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4F) tabine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section including various hot water piping equipment (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection unit (79K) including various hot water piping facilities and equipment including a combined turbine combustion unit (31X) for hydroelectric power generation with a turbine blade cross section (4F) and a turbine blade turbine 8 ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Combined engine injection unit (79K) including various hot water piping facilities and equipment including a combined turbine combustion unit (31Y) for hydroelectric power generation with a turbine blade cross section (4F) and a turbine blade turbine (8F) and a turbine blade turbine ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and all blade impeller water turbine with heating high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation and various hot water piping equipment Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation with a heating blade high speed turbine (3B) with all blade impeller water turbines and various hot water piping equipment Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   Turbine blade (8c) of power generation technology with turbine blade cross section (4E) and heating blade high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, and various hot water pipes Combined engine injection unit (79K) including equipment and equipment Various energy storage cycle combined engines as various air suction injection drive equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a heating blade high temperature means (3B) all blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, and various hot water pipes Combined engine injection unit (79K) including equipment and equipment Various energy storage cycle combined engines as various air suction injection drive equipment.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, combined with various hot water piping equipment Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blades (8c) of power generation technology with turbine blade cross section (4E) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, combined with various hot water piping equipment Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection including a turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31X) for hydroelectric power generation with a fully-rotor impeller water turbine, including various hot water piping equipment (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation with a fully-rotor impeller water turbine, including various hot water piping equipment (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Includes turbine blades (8c) of power generation technology with turbine blade cross section (4E) and coalescence engine combustion part (31X) for reducing friction loss water generation with all blade impeller water turbines, including various hot water piping equipment Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Includes turbine blade (8c) of power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31Y) for reducing friction loss hydroelectric power generation with all blade impeller water turbine, including various hot water piping equipment Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Combined engine injection unit (79K) including a turbine blade cross section (4F) and a turbine blade combustion unit (32X) for hydroelectric power generation using a vertical all-blade water turbine with various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Combined engine injection section (79K) including a turbine blade cross section (4F) and a turbine blade combustion section (32Y) for hydroelectric power generation by a vertical all blade water turbine with various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Combined engine injection part (79K) with various vertical ascending and descending parts, including a turbine blade section (4F) and a combined engine combustion part (31X) for hydroelectric power generation with a turbine blade turbine (8F) and a turbine blade turbine. Various energy storage cycle coalescing engines as suction injection drive devices.   Combined engine injection part (79K) with various vertical ascending / descending parts, including a turbine blade section (4F) and a combined engine combustion part (31Y) for hydroelectric power generation with a turbine blade turbine (8F). Various energy storage cycle coalescing engines as suction injection drive devices.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and all blade impeller water turbine with heating high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation, including various vertical rise and fall Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade impeller water turbine with heating high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation, including various vertical rise and fall Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and vertical all blade water turbine with heating high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation and various vertical rise and fall Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and vertical all blade blade water turbine with heating high temperature means (3B) all blade combustion section (32Y) for hydroelectric power generation, various vertical rise and fall Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blades (8c) of power generation technology with a turbine blade cross section (4E) and a full blade combustion unit (32X) for hydroelectric power generation with a vertical all blade water turbine, and a combined engine injection unit including various vertical rise and fall (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section including various vertical rise and fall (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection part (79K) including a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined engine combustion part (31X) for hydroelectric power generation with a full-rotor impeller water turbine and including various vertical rising and falling ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Combined engine injection part (79K) including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion part (31Y) for hydroelectric power generation with a fully moving blade impeller water turbine and including various vertical rise and fall ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Combined engine injection with various vertical rise and fall with turbine blade (8c) of power generation technology with turbine blade cross section (4E) and combined engine combustion part (31X) for hydrodynamic power generation with reduced friction loss with all blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection with various vertical rise and fall with turbine blade (8c) of power generation technology with turbine blade cross section (4E) and combined engine combustion section (31Y) for hydrodynamic power generation with reduced friction loss with all blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection unit (79K) including a turbine blade cross section (4F) and a turbine blade combustion unit (32X) for hydroelectric power generation using a vertical all-blade water turbine with various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Combined engine injection section (79K) including a turbine blade cross section (4F) and a turbine blade combustion section (32Y) for hydroelectric power generation by a vertical all blade water turbine with various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Combined engine injection part (79K) with various vertical ascending and descending parts, including a turbine blade section (4F) and a combined engine combustion part (31X) for hydroelectric power generation with a turbine blade turbine (8F) and a turbine blade turbine. Various energy storage cycle coalescing engines as suction injection drive devices.   Combined engine injection part (79K) with various vertical ascending / descending parts, including a turbine blade section (4F) and a combined engine combustion part (31Y) for hydroelectric power generation with a turbine blade turbine (8F). Various energy storage cycle coalescing engines as suction injection drive devices.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and all blade impeller water turbine with heating high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation, including various vertical rise and fall Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade impeller water turbine with heating high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation, including various vertical rise and fall Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and vertical all blade water turbine with heating high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation and various vertical rise and fall Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and vertical all blade blade water turbine with heating high temperature means (3B) all blade combustion section (32Y) for hydroelectric power generation, various vertical rise and fall Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blades (8c) of power generation technology with a turbine blade cross section (4E) and a full blade combustion unit (32X) for hydroelectric power generation with a vertical all blade water turbine, and a combined engine injection unit including various vertical rise and fall (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section including various vertical rise and fall (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection part (79K) including a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined engine combustion part (31X) for hydroelectric power generation with a full-rotor impeller water turbine and including various vertical rising and falling ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Combined engine injection part (79K) including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion part (31Y) for hydroelectric power generation with a fully moving blade impeller water turbine and including various vertical rise and fall ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Combined engine injection with various vertical rise and fall with turbine blade (8c) of power generation technology with turbine blade cross section (4E) and combined engine combustion part (31X) for hydrodynamic power generation with reduced friction loss with all blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection with various vertical rise and fall with turbine blade (8c) of power generation technology with turbine blade cross section (4E) and combined engine combustion section (31Y) for hydrodynamic power generation with reduced friction loss with all blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection unit (79K) including various supersonic flight with a turbine blade cross section (4F) and a tabine blade (8c) and a full blade combustion unit (32X) for hydroelectric power generation with a vertical all blade water turbine Various energy storage cycle coalescing engines as various air suction jet drive devices.   Combined engine injection unit (79K) including various supersonic flight with a turbine blade cross section (4F), a tabine blade (8c) and a full blade combustion unit (32Y) for hydroelectric power generation with a vertical all blade water turbine Various energy storage cycle coalescing engines as various air suction jet drive devices.   Combined engine injection unit (79K) with various supersonic flights, including a turbine blade section (4F) and a combined engine combustion unit (31X) for hydroelectric power generation with a turbine blade turbine (8F) and a turbine blade turbine. Various energy storage cycle coalescing engines as suction injection drive devices.   Combined engine injection unit (79K) with various supersonic flights, including a turbine blade section (4F) and a combined engine combustion unit (31Y) for hydroelectric power generation with a turbine blade turbine (8F) and a turbine blade turbine. Various energy storage cycle coalescing engines as suction injection drive devices.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade impeller water turbine with heating high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation, including various supersonic flight Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and all blade impeller water turbine with heating high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation, including various supersonic flight Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade (8c) with power generation technology with a turbine blade cross section (4E) and a full blade combustion section (32X) for hydroelectric power generation with a heating high temperature means (3B) by a vertical all blade water turbine and various supersonic flight Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and vertical all blade water turbine with heating high temperature means (3B) all blade combustion section (32Y) for hydroelectric power generation and various supersonic flight Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Combined engine injection section including various supersonic flight with turbine blade (8c) of power generation technology with turbine blade cross section (4E) and full blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and full blade combustion portion (32Y) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section including various supersonic flight (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection part (79K) including a supersonic flight including a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined engine combustion part (31X) for hydroelectric power generation with a fully moving blade impeller water turbine ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Combined engine injection part (79K) including a supersonic flight including a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined engine combustion part (31Y) for hydroelectric power generation with a fully moving blade impeller water turbine ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Combined engine injection including a supersonic flight with a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) that generates hydrodynamic power with reduced friction loss by all-wheel impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including a supersonic flight with a turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation with reduced friction loss by all-wheel impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection unit (79K) including various supersonic flight with a turbine blade cross section (4F) and a tabine blade (8c) and a full blade combustion unit (32X) for hydroelectric power generation with a vertical all blade water turbine Various energy storage cycle coalescing engines as various air suction jet drive devices.   Combined engine injection unit (79K) including various supersonic flight with a turbine blade cross section (4F), a tabine blade (8c) and a full blade combustion unit (32Y) for hydroelectric power generation with a vertical all blade water turbine Various energy storage cycle coalescing engines as various air suction jet drive devices.   Combined engine injection unit (79K) with various supersonic flights, including a turbine blade section (4F) and a combined engine combustion unit (31X) for hydroelectric power generation with a turbine blade turbine (8F) and a turbine blade turbine. Various energy storage cycle coalescing engines as suction injection drive devices.   Combined engine injection unit (79K) with various supersonic flights, including a turbine blade section (4F) and a combined engine combustion unit (31Y) for hydroelectric power generation with a turbine blade turbine (8F) and a turbine blade turbine. Various energy storage cycle coalescing engines as suction injection drive devices.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade impeller water turbine with heating high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation, including various supersonic flight Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and all blade impeller water turbine with heating high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation, including various supersonic flight Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade (8c) with power generation technology with a turbine blade cross section (4E) and a full blade combustion section (32X) for hydroelectric power generation with a heating high temperature means (3B) by a vertical all blade water turbine and various supersonic flight Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and vertical all blade water turbine with heating high temperature means (3B) all blade combustion section (32Y) for hydroelectric power generation and various supersonic flight Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Combined engine injection section including various supersonic flight with turbine blade (8c) of power generation technology with turbine blade cross section (4E) and full blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and full blade combustion portion (32Y) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section including various supersonic flight (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection part (79K) including a supersonic flight including a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined engine combustion part (31X) for hydroelectric power generation with a fully moving blade impeller water turbine ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Combined engine injection part (79K) including a supersonic flight including a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined engine combustion part (31Y) for hydroelectric power generation with a fully moving blade impeller water turbine ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Combined engine injection including a supersonic flight with a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) that generates hydrodynamic power with reduced friction loss by all-wheel impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including a supersonic flight with a turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation with reduced friction loss by all-wheel impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection part (79K) with various space flight, equipped with a turbine blade cross section (4F), a tabine blade (8c) and a full blade combustion part (32X) for hydroelectric power generation with a vertical all blade water turbine Various energy storage cycle coalescing engine as air suction jet drive equipment.   Combined engine injection part (79K) with various space flight, equipped with a turbine blade cross section (4F), a tabine blade (8c) and a full blade combustion part (32Y) for hydroelectric power generation with a vertical all blade water turbine Various energy storage cycle coalescing engine as air suction jet drive equipment.   Combined engine injection part (79K) including various space flights, equipped with a turbine blade section (4F) and a combined engine combustion part (31X) for hydroelectric power generation with all blade impeller water turbines with a turbine blade cross section (4F) Various energy storage cycle coalescing engines as injection drive devices.   Combined engine injection part (79K) including various space flights, equipped with a turbine blade section (4F) and a combined engine combustion part (31Y) for hydroelectric power generation with a turbine blade turbine (8F) and a turbine blade turbine. Various energy storage cycle coalescing engines as injection drive devices.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and all blade impeller water turbine with heating high temperature means (3B) coalescence engine combustion part (31X) for hydroelectric power generation, including various space flights Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blade (8c) of power generation technology with turbine blade cross-section (4E) and coalescence engine combustion unit (31Y) for hydroelectric power generation with heating blade high-speed means (3B) hydrodynamic power generation with all blade impeller water turbine, including various space flight Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   The turbine blade cross section (4E) has a power generation technology turbine blade (8c) and a vertical blade-type all-blade water turbine with a high-temperature heating means (3B) and a full-blade combustion section (32X) for hydroelectric power generation. Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a full-blade combustion section (32Y) for hydroelectric power generation with heating high-temperature means (3B) by a vertical all-blade water turbine and various space flights Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and all blade combustion section (32X) that performs hydroelectric power generation with vertical all blade water turbine, combined engine injection section including various space flight ( 79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4E) with a turbine blade (8c) of power generation technology and a full blade combustion section (32Y) that performs hydroelectric power generation with a vertical all blade water turbine, and a combined engine injection section including various space flights ( 79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section (79K) including various space flight, equipped with turbine blade (8c) of power generation technology with turbine blade cross section (4E) and combined engine combustion section (31X) for hydroelectric power generation with all blade impeller water turbine Various energy storage cycle coalescing engines as various air suction jet drive devices.   Combined engine injection part (79K) including various space flight, equipped with turbine blade (8c) of power generation technology with turbine blade cross section (4E) and combined engine combustion part (31Y) for hydroelectric power generation with all blade impeller water turbine Various energy storage cycle coalescing engines as various air suction jet drive devices.   Combined engine injection section including various space flight, equipped with turbine blade (8c) of power generation technology with turbine blade cross section (4E) and combined engine combustion section (31X) for reducing friction loss hydroelectric power generation with all blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section including various space flight with turbine blade (8c) of power generation technology with turbine blade cross section (4E) and combined engine combustion section (31Y) for hydroelectric power generation with reduced friction loss with all blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection part (79K) with various space flight, equipped with a turbine blade cross section (4F), a tabine blade (8c) and a full blade combustion part (32X) for hydroelectric power generation with a vertical all blade water turbine Various energy storage cycle coalescing engine as air suction jet drive equipment.   Combined engine injection part (79K) with various space flight, equipped with a turbine blade cross section (4F), a tabine blade (8c) and a full blade combustion part (32Y) for hydroelectric power generation with a vertical all blade water turbine Various energy storage cycle coalescing engine as air suction jet drive equipment.   Combined engine injection part (79K) including various space flights, equipped with a turbine blade section (4F) and a combined engine combustion part (31X) for hydroelectric power generation with all blade impeller water turbines with a turbine blade cross section (4F) Various energy storage cycle coalescing engines as injection drive devices.   Combined engine injection part (79K) including various space flights, equipped with a turbine blade section (4F) and a combined engine combustion part (31Y) for hydroelectric power generation with a turbine blade turbine (8F) and a turbine blade turbine. Various energy storage cycle coalescing engines as injection drive devices.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and all blade impeller water turbine with heating high temperature means (3B) coalescence engine combustion part (31X) for hydroelectric power generation, including various space flights Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blade (8c) of power generation technology with turbine blade cross-section (4E) and coalescence engine combustion unit (31Y) for hydroelectric power generation with heating blade high-speed means (3B) hydrodynamic power generation with all blade impeller water turbine, including various space flight Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   The turbine blade cross section (4E) has a power generation technology turbine blade (8c) and a vertical blade-type all-blade water turbine with a high-temperature heating means (3B) and a full-blade combustion section (32X) for hydroelectric power generation. Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a full-blade combustion section (32Y) for hydroelectric power generation with heating high-temperature means (3B) by a vertical all-blade water turbine and various space flights Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and all blade combustion section (32X) that performs hydroelectric power generation with vertical all blade water turbine, combined engine injection section including various space flight ( 79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4E) with a turbine blade (8c) of power generation technology and a full blade combustion section (32Y) that performs hydroelectric power generation with a vertical all blade water turbine, and a combined engine injection section including various space flights ( 79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section including various space flight, equipped with turbine blade (8c) of power generation technology with turbine blade cross section (4E) and combined engine combustion section (31X) for reducing friction loss hydroelectric power generation with all blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section including various space flight with turbine blade (8c) of power generation technology with turbine blade cross section (4E) and combined engine combustion section (31Y) for hydroelectric power generation with reduced friction loss with all blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Driven by a hydroelectric storage battery with a turbine blade cross section (4F) and a turbine blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine, including various refrigeration equipment using cold heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Driven by a hydroelectric storage battery including a turbine blade cross section (4F) and a turbine blade combustion section (32Y) for hydroelectric power generation by a vertical all blade water turbine with a turbine blade cross section (4F) and various refrigeration equipment using cold heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross section (4F) tabine blade (8c) and a combined engine combustion unit (31X) for hydroelectric power generation with all-wheel impeller water turbines, and various rotations driven by hydroelectric storage batteries including various refrigeration equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   Turbine blade cross section (4F) tabine blade (8c) and all-wheel blade bobbin water turbine combined unit combustion unit (31Y) for hydroelectric power generation and various rotations driven by hydroelectric storage battery including various refrigeration equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation with all-wheel impeller water turbines and various refrigeration equipment utilizing cold energy Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation with a fully moving blade impeller water turbine, and various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32X) for hydroelectric power generation with heating high temperature means (3B) by a vertical all blade water turbine, and various cold storage using cold energy Various energy storage cycle coalescing engines, which are driven by hydroelectric storage batteries and various rotational output drive devices including equipment.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a all-blade combustion section (32Y) for hydroelectric power generation by a high temperature heating means (3B) with a vertical all blade water turbine and various cold storage using cold energy Various energy storage cycle coalescing engines, which are driven by hydroelectric storage batteries and various rotational output drive devices including equipment.   Water including a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine, including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Water including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Hydroelectric power storage battery comprising a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) for hydroelectric power generation using a fully-rotated blade impeller water turbine and including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   A hydroelectric storage battery comprising a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation using a water turbine with all rotor blades, and various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   Includes turbine blade (8c) with power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31X) for hydrodynamic power generation with reduced friction loss with all blade impeller water turbine, including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes turbine blade (8c) with power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31Y) for reducing friction loss with all blade impeller water turbines and including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Driven by a hydroelectric storage battery with a turbine blade cross section (4F) and a turbine blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine, including various refrigeration equipment using cold heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Driven by a hydroelectric storage battery including a turbine blade cross section (4F) and a turbine blade combustion section (32Y) for hydroelectric power generation by a vertical all blade water turbine with a turbine blade cross section (4F) and various refrigeration equipment using cold heat Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross section (4F) tabine blade (8c) and a combined engine combustion unit (31X) for hydroelectric power generation with all-wheel impeller water turbines, and various rotations driven by hydroelectric storage batteries including various refrigeration equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   Turbine blade cross section (4F) tabine blade (8c) and all-wheel blade bobbin water turbine combined unit combustion unit (31Y) for hydroelectric power generation and various rotations driven by hydroelectric storage battery including various refrigeration equipment using cold energy Various energy storage cycle coalescence engine as output drive equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation with all-wheel impeller water turbines and various refrigeration equipment utilizing cold energy Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation with a fully moving blade impeller water turbine, and various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32X) for hydroelectric power generation with heating high temperature means (3B) by a vertical all blade water turbine, and various cold storage using cold energy Various energy storage cycle coalescing engines, which are driven by hydroelectric storage batteries and various rotational output drive devices including equipment.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a all-blade combustion section (32Y) for hydroelectric power generation by a high temperature heating means (3B) with a vertical all blade water turbine and various cold storage using cold energy Various energy storage cycle coalescing engines, which are driven by hydroelectric storage batteries and various rotational output drive devices including equipment.   Water including a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine, including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Water including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Hydroelectric power storage battery comprising a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) for hydroelectric power generation using a fully-rotated blade impeller water turbine and including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   A hydroelectric storage battery comprising a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation using a water turbine with all rotor blades, and various refrigeration equipment using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   Includes turbine blade (8c) with power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31X) for hydrodynamic power generation with reduced friction loss with all blade impeller water turbine, including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes turbine blade (8c) with power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31Y) for reducing friction loss with all blade impeller water turbines and including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Driven by a hydroelectric power storage battery with a turbine blade cross section (4F) and a turbine blade combustion section (32X) for hydroelectric power generation by a vertical all blade water turbine with various cooling equipments Various energy storage cycle coalescing engines as various rotational output drive devices.   Driven by a hydroelectric power storage battery, including a turbine blade cross section (4F) and a turbine blade combustion section (32Y) for hydroelectric power generation by a vertical all blade water turbine with a turbine blade cross section (4F) and various cooling equipment using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross section (4F) tabine vane (8c) and all-wheel impeller spearwheel combined turbine combustion unit (31X) for hydroelectric power generation and hydroelectric storage battery driven various rotations including various cooling equipment Various energy storage cycle coalescence engine as output drive equipment.   Turbine blade cross section (4F) tabine blades (8c) and all-compartment blade propeller water turbine combined unit combustion unit (31Y) for hydroelectric power generation and various types of hydroelectric storage battery driven rotation using various cooling equipment Various energy storage cycle coalescence engine as output drive equipment.   Power generation technology turbine blade (8c) with a turbine blade cross section (4E) and heating and high temperature means (3B) with a combined turbine combustion section (31X) for hydroelectric power generation with all blade impeller water turbines. Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation with all-wheel impeller water turbines and various cooling equipment using cold heat Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a all-blade combustion section (32X) for hydroelectric power generation with a heating high-temperature means (3B) by a vertical all-blade water turbine, and various cooling using cold heat Various energy storage cycle coalescing engines, which are driven by hydroelectric storage batteries and various rotational output drive devices including equipment.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a all-blade combustion section (32Y) for hydroelectric power generation with a heating high temperature means (3B) by a vertical all blade water turbine and various cooling using cold heat Various energy storage cycle coalescing engines, which are driven by hydroelectric storage batteries and various rotational output drive devices including equipment.   Water including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine, including various cooling equipment using cold energy Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Water including a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, including various cooling equipment using cold energy Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Hydroelectric power storage battery comprising a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) for hydroelectric power generation with a water turbine with all rotor blades and a variety of cooling equipment using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   Hydroelectric power storage battery comprising a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation using a water turbine with all rotor blades and a variety of cooling equipment using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   Includes a turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31X) that reduces friction loss with all blade impeller water turbines and includes various cooling equipment using cold energy Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes a turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31Y) that reduces friction loss with all blade impeller water turbines and includes various cooling equipment using cold energy Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Driven by a hydroelectric power storage battery with a turbine blade cross section (4F) and a turbine blade combustion section (32X) for hydroelectric power generation by a vertical all blade water turbine with various cooling equipments Various energy storage cycle coalescing engines as various rotational output drive devices.   Driven by a hydroelectric power storage battery, including a turbine blade cross section (4F) and a turbine blade combustion section (32Y) for hydroelectric power generation by a vertical all blade water turbine with a turbine blade cross section (4F) and various cooling equipment using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross section (4F) tabine vane (8c) and all-wheel impeller spearwheel combined turbine combustion unit (31X) for hydroelectric power generation and hydroelectric storage battery driven various rotations including various cooling equipment Various energy storage cycle coalescence engine as output drive equipment.   Turbine blade cross section (4F) tabine blades (8c) and all-compartment blade propeller water turbine combined unit combustion unit (31Y) for hydroelectric power generation and various types of hydroelectric storage battery driven rotation using various cooling equipment Various energy storage cycle coalescence engine as output drive equipment.   Power generation technology turbine blade (8c) with a turbine blade cross section (4E) and heating and high temperature means (3B) with a combined turbine combustion section (31X) for hydroelectric power generation with all blade impeller water turbines. Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation with all-wheel impeller water turbines and various cooling equipment using cold heat Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a all-blade combustion section (32X) for hydroelectric power generation with a heating high-temperature means (3B) by a vertical all-blade water turbine, and various cooling using cold heat Various energy storage cycle coalescing engines, which are driven by hydroelectric storage batteries and various rotational output drive devices including equipment.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a all-blade combustion section (32Y) for hydroelectric power generation with a heating high temperature means (3B) by a vertical all blade water turbine and various cooling using cold heat Various energy storage cycle coalescing engines, which are driven by hydroelectric storage batteries and various rotational output drive devices including equipment.   Water including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine, including various cooling equipment using cold energy Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Water including a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, including various cooling equipment using cold energy Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Hydroelectric power storage battery comprising a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) for hydroelectric power generation with a water turbine with all rotor blades and a variety of cooling equipment using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   Hydroelectric power storage battery comprising a turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation using a water turbine with all rotor blades and a variety of cooling equipment using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   Includes a turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31X) that reduces friction loss with all blade impeller water turbines and includes various cooling equipment using cold energy Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes a turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31Y) that reduces friction loss with all blade impeller water turbines and includes various cooling equipment using cold energy Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Driven by a hydroelectric storage battery, which has a turbine blade cross section (4F) and a turbine blade combustion section (32X) for hydroelectric power generation by a vertical all blade water turbine, including various ice making equipment Various energy storage cycle coalescing engines as various rotational output drive devices.   Driven by a hydroelectric storage battery with a turbine blade cross section (4F) and a turbine blade combustion section (32Y) for hydroelectric power generation by a vertical all blade water turbine, including various ice making equipment Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross section (4F) with tabine blades (8c) and a combined engine combustion section (31X) for hydroelectric power generation with all blade impeller water turbines and various rotations driven by hydroelectric storage batteries including various ice making equipment Various energy storage cycle coalescence engine as output drive equipment.   Turbine blade cross section (4F) with tabine blade (8c) and a combined engine combustion section (31Y) for hydroelectric power generation with all blade impeller water turbines and various rotations driven by hydroelectric storage batteries including various ice making equipment Various energy storage cycle coalescence engine as output drive equipment.   Power generation technology turbine blade (8c) having a turbine blade cross section (4E) and a combined high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller water turbine Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   Power generation technology turbine blade (8c) with a turbine blade cross section (4E) and a combined high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation with all-wheel impeller water turbine, and various ice making equipment using cold energy Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32X) for hydroelectric power generation by a high temperature heating means (3B) with a vertical all blade water turbine, and various ice making using cold heat Various energy storage cycle coalescing engines, which are driven by hydroelectric storage batteries and various rotational output drive devices including equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a whole blade combustion section (32Y) for hydroelectric power generation with heating high temperature means (3B) by a vertical all blade water turbine, and various ice making using cold heat Various energy storage cycle coalescing engines, which are driven by hydroelectric storage batteries and various rotational output drive devices including equipment.   Water including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine, including various ice making equipment using cold energy Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Water including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and an all-blade combustion section (32Y) for hydroelectric power generation by a vertical all-blade water turbine and including various ice making equipment using cold energy Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   A hydroelectric power storage battery comprising a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) for hydroelectric power generation using a water turbine with all rotor blades, and including various ice making equipment using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   A hydroelectric storage battery comprising a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation using a water turbine with all rotor blades, and including various ice making equipment using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   Includes turbine blade (8c) with power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31X) for reducing friction loss with all-wheel impeller water turbine, and includes various ice making equipment using cold energy Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes a turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31Y) for reducing friction loss with all-wheel impeller water turbines and including various ice making equipment using cold energy Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Driven by a hydroelectric storage battery, which has a turbine blade cross section (4F) and a turbine blade combustion section (32X) for hydroelectric power generation by a vertical all blade water turbine, including various ice making equipment Various energy storage cycle coalescing engines as various rotational output drive devices.   Driven by a hydroelectric storage battery with a turbine blade cross section (4F) and a turbine blade combustion section (32Y) for hydroelectric power generation by a vertical all blade water turbine, including various ice making equipment Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross section (4F) with tabine blades (8c) and a combined engine combustion section (31X) for hydroelectric power generation with all blade impeller water turbines and various rotations driven by hydroelectric storage batteries including various ice making equipment Various energy storage cycle coalescence engine as output drive equipment.   Turbine blade cross section (4F) with tabine blade (8c) and a combined engine combustion section (31Y) for hydroelectric power generation with all blade impeller water turbines and various rotations driven by hydroelectric storage batteries including various ice making equipment Various energy storage cycle coalescence engine as output drive equipment.   Power generation technology turbine blade (8c) having a turbine blade cross section (4E) and a combined high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller water turbine Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   Power generation technology turbine blade (8c) with a turbine blade cross section (4E) and a combined high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation with all-wheel impeller water turbine, and various ice making equipment using cold energy Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32X) for hydroelectric power generation by a high temperature heating means (3B) with a vertical all blade water turbine, and various ice making using cold heat Various energy storage cycle coalescing engines, which are driven by hydroelectric storage batteries and various rotational output drive devices including equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a whole blade combustion section (32Y) for hydroelectric power generation with heating high temperature means (3B) by a vertical all blade water turbine, and various ice making using cold heat Various energy storage cycle coalescing engines, which are driven by hydroelectric storage batteries and various rotational output drive devices including equipment.   Water including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine, including various ice making equipment using cold energy Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Water including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and an all-blade combustion section (32Y) for hydroelectric power generation by a vertical all-blade water turbine and including various ice making equipment using cold energy Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   A hydroelectric power storage battery comprising a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) for hydroelectric power generation using a water turbine with all rotor blades, and including various ice making equipment using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   A hydroelectric storage battery comprising a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation using a water turbine with all rotor blades, and including various ice making equipment using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   Includes turbine blade (8c) with power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31X) for reducing friction loss with all-wheel impeller water turbine, and includes various ice making equipment using cold energy Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes a turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31Y) for reducing friction loss with all-wheel impeller water turbines and including various ice making equipment using cold energy Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   A turbine blade section (4F), a tabine blade (8c), and a full-blade combustion section (32X) for hydroelectric power generation using a vertical all-blade water turbine, water jet (79M), various water suction and injection drive devices, Various energy conservation cycle coalescence engine.   A turbine blade cross section (4F), a tabine blade (8c), and a full-blade combustion section (32Y) for hydroelectric power generation by a vertical all-blade water turbine, water jet (79M), various water suction / injection drive devices, Various energy conservation cycle coalescence engine.   Various types of water jet (79M) water suction and injection drive devices equipped with a turbine blade section (4F) and a combined engine combustion section (31X) for hydroelectric power generation with a turbine blade turbine (8F) and a turbine blade turbine. Energy conservation cycle coalescence engine.   Various types of water suction (79M) water suction and injection drive devices equipped with a turbine blade section (4F) and a combined engine combustion section (31Y) for hydroelectric power generation with a turbine blade turbine (8F) and a turbine blade turbine. Energy conservation cycle coalescence engine.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation with all-wheel impeller water turbines and various water jets (79M) Various energy storage cycle coalescing engine as water suction jet drive equipment.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion part (31Y) for hydroelectric power generation with heating high temperature means (3B) with all blade impeller water turbine and various water jets (79M) Various energy storage cycle coalescing engine as water suction jet drive equipment.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32X) for hydroelectric power generation with heating high temperature means (3B) by a vertical all blade water turbine and a water jet (79M ) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a all blade combustion section (32Y) for hydroelectric power generation with a heating high temperature means (3B) by a vertical all blade water turbine and a water jet (79M ) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and an all-blade combustion section (32X) that performs hydroelectric power generation with a vertical all-blade water turbine and water jet (79M) various water suction / injection drive Various energy storage cycle coalescing engines as equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and an all-blade combustion section (32Y) that performs hydroelectric power generation with a vertical all-blade water turbine and water jet (79M) various water suction / injection drive Various energy storage cycle coalescing engines as equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) for hydroelectric power generation using a water turbine with all blade impellers, water jet (79M), various water suction and injection drive devices Various energy conservation cycle coalescing engines.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation using a water turbine with all blades and a water turbine (79M), various water suction and injection drive devices Various energy conservation cycle coalescing engines.   A turbine blade (8c) of the power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31X) that generates hydrodynamic power with reduced friction loss by a fully-rotor impeller water turbine, and water jet (79M) various water suction injections Various energy storage cycle coalescing engines as driving equipment.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31Y) for reducing friction loss water generation with a full-rotor impeller water turbine and water jet (79M) various water suction injection Various energy storage cycle coalescing engines as driving equipment.   A turbine blade section (4F), a tabine blade (8c), and a full-blade combustion section (32X) for hydroelectric power generation using a vertical all-blade water turbine, water jet (79M), various water suction and injection drive devices, Various energy conservation cycle coalescence engine.   A turbine blade cross section (4F), a tabine blade (8c), and a full-blade combustion section (32Y) for hydroelectric power generation by a vertical all-blade water turbine, water jet (79M), various water suction / injection drive devices, Various energy conservation cycle coalescence engine.   Various types of water jet (79M) water suction and injection drive devices equipped with a turbine blade section (4F) and a combined engine combustion section (31X) for hydroelectric power generation with a turbine blade turbine (8F) and a turbine blade turbine. Energy conservation cycle coalescence engine.   Various types of water suction (79M) water suction and injection drive devices equipped with a turbine blade section (4F) and a combined engine combustion section (31Y) for hydroelectric power generation with a turbine blade turbine (8F) and a turbine blade turbine. Energy conservation cycle coalescence engine.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation with all-wheel impeller water turbines and various water jets (79M) Various energy storage cycle coalescing engine as water suction jet drive equipment.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion part (31Y) for hydroelectric power generation with heating high temperature means (3B) with all blade impeller water turbine and various water jets (79M) Various energy storage cycle coalescing engine as water suction jet drive equipment.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32X) for hydroelectric power generation with heating high temperature means (3B) by a vertical all blade water turbine and a water jet (79M ) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a all blade combustion section (32Y) for hydroelectric power generation with a heating high temperature means (3B) by a vertical all blade water turbine and a water jet (79M ) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and an all-blade combustion section (32X) that performs hydroelectric power generation with a vertical all-blade water turbine and water jet (79M) various water suction / injection drive Various energy storage cycle coalescing engines as equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and an all-blade combustion section (32Y) that performs hydroelectric power generation with a vertical all-blade water turbine and water jet (79M) various water suction / injection drive Various energy storage cycle coalescing engines as equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) for hydroelectric power generation using a water turbine with all blade impellers, water jet (79M), various water suction and injection drive devices Various energy conservation cycle coalescing engines.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation using a water turbine with all blades and a water turbine (79M), various water suction and injection drive devices Various energy conservation cycle coalescing engines.   A turbine blade (8c) of the power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31X) that generates hydrodynamic power with reduced friction loss by a fully-rotor impeller water turbine, and water jet (79M) various water suction injections Various energy storage cycle coalescing engines as driving equipment.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31Y) for reducing friction loss water generation with a full-rotor impeller water turbine and water jet (79M) various water suction injection Various energy storage cycle coalescing engines as driving equipment.   A turbine blade cross section (4F) with a tabine blade (8c) and a whole blade combustion section (32X) for hydropower generation with a vertical all blade water turbine. Various energy storage cycle coalescing engines including various water suction / injection drive devices.   A turbine blade cross section (4F) with a tabine blade (8c) and an all-blade combustion section (32Y) for hydroelectric power generation using a vertical all-blade water turbine, and water heater (79M) for various heating equipment using heat. Various energy storage cycle coalescing engines including various water suction / injection drive devices.   A turbine blade section (4F) with a tabine blade (8c) and a combined engine combustion section (31X) for hydroelectric power generation with a full-rotor impeller water turbine, and various types of heating equipment using water jet (79M) Various energy storage cycle coalescing engine as water suction jet drive equipment.   The turbine blade cross section (4F) has a tabine blade (8c) and a combined engine combustion section (31Y) for hydroelectric power generation with a full bucket moving water turbine, and includes various types of heating equipment using water jet (79M) heat. Various energy storage cycle coalescing engine as water suction jet drive equipment.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined moving unit (31X) that generates hydroelectric power by a high temperature heating means (3B) hydroelectric turbine with a fully moving blade impeller water turbine and a water jet (79M) Various energy storage cycle coalescing engines as various water suction / injection drive devices including various heating equipment.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined moving unit (31Y) for hydroelectric power generation with a high temperature heating means (3B) hydrodynamic power generation with all blade impeller water turbines and water jet (79M) heat Various energy storage cycle coalescing engines as various water suction / injection drive devices including various heating equipment.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32X) for hydroelectric power generation with heating high temperature means (3B) by a vertical all blade water turbine and a water jet (79M ) Various energy storage cycle coalescing engines as various water suction / injection drive devices including various types of heating equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a all blade combustion section (32Y) for hydroelectric power generation with a heating high temperature means (3B) by a vertical all blade water turbine and a water jet (79M ) Various energy storage cycle coalescing engines as various water suction / injection drive devices including various types of heating equipment.   Turbine blade (8c) with power generation technology with turbine blade cross section (4E) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, various heating equipment using water jet (79M) heat Various energy storage cycle coalescing engines as various water suction / injection drive devices including devices.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and an all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, and various heating facilities using water jet (79M) heat Various energy storage cycle coalescing engines as various water suction / injection drive devices including devices.   Turbine blade (8c) of power generation technology with turbine blade cross section (4E) and coalescence engine combustion part (31X) for hydroelectric power generation with all blade impeller water turbine, water jet (79M) heating equipment using various heating equipment Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Turbine blade (8c) with power generation technology with turbine blade cross section (4E) and combined engine combustion section (31Y) for hydroelectric power generation with all-wheel impeller water turbine, water jet (79M) heating equipment using various heating equipment Various energy storage cycle coalescing engines as various water suction / injection drive devices.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31X) that generates hydrodynamic power with reduced friction loss with a fully moving blade impeller water turbine, and various types of heating using water jet (79M) heat Various energy storage cycle coalescing engines as various water suction / injection drive devices including equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion section (31Y) for reducing friction loss with all-wheel impeller spur water turbines and water jet (79M) various heating using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices including equipment.   A turbine blade cross section (4F) with a tabine blade (8c) and a whole blade combustion section (32X) for hydropower generation with a vertical all blade water turbine. Various energy storage cycle coalescing engines including various water suction / injection drive devices.   A turbine blade cross section (4F) with a tabine blade (8c) and an all-blade combustion section (32Y) for hydroelectric power generation using a vertical all-blade water turbine, and water heater (79M) for various heating equipment using heat. Various energy storage cycle coalescing engines including various water suction / injection drive devices.   A turbine blade section (4F) with a tabine blade (8c) and a combined engine combustion section (31X) for hydroelectric power generation with a full-rotor impeller water turbine, and various types of heating equipment using water jet (79M) Various energy storage cycle coalescing engine as water suction jet drive equipment.   The turbine blade cross section (4F) has a tabine blade (8c) and a combined engine combustion section (31Y) for hydroelectric power generation with a full bucket moving water turbine, and includes various types of heating equipment using water jet (79M) heat. Various energy storage cycle coalescing engine as water suction jet drive equipment.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined moving unit (31X) that generates hydroelectric power by a high temperature heating means (3B) hydroelectric turbine with a fully moving blade impeller water turbine and a water jet (79M) Various energy storage cycle coalescing engines as various water suction / injection drive devices including various heating equipment.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a combined moving unit (31Y) for hydroelectric power generation with a high temperature heating means (3B) hydrodynamic power generation with all blade impeller water turbines and water jet (79M) heat Various energy storage cycle coalescing engines as various water suction / injection drive devices including various heating equipment.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a whole blade combustion section (32X) for hydroelectric power generation with heating high temperature means (3B) by a vertical all blade water turbine and a water jet (79M ) Various energy storage cycle coalescing engines as various water suction / injection drive devices including various types of heating equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a all blade combustion section (32Y) for hydroelectric power generation with a heating high temperature means (3B) by a vertical all blade water turbine and a water jet (79M ) Various energy storage cycle coalescing engines as various water suction / injection drive devices including various types of heating equipment.   Turbine blade (8c) with power generation technology with turbine blade cross section (4E) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, various heating equipment using water jet (79M) heat Various energy storage cycle coalescing engines as various water suction / injection drive devices including devices.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and an all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, and various heating facilities using water jet (79M) heat Various energy storage cycle coalescing engines as various water suction / injection drive devices including devices.   Turbine blade (8c) of power generation technology with turbine blade cross section (4E) and coalescence engine combustion part (31X) for hydroelectric power generation with all blade impeller water turbine, water jet (79M) heating equipment using various heating equipment Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Turbine blade (8c) with power generation technology with turbine blade cross section (4E) and combined engine combustion section (31Y) for hydroelectric power generation with all-wheel impeller water turbine, water jet (79M) heating equipment using various heating equipment Various energy storage cycle coalescing engines as various water suction / injection drive devices.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31X) that generates hydrodynamic power with reduced friction loss with a fully moving blade impeller water turbine, and various types of heating using water jet (79M) heat Various energy storage cycle coalescing engines as various water suction / injection drive devices including equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion section (31Y) for reducing friction loss with all-wheel impeller spur water turbines and water jet (79M) various heating using heat Various energy storage cycle coalescing engines as various water suction / injection drive devices including equipment.   Turbine blade cross section (4F) tabine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section (79K) various air suction injection drive equipment A variety of energy conservation cycle coalescence engine.   Turbine blade cross section (4F) tabine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section (79K) various air suction injection drive equipment A variety of energy conservation cycle coalescence engine.   The turbine blade cross section (4F) has a tabine blade (8c) and a combined engine combustion section (31X) for hydroelectric power generation using a fully moving impeller turbine, and a combined engine injection section (79K), various air suction injection drive devices, Various energy conservation cycle coalescence engine.   The turbine blade section (4F) has a tabine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation with a fully moving blade spring turbine water turbine, and a combined engine injection section (79K) with various air suction injection drive devices, Various energy conservation cycle coalescence engine.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion unit (31X) for hydroelectric power generation by a heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection unit (79K) ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation by heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection section (79K) ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and vertical all blade water turbine heating high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a heating and high-temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and all blade combustion section (32X) generating hydroelectric power with vertical all blade water turbine, combined engine injection section (79K) various air suction Various energy storage cycle coalescing engines as injection drive devices.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section (79K) various air suction Various energy storage cycle coalescing engines as injection drive devices.   The turbine blade cross section (4E) has a turbine blade (8c) of power generation technology and a combined engine combustion section (31X) that performs hydroelectric power generation with a fully-rotor impeller water turbine, and includes a combined engine injection section (79K) and various air suction injection drives Various energy storage cycle coalescing engines as equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion unit (31Y) that performs hydroelectric power generation with a fully-rotated blade impeller water turbine and a combined engine injection unit (79K) various air suction injection drives Various energy storage cycle coalescing engines as equipment.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and a combined engine combustion section (31X) that generates friction loss reduced water generation with all blade impeller water turbines, combined engine injection section (79K) various air Various energy storage cycle coalescing engines as suction injection drive devices.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all-combined blade impeller water turbine with combined engine combustion section (31Y) for reducing friction loss hydroelectric power and combined engine injection section (79K) various air Various energy storage cycle coalescing engines as suction injection drive devices.   Turbine blade cross section (4F) tabine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section (79K) various air suction injection drive equipment A variety of energy conservation cycle coalescence engine.   Turbine blade cross section (4F) tabine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section (79K) various air suction injection drive equipment A variety of energy conservation cycle coalescence engine.   The turbine blade cross section (4F) has a tabine blade (8c) and a combined engine combustion section (31X) for hydroelectric power generation using a fully moving impeller turbine, and a combined engine injection section (79K), various air suction injection drive devices, Various energy conservation cycle coalescence engine.   The turbine blade section (4F) has a tabine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation with a fully moving blade spring turbine water turbine, and a combined engine injection section (79K) with various air suction injection drive devices, Various energy conservation cycle coalescence engine.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion unit (31X) for hydroelectric power generation by a heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection unit (79K) ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation by heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection section (79K) ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and vertical all blade water turbine heating high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a heating and high-temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and all blade combustion section (32X) generating hydroelectric power with vertical all blade water turbine, combined engine injection section (79K) various air suction Various energy storage cycle coalescing engines as injection drive devices.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section (79K) various air suction Various energy storage cycle coalescing engines as injection drive devices.   The turbine blade cross section (4E) has a turbine blade (8c) of power generation technology and a combined engine combustion section (31X) that performs hydroelectric power generation with a fully-rotor impeller water turbine, and includes a combined engine injection section (79K) and various air suction injection drives Various energy storage cycle coalescing engines as equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion unit (31Y) that performs hydroelectric power generation with a fully-rotated blade impeller water turbine and a combined engine injection unit (79K) various air suction injection drives Various energy storage cycle coalescing engines as equipment.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and a combined engine combustion section (31X) that generates friction loss reduced water generation with all blade impeller water turbines, combined engine injection section (79K) various air Various energy storage cycle coalescing engines as suction injection drive devices.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all-combined blade impeller water turbine with combined engine combustion section (31Y) for reducing friction loss hydroelectric power and combined engine injection section (79K) various air Various energy storage cycle coalescing engines as suction injection drive devices.   Turbine blade cross section (4F) tabine blade (8c) and all blade combustion section (32X) generating hydroelectric power with a vertical all-blade water turbine, combined engine injection section (79K) and various combat capabilities Various energy storage cycle coalescing engine as air suction jet drive equipment.   The turbine blade cross section (4F) has a tabine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) and various combat capabilities Various energy storage cycle coalescing engine as air suction jet drive equipment.   Turbine blade cross section (4F) with tabine blade (8c) and combined moving unit combustion unit (31X) for hydroelectric power generation with all blade impeller water turbine, combined engine injection unit (79K) various air suction including various combat capabilities Various energy storage cycle coalescing engines as injection drive devices.   Turbine blade cross section (4F) tabine wing (8c) and combined moving body combustion unit (31Y) for hydroelectric power generation with all blade impeller water turbine, combined engine injection unit (79K) various air suction including various combat capabilities Various energy storage cycle coalescing engines as injection drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion unit (31X) for hydroelectric power generation by a heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection unit (79K) ) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation by heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection section (79K) ) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and vertical all blade water turbine heating high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various combat capabilities.   Turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a heating and high-temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various combat capabilities.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade combustion section (32X) that generates hydroelectric power with vertical all blade water turbine, combined engine injection section (79K) various combat capabilities Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combining engine injection part (79K) with various turbines (8K) with a turbine blade cross section (4E) and an all-blade combustion part (32Y) that generates hydroelectric power with a vertical all-blade water turbine. Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all-combined blade impeller water turbine combined turbine combustion section (31X) and combined engine injection section (79K) with various combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Turbine blade cross section (4E) and power generation technology turbine blade (8c) and all-combined blade impeller water turbine combined hydrocombustion engine combustion unit (31Y) and combined engine injection unit (79K) including various combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Combining engine injection section (79K) various battles equipped with turbine blade (8c) of power generation technology with turbine blade cross section (4E) and combined engine combustion section (31X) generating friction loss water power with all blade impeller water turbine Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and a combined engine combustion unit (31Y) that generates friction loss water power with all blade impeller water turbines, combined engine injection unit (79K) various battles Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   Turbine blade cross section (4F) tabine blade (8c) and all blade combustion section (32X) generating hydroelectric power with a vertical all-blade water turbine, combined engine injection section (79K) and various combat capabilities Various energy storage cycle coalescing engine as air suction jet drive equipment.   The turbine blade cross section (4F) has a tabine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) and various combat capabilities Various energy storage cycle coalescing engine as air suction jet drive equipment.   Turbine blade cross section (4F) with tabine blade (8c) and combined moving unit combustion unit (31X) for hydroelectric power generation with all blade impeller water turbine, combined engine injection unit (79K) various air suction including various combat capabilities Various energy storage cycle coalescing engines as injection drive devices.   Turbine blade cross section (4F) tabine wing (8c) and combined moving body combustion unit (31Y) for hydroelectric power generation with all blade impeller water turbine, combined engine injection unit (79K) various air suction including various combat capabilities Various energy storage cycle coalescing engines as injection drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion unit (31X) for hydroelectric power generation by a heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection unit (79K) ) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation by heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection section (79K) ) Various energy storage cycle coalescing engines with various air suction jet drive equipment including various combat capabilities.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and vertical all blade water turbine heating high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various combat capabilities.   Turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a heating and high-temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various combat capabilities.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade combustion section (32X) that generates hydroelectric power with vertical all blade water turbine, combined engine injection section (79K) various combat capabilities Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combining engine injection part (79K) with various turbines (8K) with a turbine blade cross section (4E) and an all-blade combustion part (32Y) that generates hydroelectric power with a vertical all-blade water turbine. Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all-combined blade impeller water turbine combined turbine combustion section (31X) and combined engine injection section (79K) with various combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Turbine blade cross section (4E) and power generation technology turbine blade (8c) and all-combined blade impeller water turbine combined hydrocombustion engine combustion unit (31Y) and combined engine injection unit (79K) including various combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Combining engine injection section (79K) various battles equipped with turbine blade (8c) of power generation technology with turbine blade cross section (4E) and combined engine combustion section (31X) generating friction loss water power with all blade impeller water turbine Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and a combined engine combustion unit (31Y) that generates friction loss water power with all blade impeller water turbines, combined engine injection unit (79K) various battles Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   A turbine blade cross section (4F) with a tabine blade (8c) and a full blade combustion unit (32X) for hydroelectric power generation with a saddle type all blade water turbine, and a combined engine injection unit (79K) including various air combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a turbine blade cross section (4F), a tabine blade (8c), and a full-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, and a combined engine injection section (79K) with various air combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Turbine blade cross section (4F) tabine wing (8c) and all-moving blade bouncing water turbine combined coal combustion combustion part (31X), combined engine injection unit (79K) various air including various air combat capabilities Various energy storage cycle coalescing engines as suction injection drive devices.   Turbine blade cross section (4F) tabine wing (8c) and combined engine combustion section (31Y) for hydroelectric power generation with all blade impeller water turbine, combined engine injection section (79K) various air including various air combat capabilities Various energy storage cycle coalescing engines as suction injection drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion unit (31X) for hydroelectric power generation by a heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection unit (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation by heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection section (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and vertical all blade water turbine heating high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various air combat capabilities.   Turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a heating and high-temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various air combat capabilities.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section (79K) various air battles Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade combustion section (32Y) for hydropower generation with vertical all blade water turbine, combined engine injection section (79K) various air battles Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   The turbine blade cross section (4E) has a power generation technology turbine blade (8c) and a combined engine combustion section (31X) that hydroelectrically generates electricity with a fully moving blade impeller water turbine. The combined engine injection section (79K) has various air combat capabilities. Various energy storage cycle coalescing engines including various air suction / injection drive devices.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion unit (31Y) for hydroelectric power generation with a water turbine with all rotor blades, and a combined engine injection unit (79K) with various air combat capabilities Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and combined rotor combustion unit (31X) for reducing friction loss water generation with all blade impeller water turbines, combined engine injection section (79K) various aerial Various energy storage cycle coalescing engines as various air suction / injection drive devices including war capabilities.   Turbine blade cross section (4E) and turbine blade (8c) of the power generation technology and a combined engine combustion unit (31Y) for reducing friction loss water generation with all blade impeller water turbines, and a variety of combined engine injection unit (79K) in the air Various energy storage cycle coalescing engines as various air suction / injection drive devices including war capabilities.   A turbine blade cross section (4F) with a tabine blade (8c) and a full blade combustion unit (32X) for hydroelectric power generation with a saddle type all blade water turbine, and a combined engine injection unit (79K) including various air combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   It has a turbine blade cross section (4F), a tabine blade (8c), and a full-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, and a combined engine injection section (79K) with various air combat capabilities Various energy storage cycle coalescing engines as various air suction jet drive devices.   Turbine blade cross section (4F) tabine wing (8c) and all-moving blade bouncing water turbine combined coal combustion combustion part (31X), combined engine injection unit (79K) various air including various air combat capabilities Various energy storage cycle coalescing engines as suction injection drive devices.   Turbine blade cross section (4F) tabine wing (8c) and combined engine combustion section (31Y) for hydroelectric power generation with all blade impeller water turbine, combined engine injection section (79K) various air including various air combat capabilities Various energy storage cycle coalescing engines as suction injection drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion unit (31X) for hydroelectric power generation by a heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection unit (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation by heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection section (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various air combat capabilities.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and vertical all blade water turbine heating high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various air combat capabilities.   Turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a heating and high-temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various air combat capabilities.   Turbine blade cross section (4E) and power generation technology turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation using vertical all blade water turbine, combined engine injection section (79K) various air battles Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade combustion section (32Y) for hydropower generation with vertical all blade water turbine, combined engine injection section (79K) various air battles Various energy storage cycle coalescing engines as various air suction / injection drive devices including capacity.   The turbine blade cross section (4E) has a power generation technology turbine blade (8c) and a combined engine combustion section (31X) that hydroelectrically generates electricity with a fully moving blade impeller water turbine. The combined engine injection section (79K) has various air combat capabilities. Various energy storage cycle coalescing engines including various air suction / injection drive devices.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion unit (31Y) for hydroelectric power generation with a water turbine with all rotor blades, and a combined engine injection unit (79K) with various air combat capabilities Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and combined rotor combustion unit (31X) for reducing friction loss water generation with all blade impeller water turbines, combined engine injection section (79K) various aerial Various energy storage cycle coalescing engines as various air suction / injection drive devices including war capabilities.   Turbine blade cross section (4E) and turbine blade (8c) of the power generation technology and a combined engine combustion unit (31Y) for reducing friction loss water generation with all blade impeller water turbines, and a variety of combined engine injection unit (79K) in the air Various energy storage cycle coalescing engines as various air suction / injection drive devices including war capabilities.   A turbine blade section (4F) with a tabine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) and various types of cockpits Various energy storage cycle coalescing engine as air suction jet drive equipment.   A turbine blade cross section (4F) with a tabine blade (8c) and a full blade combustion portion (32Y) for hydroelectric power generation with a vertical all blade water turbine, combined engine injection section (79K), including various cockpits Various energy storage cycle coalescing engine as air suction jet drive equipment.   The turbine blade section (4F) has a tabine blade (8c) and a combined engine combustion section (31X) for hydroelectric power generation with a fully moving impeller wheel turbine. Various energy storage cycle coalescing engines as injection drive devices.   The turbine blade cross section (4F) has a tabine blade (8c) and a combined engine combustion unit (31Y) for hydroelectric power generation with a fully moving impeller wheel turbine, and a combined engine injection unit (79K) and various air suctions including various cockpits Various energy storage cycle coalescing engines as injection drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion unit (31X) for hydroelectric power generation by a heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection unit (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cockpits.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation by heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection section (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cockpits.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and vertical all blade water turbine heating high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation, combined engine injection section (79K) Various energy storage cycle combined engines as various air suction / injection drive devices including various cockpits.   Turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a heating and high-temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) Various energy storage cycle combined engines as various air suction / injection drive devices including various cockpits.   Combined engine injection section (79K) various cockpits with turbine blade (8c) of power generation technology with turbine blade cross section (4E) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section (79K) various cockpits with turbine blade (8c) of power generation technology with turbine blade cross section (4E) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and a combined engine combustion section (31X) for hydroelectric power generation with all-wheel impeller water turbines, combined engine injection section (79K) including various cockpits Various energy storage cycle coalescing engines as various air suction jet drive devices.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and a combined engine combustion unit (31Y) for hydroelectric power generation with all-wheel impeller water turbine, combined engine injection unit (79K) including various cockpits Various energy storage cycle coalescing engines as various air suction jet drive devices.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and a combined engine combustion section (31X) that generates friction loss water power with all blade impeller water turbines and various engine operations with combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   A turbine blade (8c) of power generation technology with a turbine blade cross-section (4E) and a combined engine combustion unit (31Y) for reducing friction loss hydroelectric power generation with all blade impeller water turbines and various operations of combined engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   A turbine blade section (4F) with a tabine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) and various types of cockpits Various energy storage cycle coalescing engine as air suction jet drive equipment.   A turbine blade cross section (4F) with a tabine blade (8c) and a full blade combustion portion (32Y) for hydroelectric power generation with a vertical all blade water turbine, combined engine injection section (79K), including various cockpits Various energy storage cycle coalescing engine as air suction jet drive equipment.   The turbine blade section (4F) has a tabine blade (8c) and a combined engine combustion section (31X) for hydroelectric power generation with a fully moving impeller wheel turbine. Various energy storage cycle coalescing engines as injection drive devices.   The turbine blade cross section (4F) has a tabine blade (8c) and a combined engine combustion unit (31Y) for hydroelectric power generation with a fully moving impeller wheel turbine, and a combined engine injection unit (79K) and various air suctions including various cockpits Various energy storage cycle coalescing engines as injection drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion unit (31X) for hydroelectric power generation by a heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection unit (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cockpits.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation by heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection section (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various cockpits.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and vertical all blade water turbine heating high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation, combined engine injection section (79K) Various energy storage cycle combined engines as various air suction / injection drive devices including various cockpits.   Turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a heating and high-temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) Various energy storage cycle combined engines as various air suction / injection drive devices including various cockpits.   Combined engine injection section (79K) various cockpits with turbine blade (8c) of power generation technology with turbine blade cross section (4E) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section (79K) various cockpits with turbine blade (8c) of power generation technology with turbine blade cross section (4E) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and a combined engine combustion section (31X) for hydroelectric power generation with all-wheel impeller water turbines, combined engine injection section (79K) including various cockpits Various energy storage cycle coalescing engines as various air suction jet drive devices.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and a combined engine combustion unit (31Y) for hydroelectric power generation with all-wheel impeller water turbine, combined engine injection unit (79K) including various cockpits Various energy storage cycle coalescing engines as various air suction jet drive devices.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and a combined engine combustion section (31X) that generates friction loss water power with all blade impeller water turbines and various engine operations with combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   A turbine blade (8c) of power generation technology with a turbine blade cross-section (4E) and a combined engine combustion unit (31Y) for reducing friction loss hydroelectric power generation with all blade impeller water turbines and various operations of combined engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   A turbine blade section (4F) with a tabine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) and various control chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   A turbine blade section (4F) with a tabine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) and various control chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Various air suctions including a combined engine injection section (79K) and various control chambers having a combined turbine combustion section (31X) for hydroelectric power generation with a turbine blade cross section (4F) and a turbine blade turbine (8F) and a turbine blade turbine. Various energy storage cycle coalescing engines as injection drive devices.   A variety of air suction including a combined engine injection section (79K) and various control chambers having a combined turbine combustion section (31Y) for hydroelectric power generation with a turbine blade cross section (4F) and a turbine blade turbine (8c) that makes a turbine blade cross section (4F). Various energy storage cycle coalescing engines as injection drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion unit (31X) for hydroelectric power generation by a heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection unit (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various control rooms.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation by heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection section (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various control rooms.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and vertical all blade water turbine heating high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation, combined engine injection section (79K) Various energy storage cycle combined engines as various air suction / injection drive devices including various control rooms.   Turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a heating and high-temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) Various energy storage cycle combined engines as various air suction / injection drive devices including various control rooms.   Combined engine injection section (79K) various control chambers with turbine blade (8c) of power generation technology with turbine blade cross section (4E) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section (79K) various control chambers with turbine blade cross section (4E) and turbine blade (8c) of power generation technology and all blade combustion section (32Y) for hydroelectric generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and combined engine combustion unit (31X) for hydroelectric power generation with all blade impeller water turbine, combined control unit injection unit (79K) including various control chambers Various energy storage cycle coalescing engines as various air suction jet drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion unit (31Y) for hydroelectric power generation with a fully-rotor impeller water turbine includes various control chambers of a combined engine injection unit (79K). Various energy storage cycle coalescing engines as various air suction jet drive devices.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and all rotor blade impeller water turbine combined with coalescence engine combustion section (31X) for reducing friction loss hydroelectric power generation, combined engine injection section (79K) various controls Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion unit (31Y) for reducing friction loss hydroelectric power generation with all blade impeller water turbines and various controls of the combined engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   A turbine blade section (4F) with a tabine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) and various control chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   A turbine blade section (4F) with a tabine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) and various control chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   Various air suctions including a combined engine injection section (79K) and various control chambers having a combined turbine combustion section (31X) for hydroelectric power generation with a turbine blade cross section (4F) and a turbine blade turbine (8F) and a turbine blade turbine. Various energy storage cycle coalescing engines as injection drive devices.   A variety of air suction including a combined engine injection section (79K) and various control chambers having a combined turbine combustion section (31Y) for hydroelectric power generation with a turbine blade cross section (4F) and a turbine blade turbine (8c) that makes a turbine blade cross section (4F). Various energy storage cycle coalescing engines as injection drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion unit (31X) for hydroelectric power generation by a heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection unit (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various control rooms.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation by heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection section (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various control rooms.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and vertical all blade water turbine heating high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation, combined engine injection section (79K) Various energy storage cycle combined engines as various air suction / injection drive devices including various control rooms.   Turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a heating and high-temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) Various energy storage cycle combined engines as various air suction / injection drive devices including various control rooms.   Combined engine injection section (79K) various control chambers with turbine blade (8c) of power generation technology with turbine blade cross section (4E) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section (79K) various control chambers with turbine blade cross section (4E) and turbine blade (8c) of power generation technology and all blade combustion section (32Y) for hydroelectric generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and combined engine combustion unit (31X) for hydroelectric power generation with all blade impeller water turbine, combined control unit injection unit (79K) including various control chambers Various energy storage cycle coalescing engines as various air suction jet drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion unit (31Y) for hydroelectric power generation with a fully-rotor impeller water turbine includes various control chambers of a combined engine injection unit (79K). Various energy storage cycle coalescing engines as various air suction jet drive devices.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and all rotor blade impeller water turbine combined with coalescence engine combustion section (31X) for reducing friction loss hydroelectric power generation, combined engine injection section (79K) various controls Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion unit (31Y) for reducing friction loss hydroelectric power generation with all blade impeller water turbines and various controls of the combined engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Turbine blade cross section (4F) with tabine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section (79K) various types including space travel Various energy storage cycle coalescing engine as air suction jet drive equipment.   Turbine blade cross section (4F) tabine blade (8c) and all blade combustion unit (32Y) for hydroelectric power generation using vertical all blade water turbine, combined engine injection unit (79K) various types including space travel Various energy storage cycle coalescing engine as air suction jet drive equipment.   Turbine blade cross section (4F) with tabine blade (8c) and combined engine combustion unit (31X) for hydroelectric power generation with all blade impeller water turbine, combined engine injection unit (79K) various air suction including various space travel Various energy storage cycle coalescing engines as injection drive devices.   The turbine blade cross section (4F) has a tabine blade (8c) and a combined engine combustion unit (31Y) for hydroelectric power generation with a full moving blade impeller water turbine, and a combined engine injection unit (79K) various air suction including various space trips Various energy storage cycle coalescing engines as injection drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion unit (31X) for hydroelectric power generation by a heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection unit (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation by heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection section (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and vertical all blade water turbine heating high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation, combined engine injection section (79K) Various energy storage cycle combined engines as various air suction / injection drive devices including various space trips.   Turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a heating and high-temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) Various energy storage cycle combined engines as various air suction / injection drive devices including various space trips.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade combustion section (32X) for hydropower generation with vertical all blade water turbine, combined engine injection section (79K) various space travel Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section (79K) various space travel Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and all-wheel impeller combined turbine combustion unit (31X) for hydropower generation with water turbine, combined engine injection unit (79K) including various space travel Various energy storage cycle coalescing engines as various air suction jet drive devices.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and all-combined blade impeller water turbine combined unit combustion unit (31Y) and combined unit injection unit (79K) including various space travel Various energy storage cycle coalescing engines as various air suction jet drive devices.   Turbine blade cross section (4E) and power generation technology turbine blade (8c) and all-combined blade impeller water turbine combined with coalescence engine combustion section (31X) to reduce friction loss hydroelectric power, combined engine injection section (79K) various universes Various energy storage cycle coalescing engines as various air suction jet drive equipment including travel.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and a combined engine combustion section (31Y) for reducing friction loss water power generation with all blade impeller water turbines, combined engine injection section (79K) various universes Various energy storage cycle coalescing engines as various air suction jet drive equipment including travel.   Turbine blade cross section (4F) with tabine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section (79K) various types including space travel Various energy storage cycle coalescing engine as air suction jet drive equipment.   Turbine blade cross section (4F) tabine blade (8c) and all blade combustion unit (32Y) for hydroelectric power generation using vertical all blade water turbine, combined engine injection unit (79K) various types including space travel Various energy storage cycle coalescing engine as air suction jet drive equipment.   Turbine blade cross section (4F) with tabine blade (8c) and combined engine combustion unit (31X) for hydroelectric power generation with all blade impeller water turbine, combined engine injection unit (79K) various air suction including various space travel Various energy storage cycle coalescing engines as injection drive devices.   The turbine blade cross section (4F) has a tabine blade (8c) and a combined engine combustion unit (31Y) for hydroelectric power generation with a full moving blade impeller water turbine, and a combined engine injection unit (79K) various air suction including various space trips Various energy storage cycle coalescing engines as injection drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion unit (31X) for hydroelectric power generation by a heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection unit (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation by heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection section (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various space trips.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and vertical all blade water turbine heating high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation, combined engine injection section (79K) Various energy storage cycle combined engines as various air suction / injection drive devices including various space trips.   Turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a heating and high-temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) Various energy storage cycle combined engines as various air suction / injection drive devices including various space trips.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade combustion section (32X) for hydropower generation with vertical all blade water turbine, combined engine injection section (79K) various space travel Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section (79K) various space travel Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and all-wheel impeller combined turbine combustion unit (31X) for hydropower generation with water turbine, combined engine injection unit (79K) including various space travel Various energy storage cycle coalescing engines as various air suction jet drive devices.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and all-combined blade impeller water turbine combined unit combustion unit (31Y) and combined unit injection unit (79K) including various space travel Various energy storage cycle coalescing engines as various air suction jet drive devices.   Turbine blade cross section (4E) and power generation technology turbine blade (8c) and all-combined blade impeller water turbine combined with coalescence engine combustion section (31X) to reduce friction loss hydroelectric power, combined engine injection section (79K) various universes Various energy storage cycle coalescing engines as various air suction jet drive equipment including travel.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and a combined engine combustion section (31Y) for reducing friction loss water power generation with all blade impeller water turbines, combined engine injection section (79K) various universes Various energy storage cycle coalescing engines as various air suction jet drive equipment including travel.   Turbine blade cross section (4F) tabine blade (8c) and all-blade combustion section (32X) generating hydroelectric power with vertical all-blade water turbine, combined engine injection section (79K) various air including various guest rooms Various energy storage cycle coalescing engines as suction injection drive devices.   Turbine blade cross section (4F) tabine blade (8c) and all-blade combustion section (32Y) generating hydroelectric power with vertical all-blade water turbine, combined engine injection section (79K) various air including various guest rooms Various energy storage cycle coalescing engines as suction injection drive devices.   The turbine blade cross section (4F) has a tabine blade (8c) and a combined engine combustion section (31X) for hydroelectric power generation with a full turbine impeller water turbine. Combined engine injection section (79K) Various air suction injection including various guest rooms Various energy storage cycle coalescing engines as driving equipment.   The turbine blade cross section (4F) has a tabine blade (8c) and a combined engine combustion section (31Y) for hydroelectric power generation with a fully moving blade bouncing water turbine, and a combined engine injection section (79K) various air suction injection including various guest rooms Various energy storage cycle coalescing engines as driving equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion unit (31X) for hydroelectric power generation by a heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection unit (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation by heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection section (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and vertical all blade water turbine heating high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various guest rooms.   Turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a heating and high-temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various guest rooms.   A turbine blade (8c) with power generation technology with a turbine blade cross section (4E) and an all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) various guest rooms Various energy storage cycle coalescing engines including various air suction / injection drive devices.   A turbine blade (8c) with power generation technology with a turbine blade cross section (4E) and an all-blade combustion section (32Y) that performs hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) various guest rooms Various energy storage cycle coalescing engines including various air suction / injection drive devices.   A turbine blade (8c) with power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) that performs hydroelectric power generation with a fully moving impeller water turbine and various engine including a combined engine injection section (79K) and various guest rooms Various energy storage cycle coalescing engine as air suction jet drive equipment.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31Y) that performs hydroelectric power generation with a full-rotor impeller water turbine and various engine including a combined engine injection section (79K) and various guest rooms Various energy storage cycle coalescing engine as air suction jet drive equipment.   Turbine blade cross section (4E) and turbine blade (8c) of the power generation technology and combined rotor combustion unit (31X) that generates friction loss water power with all blade impeller water turbines, combined engine injection section (79K) various guest rooms Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section (79K) with a turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31Y) that generates hydrodynamic power with reduced friction loss with all-wheel impeller water turbine Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4F) tabine blade (8c) and all-blade combustion section (32X) generating hydroelectric power with vertical all-blade water turbine, combined engine injection section (79K) various air including various guest rooms Various energy storage cycle coalescing engines as suction injection drive devices.   Turbine blade cross section (4F) tabine blade (8c) and all-blade combustion section (32Y) generating hydroelectric power with vertical all-blade water turbine, combined engine injection section (79K) various air including various guest rooms Various energy storage cycle coalescing engines as suction injection drive devices.   The turbine blade cross section (4F) has a tabine blade (8c) and a combined engine combustion section (31X) for hydroelectric power generation with a full turbine impeller water turbine. Combined engine injection section (79K) Various air suction injection including various guest rooms Various energy storage cycle coalescing engines as driving equipment.   The turbine blade cross section (4F) has a tabine blade (8c) and a combined engine combustion section (31Y) for hydroelectric power generation with a fully moving blade bouncing water turbine, and a combined engine injection section (79K) various air suction injection including various guest rooms Various energy storage cycle coalescing engines as driving equipment.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion unit (31X) for hydroelectric power generation by a heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection unit (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation by heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection section (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various guest rooms.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and vertical all blade water turbine heating high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various guest rooms.   Turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a heating and high-temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various guest rooms.   A turbine blade (8c) with power generation technology with a turbine blade cross section (4E) and an all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) various guest rooms Various energy storage cycle coalescing engines including various air suction / injection drive devices.   A turbine blade (8c) with power generation technology with a turbine blade cross section (4E) and an all-blade combustion section (32Y) that performs hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) various guest rooms Various energy storage cycle coalescing engines including various air suction / injection drive devices.   A turbine blade (8c) with power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31X) that performs hydroelectric power generation with a fully moving impeller water turbine and various engine including a combined engine injection section (79K) and various guest rooms Various energy storage cycle coalescing engine as air suction jet drive equipment.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31Y) that performs hydroelectric power generation with a full-rotor impeller water turbine and various engine including a combined engine injection section (79K) and various guest rooms Various energy storage cycle coalescing engine as air suction jet drive equipment.   Turbine blade cross section (4E) and turbine blade (8c) of the power generation technology and combined rotor combustion unit (31X) that generates friction loss water power with all blade impeller water turbines, combined engine injection section (79K) various guest rooms Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section (79K) with a turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31Y) that generates hydrodynamic power with reduced friction loss with all-wheel impeller water turbine Various energy storage cycle coalescing engines as various air suction / injection drive devices.   A turbine blade cross section (4F) with a tabine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) and various cargo chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   A turbine blade cross section (4F) with a tabine blade (8c) and an all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) and various cargo chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   The turbine blade cross section (4F) has a tabine blade (8c) and a combined engine combustion section (31X) for hydroelectric power generation with a full bucket impeller water turbine. Combined engine injection section (79K) Various air suction including various cargo chambers Various energy storage cycle coalescing engines as injection drive devices.   The turbine blade cross section (4F) has a tabine blade (8c) and a combined engine combustion section (31Y) for hydroelectric power generation with a fully moving impeller water turbine. Various energy storage cycle coalescing engines as injection drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion unit (31X) for hydroelectric power generation by a heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection unit (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cargo compartments.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation by heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection section (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cargo compartments.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and vertical all blade water turbine heating high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various cargo compartments.   Turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a heating and high-temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various cargo compartments.   Combined engine injection section (79K) various cargo chambers with turbine blade (8c) of power generation technology with turbine blade cross section (4E) and full blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section (79K) various cargo chambers with turbine blade (8c) of power generation technology with turbine blade cross section (4E) and full blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and combined moving body combustion unit (31X) for hydroelectric power generation with all blade impeller water turbine, combined engine injection unit (79K) including various cargo chambers Various energy storage cycle coalescing engines as various air suction jet drive devices.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and a combined engine combustion unit (31Y) for hydroelectric power generation with all-wheel impeller water turbines, and a combined engine injection unit (79K) including various cargo compartments Various energy storage cycle coalescing engines as various air suction jet drive devices.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade impeller water turbine combined with coalescence engine combustion section (31X) for reducing friction loss hydroelectric power, combined engine injection section (79K) various cargo Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all-combined blade impeller water turbine combined coal combustion engine (31Y) for reducing friction loss hydroelectric power generation, combined engine injection unit (79K) various cargo Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   A turbine blade cross section (4F) with a tabine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) and various cargo chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   A turbine blade cross section (4F) with a tabine blade (8c) and an all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) and various cargo chambers Various energy storage cycle coalescing engine as air suction jet drive equipment.   The turbine blade cross section (4F) has a tabine blade (8c) and a combined engine combustion section (31X) for hydroelectric power generation with a full bucket impeller water turbine. Combined engine injection section (79K) Various air suction including various cargo chambers Various energy storage cycle coalescing engines as injection drive devices.   The turbine blade cross section (4F) has a tabine blade (8c) and a combined engine combustion section (31Y) for hydroelectric power generation with a fully moving impeller water turbine. Various energy storage cycle coalescing engines as injection drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion unit (31X) for hydroelectric power generation by a heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection unit (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cargo compartments.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation by heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection section (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various cargo compartments.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and vertical all blade water turbine heating high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various cargo compartments.   Turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a heating and high-temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various cargo compartments.   Combined engine injection section (79K) various cargo chambers with turbine blade (8c) of power generation technology with turbine blade cross section (4E) and full blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section (79K) various cargo chambers with turbine blade (8c) of power generation technology with turbine blade cross section (4E) and full blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and combined moving body combustion unit (31X) for hydroelectric power generation with all blade impeller water turbine, combined engine injection unit (79K) including various cargo chambers Various energy storage cycle coalescing engines as various air suction jet drive devices.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and a combined engine combustion unit (31Y) for hydroelectric power generation with all-wheel impeller water turbines, and a combined engine injection unit (79K) including various cargo compartments Various energy storage cycle coalescing engines as various air suction jet drive devices.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade impeller water turbine combined with coalescence engine combustion section (31X) for reducing friction loss hydroelectric power, combined engine injection section (79K) various cargo Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all-combined blade impeller water turbine combined coal combustion engine (31Y) for reducing friction loss hydroelectric power generation, combined engine injection unit (79K) various cargo Various energy storage cycle coalescing engines as various air suction / injection drive devices including chambers.   The turbine blade section (4F) has a tabine blade (8c) and a full-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine, including a combined engine injection section (79K) with various vertical rises and drops Various energy storage cycle coalescing engines as various air suction jet drive devices.   The turbine blade cross section (4F) has a tabine blade (8c) and a full blade combustion portion (32Y) for hydroelectric power generation with a vertical all blade water turbine, and a combined engine injection portion (79K) includes various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Turbine blade cross section (4F) with tabine blade (8c) and combined engine combustion section (31X) for hydroelectric power generation with all blade impeller water turbine, combined engine injection section (79K) various air including vertical rise and fall Various energy storage cycle coalescing engines as suction injection drive devices.   Turbine blade cross section (4F) with tabine blade (8c) and coalescence engine combustion unit (31Y) for hydroelectric power generation with all blade impeller water turbine, combined engine injection unit (79K) various air including various vertical rise and fall Various energy storage cycle coalescing engines as suction injection drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion unit (31X) for hydroelectric power generation by a heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection unit (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation by heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection section (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and vertical all blade water turbine heating high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation, combined engine injection section (79K) Various energy storage cycle combined engines as various air suction / injection drive devices including various vertical ascent and descent.   Turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a heating and high-temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) Various energy storage cycle combined engines as various air suction / injection drive devices including various vertical ascent and descent.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and all blade combustion section (32X) for hydropower generation with vertical all blade water turbine, combined engine injection section (79K) various vertical rise Various energy storage cycle coalescing engine as various air suction jet drive equipment including descent.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade combustion section (32Y) generating hydroelectric power with vertical all blade water turbine, combined engine injection section (79K) various vertical rise Various energy storage cycle coalescing engines as various air suction jet drive equipment including descent.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31X) that performs hydroelectric power generation with a water turbine with all-wheel impellers, and a combined engine injection section (79K) with various vertical rise and fall Various energy storage cycle coalescing engines including various air suction / injection drive devices.   The turbine blade cross section (4E) has a power generation technology turbine blade (8c) and a combined engine combustion section (31Y) that performs hydroelectric power generation using a fully-rotor impeller water turbine. Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and all-moving blade impeller water turbine combined coal combustion engine (31X) for reducing friction loss hydroelectric power generation, combined engine injection unit (79K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including ascent and descent.   Turbine blades (8c) with power generation technology with a turbine blade cross section (4E) and a combined engine combustion unit (31Y) that generates frictional power with reduced friction loss by all-wheel impeller water turbines, combined engine injection unit (79K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including ascent and descent.   The turbine blade section (4F) has a tabine blade (8c) and a full-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine, including a combined engine injection section (79K) with various vertical rises and drops Various energy storage cycle coalescing engines as various air suction jet drive devices.   The turbine blade cross section (4F) has a tabine blade (8c) and a full blade combustion portion (32Y) for hydroelectric power generation with a vertical all blade water turbine, and a combined engine injection portion (79K) includes various vertical rise and fall Various energy storage cycle coalescing engines as various air suction jet drive devices.   Turbine blade cross section (4F) with tabine blade (8c) and combined engine combustion section (31X) for hydroelectric power generation with all blade impeller water turbine, combined engine injection section (79K) various air including vertical rise and fall Various energy storage cycle coalescing engines as suction injection drive devices.   Turbine blade cross section (4F) with tabine blade (8c) and coalescence engine combustion unit (31Y) for hydroelectric power generation with all blade impeller water turbine, combined engine injection unit (79K) various air including various vertical rise and fall Various energy storage cycle coalescing engines as suction injection drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion unit (31X) for hydroelectric power generation by a heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection unit (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation by heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection section (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various vertical ascent and descent.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and vertical all blade water turbine heating high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation, combined engine injection section (79K) Various energy storage cycle combined engines as various air suction / injection drive devices including various vertical ascent and descent.   Turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a heating and high-temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) Various energy storage cycle combined engines as various air suction / injection drive devices including various vertical ascent and descent.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and all blade combustion section (32X) for hydropower generation with vertical all blade water turbine, combined engine injection section (79K) various vertical rise Various energy storage cycle coalescing engines as various air suction jet drive equipment including descent.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade combustion section (32Y) generating hydroelectric power with vertical all blade water turbine, combined engine injection section (79K) various vertical rise Various energy storage cycle coalescing engines as various air suction jet drive equipment including descent.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31X) that performs hydroelectric power generation with a water turbine with all-wheel impellers, and a combined engine injection section (79K) with various vertical rise and fall Various energy storage cycle coalescing engines including various air suction / injection drive devices.   The turbine blade cross section (4E) has a power generation technology turbine blade (8c) and a combined engine combustion section (31Y) that performs hydroelectric power generation using a fully-rotor impeller water turbine. Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and all-moving blade impeller water turbine combined coal combustion engine (31X) for reducing friction loss hydroelectric power generation, combined engine injection unit (79K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including ascent and descent.   Turbine blades (8c) with power generation technology with a turbine blade cross section (4E) and a combined engine combustion unit (31Y) that generates frictional power with reduced friction loss by all-wheel impeller water turbines, combined engine injection unit (79K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including ascent and descent.   A turbine blade cross section (4F) with a tabine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation using a vertical all blade water turbine, and a combined engine injection section (79K) with various vertical rise and fall Various energy storage cycle coalescing engines as air suction jet drive equipment including airfield.   The turbine blade cross section (4F) has a tabine blade (8c) and a full-blade combustion section (32Y) for hydroelectric power generation using a vertical all-blade water turbine. Various energy storage cycle coalescing engines as air suction jet drive equipment including airfield.   The turbine blade cross section (4F) has a tabine blade (8c) and a combined engine combustion unit (31X) for hydroelectric power generation with a full turbine impeller, and a combined engine injection unit (79K). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   The turbine blade cross section (4F) has a tabine blade (8c) and a combined engine combustion unit (31Y) for hydroelectric power generation with a fully moving blade bouncing water turbine. Combined engine injection unit (79K). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion unit (31X) for hydroelectric power generation by a heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection unit (79K) ) Various energy storage cycle coalescing engines, which are various air suction / injection drive devices including airfields everywhere in vertical ascent and descent.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation by heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection section (79K) ) Various energy storage cycle coalescing engines, which are various air suction / injection drive devices including airfields everywhere in vertical ascent and descent.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and vertical all blade water turbine heating high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation, combined engine injection section (79K) Various types of energy storage cycle coalescing engines as various air suction / injection drive devices including airfields everywhere in vertical ascent and descent.   Turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a heating and high-temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) Various types of energy storage cycle coalescing engines as various air suction / injection drive devices including airfields everywhere in vertical ascent and descent.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and all blade combustion section (32X) for hydropower generation with vertical all blade water turbine, combined engine injection section (79K) various vertical rise Various energy storage cycle coalescing engines as air suction jet drive equipment including airfields wherever descending.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade combustion section (32Y) generating hydroelectric power with vertical all blade water turbine, combined engine injection section (79K) various vertical rise Various energy storage cycle coalescing engines as air suction jet drive equipment including airfields wherever descending.   The turbine blade cross section (4E) has a turbine blade (8c) of power generation technology and a combined engine combustion section (31X) that performs hydroelectric power generation with a water turbine with all blades and a combined engine injection section (79K). But various energy storage cycle coalescing engines as various air suction jet drive equipment including airfield.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and a combined engine combustion section (31Y) for hydroelectric power generation with all-wheel impeller water turbine, combined engine injection section (79K) various vertical rising and falling But various energy storage cycle coalescing engines as various air suction jet drive equipment including airfield.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and all-moving blade impeller water turbine combined coal combustion engine (31X) for reducing friction loss hydroelectric power generation, combined engine injection unit (79K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields wherever you go up and down.   Turbine blades (8c) with power generation technology with a turbine blade cross section (4E) and a combined engine combustion unit (31Y) that generates frictional power with reduced friction loss by all-wheel impeller water turbines, combined engine injection unit (79K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields wherever ascending and descending.   A turbine blade cross section (4F) with a tabine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation using a vertical all blade water turbine, and a combined engine injection section (79K) with various vertical rise and fall Various energy storage cycle coalescing engines as air suction jet drive equipment including airfield.   The turbine blade cross section (4F) has a tabine blade (8c) and a full-blade combustion section (32Y) for hydroelectric power generation using a vertical all-blade water turbine. Various energy storage cycle coalescing engines as air suction jet drive equipment including airfield.   The turbine blade cross section (4F) has a tabine blade (8c) and a combined engine combustion unit (31X) for hydroelectric power generation with a full turbine impeller, and a combined engine injection unit (79K). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   The turbine blade cross section (4F) has a tabine blade (8c) and a combined engine combustion unit (31Y) for hydroelectric power generation with a fully moving blade bouncing water turbine. Combined engine injection unit (79K). Various energy storage cycle coalescing engines including various air suction / injection drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion unit (31X) for hydroelectric power generation by a heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection unit (79K) ) Various energy storage cycle coalescing engines, which are various air suction / injection drive devices including airfields everywhere in vertical ascent and descent.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation by heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection section (79K) ) Various energy storage cycle coalescing engines, which are various air suction / injection drive devices including airfields everywhere in vertical ascent and descent.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and vertical all blade water turbine heating high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation, combined engine injection section (79K) Various types of energy storage cycle coalescing engines as various air suction / injection drive devices including airfields everywhere in vertical ascent and descent.   Turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a heating and high-temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) Various types of energy storage cycle coalescing engines as various air suction / injection drive devices including airfields everywhere in vertical ascent and descent.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and all blade combustion section (32X) for hydropower generation with vertical all blade water turbine, combined engine injection section (79K) various vertical rise Various energy storage cycle coalescing engines as air suction jet drive equipment including airfields wherever descending.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all blade combustion section (32Y) generating hydroelectric power with vertical all blade water turbine, combined engine injection section (79K) various vertical rise Various energy storage cycle coalescing engines as air suction jet drive equipment including airfields wherever descending.   The turbine blade cross section (4E) has a turbine blade (8c) of power generation technology and a combined engine combustion section (31X) that performs hydroelectric power generation with a water turbine with all blades and a combined engine injection section (79K). But various energy storage cycle coalescing engines as various air suction jet drive equipment including airfield.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and a combined engine combustion section (31Y) for hydroelectric power generation with all-wheel impeller water turbine, combined engine injection section (79K) various vertical rising and falling But various energy storage cycle coalescing engines as various air suction jet drive equipment including airfield.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and all-moving blade impeller water turbine combined coal combustion engine (31X) for reducing friction loss hydroelectric power generation, combined engine injection unit (79K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields wherever ascending and descending.   Turbine blades (8c) with power generation technology with a turbine blade cross section (4E) and a combined engine combustion unit (31Y) that generates frictional power with reduced friction loss by all-wheel impeller water turbines, combined engine injection unit (79K) various vertical Various energy storage cycle coalescing engines as various air suction / injection drive devices including airfields wherever ascending and descending.   The turbine blade cross section (4F) has a tabine blade (8c) and a full-blade combustion section (32X) for hydroelectric power generation using a vertical all-blade water turbine. Various energy storage cycle coalescing engines as various air suction jet drive devices.   The turbine blade cross section (4F) has a tabine blade (8c) and a full blade combustion unit (32Y) for hydroelectric power generation using a vertical all blade water turbine, and includes a combined engine injection unit (79K) and various satellite installations. Various energy storage cycle coalescing engines as various air suction jet drive devices.   A turbine blade section (4F) with a tabine blade (8c) and a combined engine combustion section (31X) for hydroelectric power generation with a full turbine impeller water turbine, combined engine injection section (79K) and various air including various satellite installations Various energy storage cycle coalescing engines as suction injection drive devices.   A turbine blade section (4F) with a tabine blade (8c) and a combined engine combustion section (31Y) for hydroelectric power generation with a full turbine impeller water turbine, combined engine injection section (79K) and various air including various satellite installations Various energy storage cycle coalescing engines as suction injection drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion unit (31X) for hydroelectric power generation by a heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection unit (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various satellite installations.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation by heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection section (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various satellite installations.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and vertical all blade water turbine heating high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various satellite installations.   Turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a heating and high-temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various satellite installations.   Combined engine injection unit (79K) various artificial satellites with turbine blade (8c) of power generation technology with turbine blade cross section (4E) and full blade combustion unit (32X) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various air suction jet drive equipment including installation.   Combined engine injection unit (79K) various artificial satellites equipped with turbine blade (8c) of power generation technology with turbine blade cross section (4E) and full blade combustion unit (32Y) generating hydroelectric power with vertical all blade water turbine Various energy storage cycle coalescing engines as various air suction jet drive equipment including installation.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion unit (31X) for hydroelectric power generation with a water turbine with all rotor blades and a combined engine injection unit (79K) installed various satellites. Various energy storage cycle coalescing engines including various air suction / injection drive devices.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion unit (31Y) for hydroelectric power generation with a full-rotor impeller water turbine equipped with a combined engine injection unit (79K) and various satellite installations Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all rotor blade impeller water turbine combined with coalescence engine combustion section (31X) to reduce friction loss hydroelectric power generation, combined engine injection section (79K) various artificial Various energy storage cycle coalescing engines as various air suction jet drive equipment including satellite installation.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and a combined engine combustion section (31Y) for reducing friction loss water power generation with all blade impeller water turbines, combined engine injection section (79K) various artificial Various energy storage cycle coalescing engines as various air suction jet drive equipment including satellite installation.   The turbine blade cross section (4F) has a tabine blade (8c) and a full-blade combustion section (32X) for hydroelectric power generation using a vertical all-blade water turbine. Various energy storage cycle coalescing engines as various air suction jet drive devices.   The turbine blade cross section (4F) has a tabine blade (8c) and a full blade combustion unit (32Y) for hydroelectric power generation using a vertical all blade water turbine, and includes a combined engine injection unit (79K) and various satellite installations. Various energy storage cycle coalescing engines as various air suction jet drive devices.   A turbine blade section (4F) with a tabine blade (8c) and a combined engine combustion section (31X) for hydroelectric power generation with a full turbine impeller water turbine, combined engine injection section (79K) and various air including various satellite installations Various energy storage cycle coalescing engines as suction injection drive devices.   A turbine blade section (4F) with a tabine blade (8c) and a combined engine combustion section (31Y) for hydroelectric power generation with a full turbine impeller water turbine, combined engine injection section (79K) and various air including various satellite installations Various energy storage cycle coalescing engines as suction injection drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion unit (31X) for hydroelectric power generation by a heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection unit (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various satellite installations.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation by heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection section (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including various satellite installations.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and vertical all blade water turbine heating high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various satellite installations.   Turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a heating and high-temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various satellite installations.   Combined engine injection unit (79K) various artificial satellites with turbine blade (8c) of power generation technology with turbine blade cross section (4E) and full blade combustion unit (32X) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various air suction jet drive equipment including installation.   Combined engine injection unit (79K) various artificial satellites equipped with turbine blade (8c) of power generation technology with turbine blade cross section (4E) and full blade combustion unit (32Y) generating hydroelectric power with vertical all blade water turbine Various energy storage cycle coalescing engines as various air suction jet drive equipment including installation.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all rotor blade impeller water turbine combined with coalescence engine combustion section (31X) to reduce friction loss hydroelectric power generation, combined engine injection section (79K) various artificial Various energy storage cycle coalescing engines as various air suction jet drive equipment including satellite installation.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and a combined engine combustion section (31Y) for reducing friction loss water power generation with all blade impeller water turbines, combined engine injection section (79K) various artificial Various energy storage cycle coalescing engines as various air suction jet drive equipment including satellite installation.   Includes turbine blade section (4F), tabine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section (79K) including lunar landing start Various energy storage cycle coalescing engines as various air suction jet drive devices.   A turbine blade section (4F) with a tabine blade (8c) and a full-blade combustion section (32Y) for hydroelectric power generation using a vertical all-blade water turbine and a combined engine injection section (79K) including lunar landing start Various energy storage cycle coalescing engines as various air suction jet drive devices.   A variety of air including a lunar landing start with a combined engine injection section (79K) comprising a combined turbine combustion section (31X) for hydroelectric power generation with a turbine blade cross section (4F) and a turbine blade turbine (8C) and a turbine blade turbine. Various energy storage cycle coalescing engines as suction injection drive devices.   A variety of air including a turbine landing section (4F) and a combined engine combustion section (31Y) for hydroelectric power generation using a turbine blade turbine (8Y) and a turbine blade turbine (3Y), including a combined engine injection section (79K) and lunar landing start Various energy storage cycle coalescing engines as suction injection drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion unit (31X) for hydroelectric power generation by a heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection unit (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including lunar landing start.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation by heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection section (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including lunar landing start.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and vertical all blade water turbine heating high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation, combined engine injection section (79K) Various energy storage cycle combined engines as various air suction / injection drive devices including lunar landing start.   Turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a heating and high-temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) Various energy storage cycle combined engines as various air suction / injection drive devices including lunar landing start.   A turbine blade (8c) with power generation technology with a turbine blade cross section (4E) and an all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine, and a combined engine injection section (79K) moon landing Various energy storage cycle coalescing engines as various air suction / injection drive devices including start.   A turbine blade (8c) with power generation technology with a turbine blade cross section (4E) and a full-blade combustion section (32Y) that performs hydroelectric power generation with a vertical all-blade water turbine and landing on a combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including start.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31Y) for generating friction loss reduced water generation with a fully-rotor impeller water turbine and a combined engine injection section (79K) moon surface Various energy storage cycle coalescing engines as various air suction jet drive equipment including landing start.   Includes turbine blade section (4F), tabine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section (79K) including lunar landing start Various energy storage cycle coalescing engines as various air suction jet drive devices.   A turbine blade section (4F) with a tabine blade (8c) and a full-blade combustion section (32Y) for hydroelectric power generation using a vertical all-blade water turbine and a combined engine injection section (79K) including lunar landing start Various energy storage cycle coalescing engines as various air suction jet drive devices.   A variety of air including a lunar landing start with a combined engine injection section (79K) comprising a combined turbine combustion section (31X) for hydroelectric power generation with a turbine blade cross section (4F) and a turbine blade turbine (8C) and a turbine blade turbine. Various energy storage cycle coalescing engines as suction injection drive devices.   A variety of air including a turbine landing section (4F) and a combined engine combustion section (31Y) for hydroelectric power generation using a turbine blade turbine (8Y) and a turbine blade turbine (3Y), including a combined engine injection section (79K) and lunar landing start Various energy storage cycle coalescing engines as suction injection drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion unit (31X) for hydroelectric power generation by a heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection unit (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including lunar landing start.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation by heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection section (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive equipment including lunar landing start.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and vertical all blade water turbine heating high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation, combined engine injection section (79K) Various energy storage cycle combined engines as various air suction / injection drive devices including lunar landing start.   Turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a heating and high-temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) Various energy storage cycle combined engines as various air suction / injection drive devices including lunar landing start.   A turbine blade (8c) with power generation technology with a turbine blade cross section (4E) and an all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine, and a combined engine injection section (79K) moon landing Various energy storage cycle coalescing engines as various air suction / injection drive devices including start.   A turbine blade (8c) with power generation technology with a turbine blade cross section (4E) and a full-blade combustion section (32Y) that performs hydroelectric power generation with a vertical all-blade water turbine and landing on a combined engine injection section (79K) on the moon surface Various energy storage cycle coalescing engines as various air suction / injection drive devices including start.   A turbine blade (8c) of the power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31X) that hydroelectrically generates electricity with a full bucket impeller water turbine and a combined engine injection section (79K) launching on the moon surface Various energy storage cycle coalescing engines including various air suction / injection drive devices.   The turbine blade cross section (4E) has a power generation technology turbine blade (8c) and a combined engine combustion section (31Y) that hydroelectrically generates power with a full-rotor impeller water turbine. The combined engine injection section (79K) starts landing on the moon. Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Turbine blade injection section (79K) equipped with a turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31X) that generates hydrodynamic power with reduced friction loss with a fully moving impeller water turbine Various energy storage cycle coalescing engines as various air suction jet drive equipment including landing start.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31Y) for generating friction loss reduced water generation with a fully-rotor impeller water turbine and a combined engine injection section (79K) moon surface Various energy storage cycle coalescing engines as various air suction jet drive equipment including landing start.   A turbine blade cross section (4F) with a tabine blade (8c) and a full blade combustion portion (32X) for hydroelectric power generation with a saddle type all blade water turbine and a combined engine injection section (79K) including various supersonic flights Various energy storage cycle coalescing engines as various air suction jet drive devices.   The turbine blade cross section (4F) has a tabine blade (8c) and a full blade combustion portion (32Y) for hydroelectric power generation using a vertical all blade water turbine, and a combined engine injection section (79K) includes various supersonic flights Various energy storage cycle coalescing engines as various air suction jet drive devices.   Turbine blade cross section (4F) with tabine blade (8c) and combined moving unit combustion unit (31X) for hydroelectric power generation with all-wheel impeller water turbine, combined engine injection unit (79K) various air including various supersonic flight Various energy storage cycle coalescing engines as suction injection drive devices.   Turbine blade cross section (4F) with tabine blade (8c) and combined engine combustion section (31Y) for hydroelectric power generation with all blade impeller water turbine, combined engine injection section (79K) various air including various supersonic flight Various energy storage cycle coalescing engines as suction injection drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion unit (31X) for hydroelectric power generation by a heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection unit (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various supersonic flight.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation by heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection section (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various supersonic flight.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and vertical all blade water turbine heating high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various supersonic flights.   Turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a heating and high-temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various supersonic flights.   Combined engine injection part (79K) with various supersonic speeds, including turbine blade (8c) with power generation technology with turbine blade cross section (4E) and full blade combustion part (32X) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various air suction / injection drive devices including flying.   Combined engine injection section (79K) with various supersonic speeds, including turbine blade (8c) of power generation technology with turbine blade cross section (4E) and full blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various air suction / injection drive devices including flying.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31X) for hydroelectric power generation with a full-rotor impeller water turbine and a combined engine injection section (79K) for various supersonic flights Various energy storage cycle coalescing engines including various air suction / injection drive devices.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation with a fully moving blade impeller water turbine, and a combined engine injection section (79K) for various supersonic flights Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and combined rotor combustion unit (31X) for reducing friction loss water power generation with all blade impeller water turbine, combined engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction jet drive devices including sonic flight.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion unit (31Y) for reducing friction loss water generation with a fully moving blade propeller water turbine, and a variety of combined engine injection units (79K) Various energy storage cycle coalescing engines as various air suction jet drive devices including sonic flight.   A turbine blade cross section (4F) with a tabine blade (8c) and a full blade combustion portion (32X) for hydroelectric power generation with a saddle type all blade water turbine and a combined engine injection section (79K) including various supersonic flights Various energy storage cycle coalescing engines as various air suction jet drive devices.   The turbine blade cross section (4F) has a tabine blade (8c) and a full blade combustion portion (32Y) for hydroelectric power generation using a vertical all blade water turbine, and a combined engine injection section (79K) includes various supersonic flights Various energy storage cycle coalescing engines as various air suction jet drive devices.   Turbine blade cross section (4F) with tabine blade (8c) and combined moving unit combustion unit (31X) for hydroelectric power generation with all-wheel impeller water turbine, combined engine injection unit (79K) various air including various supersonic flight Various energy storage cycle coalescing engines as suction injection drive devices.   Turbine blade cross section (4F) with tabine blade (8c) and combined engine combustion section (31Y) for hydroelectric power generation with all blade impeller water turbine, combined engine injection section (79K) various air including various supersonic flight Various energy storage cycle coalescing engines as suction injection drive devices.   A turbine blade (8c) of power generation technology having a turbine blade cross-section (4E) and a combined engine combustion unit (31X) for hydroelectric power generation by a heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection unit (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various supersonic flight.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation by heating high temperature means (3B) with all blade impeller water turbines and a combined engine injection section (79K) ) Various energy storage cycle coalescing engines as various air suction jet drive devices including various supersonic flight.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and vertical all blade water turbine heating high temperature means (3B) all blade combustion section (32X) for hydroelectric power generation, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various supersonic flights.   Turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a heating and high-temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices including various supersonic flights.   Combined engine injection part (79K) with various supersonic speeds, including turbine blade (8c) with power generation technology with turbine blade cross section (4E) and full blade combustion part (32X) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various air suction / injection drive devices including flying.   Combined engine injection section (79K) with various supersonic speeds, including turbine blade (8c) of power generation technology with turbine blade cross section (4E) and full blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various air suction / injection drive devices including flying.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31X) for hydroelectric power generation with a full-rotor impeller water turbine and a combined engine injection section (79K) for various supersonic flights Various energy storage cycle coalescing engines including various air suction / injection drive devices.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined engine combustion section (31Y) for hydroelectric power generation with a fully moving blade impeller water turbine, and a combined engine injection section (79K) for various supersonic flights Various energy storage cycle coalescing engines including various air suction / injection drive devices.   Turbine blade cross section (4E) and turbine blade (8c) of power generation technology and combined rotor combustion unit (31X) for reducing friction loss water power generation with all blade impeller water turbine, combined engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction jet drive devices including sonic flight.   A turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion unit (31Y) for reducing friction loss water generation with a fully moving blade propeller water turbine, and a variety of combined engine injection units (79K) Various energy storage cycle coalescing engines as various air suction jet drive devices including sonic flight.   Water including a turbine blade cross section (4F), a tabine blade (8c) and a whole blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine, including various methane hydrate decomposition and recovery facilities utilizing heat Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Water including a turbine blade cross section (4F), a tabine blade (8c) and a whole blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, including various thermal methane hydrate decomposition and recovery facilities Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Hydroelectric storage battery comprising a turbine blade section (4F) and a combined engine combustion section (31X) for hydroelectric power generation with a turbine blade turbine and a turbine blade section (4F), including various thermal methane hydrate decomposition and recovery facilities Various energy storage cycle coalescing engines as various rotational output drive devices.   Hydroelectric storage battery comprising a turbine blade section (4F) and a combined engine combustion section (31Y) for hydroelectric power generation with a turbine blade turbine and a turbine blade section (4F) and including various thermal methane hydrate decomposition and recovery facilities Various energy storage cycle coalescing engines as various rotational output drive devices.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined combustion unit (31X) for hydroelectric power generation by heating high temperature means (3B) with all blade impeller water turbines and various methane hydrates using heat Various energy storage cycle coalescing engines as hydroelectric storage battery driven various rotational output driving equipment including decomposition and recovery facilities.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation with all-wheel impeller water turbines and various methane hydrates utilizing thermal energy Various energy storage cycle coalescing engines as hydroelectric storage battery driven various rotational output driving equipment including decomposition and recovery facilities.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a whole blade combustion section (32X) for hydroelectric power generation with heating high temperature means (3B) by a vertical all blade water turbine Various energy storage cycle coalescing engines as hydroelectric storage battery driven various rotational output driving equipment including hydrate decomposition and recovery facilities.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a whole blade combustion section (32Y) for hydroelectric power generation with a high temperature heating means (3B) by a vertical all blade water turbine and various types of methane utilizing heat Various energy storage cycle coalescing engines as hydroelectric storage battery driven various rotational output driving equipment including hydrate decomposition and recovery facilities.   Turbine blade cross section (4E) power generation technology turbine blade (8c) and all blade combustion section (32X) that performs hydroelectric power generation with vertical all blade water turbine, various thermal methane hydrate decomposition and recovery facilities Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Turbine blades (8c) with power generation technology with turbine blade cross section (4E) and all blades combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, and various methane hydrate decomposition and recovery facilities utilizing thermal energy Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Includes turbine blade (8c) with power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31X) for hydroelectric power generation with all blade impeller water turbine, including various thermal methane hydrate decomposition and recovery facilities Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes turbine blade (8c) of power generation technology with turbine blade cross section (4E) and combined engine combustion section (31Y) for hydroelectric power generation with all blade impeller water turbine, including various thermal methane hydrate decomposition and recovery facilities Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and all-combined blade impeller water turbine combined coal combustion section (31X) for reducing friction loss hydroelectric power generation and various methane hydrate decomposition and recovery equipment using heat Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   Turbine blade cross section (4E) power generation technology turbine blade (8c) and all-combined blade impeller water turbine combined coal combustion section (31Y) for reducing friction loss hydroelectric power generation and various methane hydrate decomposition and recovery equipment using heat Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A variety of hydroelectric storage battery drives with various methane recovery and cooling using cold energy with a turbine blade cross section (4F) and a turbine blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines as rotary output drive equipment.   A variety of hydropower storage battery drives that include a turbine blade cross section (4F) and a turbine blade combustion section (32Y) for hydroelectric power generation by a vertical all blade water turbine with a turbine blade cross section (4F) and various methane recovery cooling using cold energy Various energy storage cycle coalescing engines as rotary output drive equipment.   Turbine blade cross section (4F) with a turbine blade (8c) and a combined engine combustion section (31X) for hydroelectric power generation with a fully moving blade propeller water turbine, and various rotational outputs driven by hydroelectric storage batteries including various methane recovery cooling using cold energy Various energy storage cycle coalescing engines as driving equipment.   Turbine blade cross section (4F) tabine blade (8c) and a combined engine combustion unit (31Y) for hydroelectric power generation with a fully moving blade bouncing water turbine, various rotational outputs for driving a hydroelectric storage battery including various methane recovery cooling using cold energy Various energy storage cycle coalescing engines as driving equipment.   Power generation technology turbine blade (8c) with turbine blade cross-section (4E) and heating blade high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation with water turbine, and various methane recovery cooling using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation with all blade impeller water turbines. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a all-blade combustion section (32X) for hydroelectric power generation by a high temperature heating means (3B) by a vertical all blade water turbine and various methane using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries including recovery cooling.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a all-blade combustion section (32Y) for hydroelectric power generation with a heating high temperature means (3B) by a vertical all blade water turbine and various methane using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries including recovery cooling.   Hydroelectric power generation including turbine blade (8c) of power generation technology with turbine blade cross section (4E) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, including various methane recovery cooling using cold energy Various energy storage cycle coalescing engine as storage battery driven various rotational output drive equipment.   Hydroelectric power generation including turbine blade (8c) of power generation technology with turbine blade cross section (4E) and full blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine including various methane recovery cooling using cold energy Various energy storage cycle coalescing engine as storage battery driven various rotational output drive equipment.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and a combined engine combustion section (31X) that generates hydroelectric power with all blade impeller water turbines and driving a hydroelectric storage battery that uses chill recovery and various methane recovery cooling Various energy storage cycle coalescing engines as various rotational output drive devices.   A hydroelectric storage battery drive that includes a turbine blade (8c) of power generation technology with a turbine blade cross-section (4E) and a combined engine combustion section (31Y) that hydroelectrically generates electricity with a full-rotor impeller water turbine and includes various methane recovery cooling using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   Water including turbine blade (8c) of power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31X) for reducing friction loss hydroelectric power generation with all blade impeller water turbine, including various methane recovery cooling using cold energy Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Water including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for generating friction loss hydroelectric power by a fully moving blade propeller water turbine and including various methane recovery cooling using cold energy Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   A variety of hydroelectric storage battery drives with various methane recovery and cooling using cold energy with a turbine blade cross section (4F) and a turbine blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines as rotary output drive equipment.   A variety of hydropower storage battery drives that include a turbine blade cross section (4F) and a turbine blade combustion section (32Y) for hydroelectric power generation by a vertical all blade water turbine with a turbine blade cross section (4F) and various methane recovery cooling using cold energy Various energy storage cycle coalescing engines as rotary output drive equipment.   Turbine blade cross section (4F) with a turbine blade (8c) and a combined engine combustion section (31X) for hydroelectric power generation with a fully moving blade propeller water turbine, and various rotational outputs driven by hydroelectric storage batteries including various methane recovery cooling using cold energy Various energy storage cycle coalescing engines as driving equipment.   Turbine blade cross section (4F) tabine blade (8c) and a combined engine combustion unit (31Y) for hydroelectric power generation with a fully moving blade bouncing water turbine, various rotational outputs for driving a hydroelectric storage battery including various methane recovery cooling using cold energy Various energy storage cycle coalescing engines as driving equipment.   Power generation technology turbine blade (8c) with turbine blade cross-section (4E) and heating blade high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation with water turbine, and various methane recovery cooling using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   A turbine blade (8c) of power generation technology with a turbine blade cross section (4E) and a combined high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation with all blade impeller water turbines. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a all-blade combustion section (32X) for hydroelectric power generation by a high temperature heating means (3B) by a vertical all blade water turbine and various methane using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries including recovery cooling.   A turbine blade (8c) of a power generation technology having a turbine blade cross section (4E) and a all-blade combustion section (32Y) for hydroelectric power generation with a heating high temperature means (3B) by a vertical all blade water turbine and various methane using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries including recovery cooling.   Hydroelectric power generation including turbine blade (8c) of power generation technology with turbine blade cross section (4E) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, including various methane recovery cooling using cold energy Various energy storage cycle coalescing engine as storage battery driven various rotational output drive equipment.   Hydroelectric power generation including turbine blade (8c) of power generation technology with turbine blade cross section (4E) and full blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine including various methane recovery cooling using cold energy Various energy storage cycle coalescing engine as storage battery driven various rotational output drive equipment.   Turbine blade cross section (4E) with power generation technology turbine blade (8c) and a combined engine combustion section (31X) that generates hydroelectric power with all blade impeller water turbines and driving a hydroelectric storage battery that uses chill recovery and various methane recovery cooling Various energy storage cycle coalescing engines as various rotational output drive devices.   A hydroelectric storage battery drive that includes a turbine blade (8c) of power generation technology with a turbine blade cross-section (4E) and a combined engine combustion section (31Y) that hydroelectrically generates electricity with a full-rotor impeller water turbine and includes various methane recovery cooling using cold energy Various energy storage cycle coalescing engines as various rotational output drive devices.   Water including turbine blade (8c) of power generation technology with turbine blade cross section (4E) and coalescence engine combustion section (31X) for reducing friction loss hydroelectric power generation with all blade impeller water turbine, including various methane recovery cooling using cold energy Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Water including a turbine blade (8c) of power generation technology having a turbine blade cross section (4E) and a combined engine combustion section (31Y) for generating friction loss hydroelectric power by a fully moving blade propeller water turbine and including various methane recovery cooling using cold energy Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   The whole blade combustion part (32X) and the turbine blade (8c) are made hollow by making the turbine blade cross-section (4A) close to the atmospheric pressure, the same speed, and the same calorie power at 910,000 times in the vertical blade-type water turbine (8B). Various energy storage cycle coalescing engine with heating high temperature means (3B).   The whole blade combustion part (32Y) and the turbine blade (8c) are made hollow by making the turbine blade cross section (4A) close to the atmospheric pressure, the same speed, and the same calorific power, with the vertical blade water turbine (8B). Various energy storage cycle coalescing engine with heating high temperature means (3B).   The combined turbine combustion section (31Y) and the turbine blade (8c) are heated to a high temperature by bringing the turbine blade cross section (4A) close to the atmospheric pressure, the same speed, and the same caloric power at 910,000 times in the all blade impeller water turbine (8b). Various energy storage cycle coalescing engines provided with means (3B).   The combined turbine combustion section (31X) and the turbine blade (8c) are heated to a high temperature by making the turbine blade cross section (4A) close to the atmospheric pressure, the same speed, and the same caloric power at 910,000 times in the all-blade spring vehicle water turbine (8b). Various energy storage cycle coalescing engines provided with means (3B).   The whole blade combustion part (32X) and the turbine blade (8c) are made hollow by making the turbine blade cross-section (4A) close to the atmospheric pressure, the same speed, and the same calorie power at 910,000 times in the vertical blade-type water turbine (8B). Various energy storage cycle coalescing engines that are provided with heating high temperature means (3B) to increase the heating temperature.   The whole blade combustion part (32Y) and the turbine blade (8c) are made hollow by making the turbine blade cross section (4A) close to the atmospheric pressure, the same speed, and the same calorific power, with the vertical blade water turbine (8B). Various energy storage cycle coalescing engines that are provided with heating high temperature means (3B) to increase the heating temperature.   The combined turbine combustion section (31Y) and the turbine blade (8c) are heated to a high temperature by bringing the turbine blade cross section (4A) close to the atmospheric pressure, the same speed, and the same caloric power at 910,000 times in the all blade impeller water turbine (8b). Various energy storage cycle coalescing engines that are provided with means (3B) and are heated to high temperatures.   The combined turbine combustion section (31X) and the turbine blade (8c) are heated to a high temperature by making the turbine blade cross section (4A) close to the atmospheric pressure, the same speed, and the same caloric power at 910,000 times in the all-blade spring vehicle water turbine (8b). Various energy storage cycle coalescing engines that are provided with means (3B) and are heated to high temperatures.   The whole blade combustion part (32X) and the turbine blade (8c) are made hollow by making the turbine blade cross-section (4A) close to the atmospheric pressure, the same speed, and the same calorie power at 910,000 times in the vertical blade-type water turbine (8B). Various energy storage cycle coalescing engines which are provided with heating high temperature means (3B) to make the electrical resistance heating high temperature.   The whole blade combustion part (32Y) and the turbine blade (8c) are made hollow by making the turbine blade cross section (4A) close to the atmospheric pressure, the same speed, and the same calorific power, with the vertical blade water turbine (8B). Various energy storage cycle coalescing engines which are provided with heating high temperature means (3B) to make the electrical resistance heating high temperature.   The combined turbine combustion section (31Y) and the turbine blade (8c) are heated to a high temperature by bringing the turbine blade cross section (4A) close to the atmospheric pressure, the same speed, and the same caloric power at 910,000 times in the all blade impeller water turbine (8b). Various energy storage cycle coalescing engines which are provided with means (3B) to make electric resistance heating high temperature.   The combined turbine combustion section (31X) and the turbine blade (8c) are heated to a high temperature by making the turbine blade cross section (4A) close to the atmospheric pressure, the same speed, and the same caloric power at 910,000 times in the all-blade spring vehicle water turbine (8b). Various energy storage cycle coalescing engines which are provided with means (3B) to make electric resistance heating high temperature.   The whole blade combustion part (32X) and the turbine blade (8c) are made hollow by making the turbine blade cross-section (4A) close to the atmospheric pressure, the same speed, and the same calorie power at 910,000 times in the vertical blade-type water turbine (8B). Various energy storage cycle coalescing engines which are provided with heating high temperature means (3B) to make electromagnetic heating high temperature.   The whole blade combustion part (32Y) and the turbine blade (8c) are made hollow by making the turbine blade cross section (4A) close to the atmospheric pressure, the same speed, and the same calorific power, with the vertical blade water turbine (8B). Various energy storage cycle coalescing engines which are provided with heating high temperature means (3B) to make electromagnetic heating high temperature.   The combined turbine combustion section (31Y) and the turbine blade (8c) are heated to a high temperature by bringing the turbine blade cross section (4A) close to the atmospheric pressure, the same speed, and the same caloric power at 910,000 times in the all blade impeller water turbine (8b). Various energy storage cycle coalescing engines that are provided with means (3B) to make electromagnetic heating high temperature.   The combined turbine combustion section (31X) and the turbine blade (8c) are heated to a high temperature by making the turbine blade cross section (4A) close to the atmospheric pressure, the same speed, and the same caloric power at 910,000 times in the all-blade spring vehicle water turbine (8b). Various energy storage cycle coalescing engines that are provided with means (3B) to make electromagnetic heating high temperature.   The whole blade combustion part (32X) and the turbine blade (8c) are made hollow by making the turbine blade cross-section (4A) close to the atmospheric pressure, the same speed, and the same calorie power at 910,000 times in the vertical blade-type water turbine (8B). Various energy storage cycle coalescing engines in which a high temperature heating means (3B) is provided in the hollow portion to make electromagnetic heating high temperature.   The whole blade combustion part (32Y) and the turbine blade (8c) are made hollow by making the turbine blade cross section (4A) close to the atmospheric pressure, the same speed, and the same calorific power, with the vertical blade water turbine (8B). Various energy storage cycle coalescing engines in which a high temperature heating means (3B) is provided in the hollow portion to make electromagnetic heating high temperature.   Combined combustion unit (31Y) and turbine blade (8c) into hollow section by bringing turbine blade cross section (4A) close to atmospheric pressure, same speed, and same calorie power at 910,000 times in all blade impeller water turbine (8b) A high temperature heating means (3B) is provided to the electromagnetic heating high temperature combined cycle engine.   Combined engine combustion part (31X) with turbine blade cross section (4A) to make the turbine blade cross section (4A) close to 910,000 times the atmospheric pressure, the same speed, and the same calorific power in the whole blade impeller water turbine (8b) A high temperature heating means (3B) is provided to the electromagnetic heating high temperature combined cycle engine.   The whole blade combustion part (32X) and the turbine blade (8c) are made hollow by making the turbine blade cross-section (4A) close to the atmospheric pressure, the same speed, and the same calorie power at 910,000 times in the vertical blade-type water turbine (8B). Various energy storage cycle coalescing engines in which a high temperature heating means (3B) is provided in the hollow portion to make the electrical resistance heating high temperature.   The whole blade combustion part (32Y) and the turbine blade (8c) are made hollow by making the turbine blade cross section (4A) close to the atmospheric pressure, the same speed, and the same calorific power, with the vertical blade water turbine (8B). Various energy storage cycle coalescing engines in which a high temperature heating means (3B) is provided in the hollow portion to make the electrical resistance heating high temperature.   Combined combustion unit (31Y) and turbine blade (8c) into hollow section by bringing turbine blade cross section (4A) close to atmospheric pressure, same speed, and same calorie power at 910,000 times in all blade impeller water turbine (8b) A high temperature heating means (3B) is provided to the electric resistance heating high temperature coalescing engine.   Combined engine combustion part (31X) with turbine blade cross section (4A) to make the turbine blade cross section (4A) close to 910,000 times the atmospheric pressure, the same speed, and the same calorific power in the whole blade impeller water turbine (8b) A high temperature heating means (3B) is provided to the electric energy heating high temperature combined cycle engine.   The whole blade combustion part (32X) and the turbine blade (8c) are made hollow by making the turbine blade cross-section (4A) close to the atmospheric pressure, the same speed, and the same calorie power at 910,000 times in the vertical blade-type water turbine (8B). Various energy storage cycle coalescing engines in which a heating high temperature means (3B) is provided in the hollow portion to make the electric resistance heating high temperature to generate a rotational output by rolling contact.   The whole blade combustion part (32Y) and the turbine blade (8c) are made hollow by making the turbine blade cross section (4A) close to the atmospheric pressure, the same speed, and the same calorific power, with the vertical blade water turbine (8B). Various energy storage cycle coalescing engines in which a heating high temperature means (3B) is provided in the hollow portion to make the electric resistance heating high temperature to generate a rotational output by rolling contact.   Combined combustion unit (31Y) and turbine blade (8c) into hollow section by bringing turbine blade cross section (4A) close to atmospheric pressure, same speed, and same calorie power at 910,000 times in all blade impeller water turbine (8b) A high temperature heating means (3B) is provided to the electric resistance heating high temperature, and various energy storage cycle coalescing engines that generate rotational output by rolling contact.   Combined engine combustion part (31X) with turbine blade cross section (4A) to make the turbine blade cross section (4A) close to 910,000 times the atmospheric pressure, the same speed, and the same calorific power in the whole blade impeller water turbine (8b) A high temperature heating means (3B) is provided to the electric resistance heating high temperature, and various energy storage cycle coalescing engines that generate rotational output by rolling contact.   The whole blade combustion part (32X) and the turbine blade (8c) are made hollow by making the turbine blade cross-section (4A) close to the atmospheric pressure, the same speed, and the same calorie power at 910,000 times in the vertical blade-type water turbine (8B). Various energy storage cycle coalescing engines in which a heating high temperature means (3B) is provided in the hollow portion to generate electromagnetic heating to generate a rotational output by rolling contact.   The whole blade combustion part (32Y) and the turbine blade (8c) are made hollow by making the turbine blade cross section (4A) close to the atmospheric pressure, the same speed, and the same calorific power, with the vertical blade water turbine (8B). Various energy storage cycle coalescing engines in which a heating high temperature means (3B) is provided in the hollow portion to generate electromagnetic heating to generate a rotational output by rolling contact.   Combined combustion unit (31Y) and turbine blade (8c) into hollow section by bringing turbine blade cross section (4A) close to atmospheric pressure, same speed, and same calorie power at 910,000 times in all blade impeller water turbine (8b) A high temperature heating means (3B) is provided to the electromagnetic heating high temperature and various energy storage cycle coalescence engines that generate rotational output by rolling contact.   Combined engine combustion part (31X) with turbine blade cross section (4A) to make the turbine blade cross section (4A) close to 910,000 times the atmospheric pressure, the same speed, and the same calorific power in the whole blade impeller water turbine (8b) A high temperature heating means (3B) is provided to the electromagnetic heating high temperature and various energy storage cycle coalescence engines that generate rotational output by rolling contact.   The whole blade combustion part (32X) and the turbine blade (8c) are made hollow by making the turbine blade cross-section (4A) close to the atmospheric pressure, the same speed, and the same calorie power at 910,000 times in the vertical blade-type water turbine (8B). Various energy storage cycle coalescing engines that generate a rotating output in which a high-temperature heating means (3B) is provided in the hollow portion to reduce the friction loss by increasing the electromagnetic heating temperature.   The whole blade combustion part (32Y) and the turbine blade (8c) are made hollow by making the turbine blade cross section (4A) close to the atmospheric pressure, the same speed, and the same calorific power, with the vertical blade water turbine (8B). Various energy storage cycle coalescing engines that generate a rotating output in which a high-temperature heating means (3B) is provided in the hollow portion to reduce the friction loss by increasing the electromagnetic heating temperature.   Combined combustion unit (31Y) and turbine blade (8c) into hollow section by bringing turbine blade cross section (4A) close to atmospheric pressure, same speed, and same calorie power at 910,000 times in all blade impeller water turbine (8b) Various energy storage cycle coalescing engines that generate rotational output with reduced friction loss by providing high temperature heating means (3B) to the electromagnetic heating temperature.   Combined engine combustion part (31X) with turbine blade cross section (4A) to make the turbine blade cross section (4A) close to 910,000 times the atmospheric pressure, the same speed, and the same calorific power in the whole blade impeller water turbine (8b) Various energy storage cycle coalescing engines that generate rotational output with reduced friction loss by providing high temperature heating means (3B) to the electromagnetic heating temperature.   The whole blade combustion part (32X) and the turbine blade (8c) are made hollow by making the turbine blade cross-section (4A) close to the atmospheric pressure, the same speed, and the same calorie power at 910,000 times in the vertical blade-type water turbine (8B). Various energy storage cycle coalescing engines that generate a rotating output in which a high-temperature heating means (3B) is provided in the hollow portion to reduce friction loss by increasing the electric resistance heating temperature.   The whole blade combustion part (32Y) and the turbine blade (8c) are made hollow by making the turbine blade cross section (4A) close to the atmospheric pressure, the same speed, and the same calorific power, with the vertical blade water turbine (8B). Various energy storage cycle coalescing engines that generate a rotating output in which a high-temperature heating means (3B) is provided in the hollow portion to reduce friction loss by increasing the electric resistance heating temperature.   Combined combustion unit (31Y) and turbine blade (8c) into hollow section by bringing turbine blade cross section (4A) close to atmospheric pressure, same speed, and same calorie power at 910,000 times in all blade impeller water turbine (8b) A high-temperature heating means (3B) is provided to the electric resistance heating high temperature to produce a rotational output with reduced friction loss.   Combined engine combustion part (31X) with turbine blade cross section (4A) to make the turbine blade cross section (4A) close to 910,000 times the atmospheric pressure, the same speed, and the same calorific power in the whole blade impeller water turbine (8b) A high-temperature heating means (3B) is provided to the electric resistance heating high temperature to produce a rotational output with reduced friction loss.   The total blade combustion part (32X) of the inner blade group (60C) of the vertical blade water turbine (8B) is made to have a turbine blade cross section (4A) with the atmospheric pressure, the same speed, and the same caloric power as close to 910,000 times. Turbine blade cross section (4A) Various energy storage cycle coalescing engines with a bearing (80) capable of aiming for a 910,000-fold work rate and generating rotational output.   The total blade combustion part (32Y) inner rotor blade group (60C) of the vertical blade water turbine (8B) has a turbine blade cross section (4A) with the atmospheric pressure, the same speed, and the same caloric power as close to 910,000 times. Various energy storage cycle coalescing engines that provide rotational output by providing bearings (80) capable of 910,000 times work rate.   Combined engine combustion section (31Y) cylindrical body (8e) 910,000 of turbine blades with turbine blade cross-section (4A) approaching 910,000 times the atmospheric pressure, the same speed, and the same calorific power at the whole turbine blade turbine water turbine (8b) Various energy storage cycle coalescing engines that provide rotational output by providing a bearing (80) capable of double work rate.   Combined engine combustion section (31X) cylindrical body (8e) turbine blade of turbine blade with full rotor blade water turbine (8b) to make the turbine blade cross section (4A) close to the atmospheric pressure, the same speed, and the same caloric power Cross section (4A) Various energy storage cycle coalescing engines that provide rotational output by providing bearings (80) that can aim for 910,000 times power.   Vertical turbine blade water turbine (8B) All blade combustion section (32X) Outer blade group (60D) Turbine blade cross section (4A) 910,000 times workability can be aimed and bearing (80) is provided for rotation output Various energy conservation cycle coalescence engine that generates   Vertically moving blade water turbine (8B) All blade combustion section (32Y) Outer blade group (60D) turbine blade cross section (4A) 910,000 times work rate can be aimed and bearing (80) is provided for rotation output Various energy conservation cycle coalescence engine that generates   All blade impeller water turbine (8b) Combined engine combustion section (31X) Cylindrical trunk (8e) Turbine blade cross section (4A) 910,000 times workable bearing (80) provided for rolling contact rotation output Various energy conservation cycle coalescence engine that generates   All-wheel impeller water turbine (8b) Combined engine combustion section (31Y) Cylindrical body (8e) Turbine blade cross section (4A) 910,000 times workable bearing (80) is provided for rolling contact rotation output Various energy conservation cycle coalescence engine that generates   Vertical rotor blade water turbine (8B) All blade combustion section (32X) Inner blade group (60C) turbine blade cross section (4A) Rolling contact by providing a bearing (80) capable of targeting 910,000 times work rate Various energy storage cycle coalescing engines that generate rotational output.   Vertical rotor blade water turbine (8B) All blade combustion section (32Y) Inner blade group (60C) turbine blade cross section (4A) Rolling contact with bearing (80) capable of targeting 910,000 times work rate Various energy storage cycle coalescing engines that generate rotational output.   Vertical rotor blade water turbine (8B) Whole blade combustion section (32X) Outer blade group (60D) turbine blade cross section (4A) Rolling contact by providing bearing (80) capable of aiming for 910,000 times work rate Various energy storage cycle coalescing engines that generate rotational output.   Vertical rotor blade water turbine (8B) All blade combustion section (32Y) Outer blade group (60D) turbine blade cross section (4A) Rolling contact with bearing (80) to enable 910,000 times workability target Various energy storage cycle coalescing engines that generate rotational output.   Various energy storage cycle coalescing engine that injects the whole blade combustion part (32X) high temperature water (52b) vertically downward and further accelerates the gravitational acceleration, and injects 910,000 times power turbine blade cross section (4A) turbine blade (8c).   Various energy storage cycle coalescing engine that injects the whole blade combustion part (32Y) high temperature water (52b) vertically downward and further accelerates the gravitational acceleration, and injects 910,000 times power turbine blade cross section (4A) turbine blade (8c).   Combined engine combustion section (31X) High-temperature water (52b) is vertically accelerated and injected with acceleration of gravitational acceleration, 910,000 times power turbine blade cross section (4A) and various energy storage cycle coalescing engines that inject into turbine blade (8c).   Combined engine combustion section (31Y) High-temperature water (52b) is vertically accelerated and injected with acceleration of gravitational acceleration, 910,000 times power turbine blade cross section (4A) and various energy storage cycle coalescing engines that inject into turbine blade (8c).   Whole blade combustion part (32X) high-temperature water (52b) injected vertically downward, acceleration of gravitational acceleration, thrust bearing capable of 910,000 times work rate (80a) turbine blade cross section (4A) turbine blade (8c) Various energy conservation cycle coalescing engines.   Whole blade combustion part (32Y) High-temperature water (52b) is injected vertically downward to accelerate acceleration of gravitational acceleration, thrust bearing capable of targeting 910,000 times power (80a), turbine blade cross section (4A), turbine blade (8c) Various energy conservation cycle coalescing engines.   Combined engine combustion section (31X) high-temperature water (52b) is injected vertically downward into a thrust bearing (80a) turbine blade cross section (4A) turbine blade (8c) capable of aiming for additional acceleration of gravitational acceleration and 910,000 times power Various energy conservation cycle coalescence engine.   Combined engine combustion part (31Y) high-temperature water (52b) is injected vertically downward into a thrust bearing (80a) turbine blade cross section (4A) turbine blade (8c) capable of further acceleration of acceleration of gravitational acceleration and 910,000 times power Various energy conservation cycle coalescence engine.   Whole blade combustion part (32X) high-temperature water (52b) injected vertically downward, acceleration of gravitational acceleration, thrust bearing capable of 910,000 times work rate (80a) turbine blade cross section (4A) turbine blade (8c) Various energy storage cycle coalescing engines that drive the vertical all blade water turbine (8B).   Whole blade combustion part (32Y) High-temperature water (52b) is injected vertically downward to accelerate acceleration of gravitational acceleration, thrust bearing capable of targeting 910,000 times power (80a), turbine blade cross section (4A), turbine blade (8c) Various energy storage cycle coalescing engines that drive the vertical all blade water turbine (8B).   Combined engine combustion section (31X) high-temperature water (52b) injected vertically downward, additional acceleration of gravitational acceleration, thrust bearing capable of targeting 910,000 times power (80a) turbine blade cross section (4A) turbine blade (8c) all injected Various energy storage cycle coalescing engines that drive the bucket impeller water turbine (8b).   Combined engine combustion part (31Y) High-temperature water (52b) is injected vertically downward to accelerate acceleration of gravity acceleration, thrust bearing capable of aiming for 910,000 times power (80a) turbine blade cross section (4A) turbine blade (8c) all injected Various energy storage cycle coalescing engines that drive the bucket impeller water turbine (8b).   Whole blade combustion part (32X) high-temperature water (52b) injected vertically downward, acceleration of gravitational acceleration, thrust bearing capable of 910,000 times work rate (80a) turbine blade cross section (4A) turbine blade (8c) Various energy storage cycle coalescing engine that drives vertical all blade water turbine (8B) with vaporization explosive force.   Whole blade combustion part (32Y) High-temperature water (52b) is injected vertically downward to accelerate acceleration of gravitational acceleration, thrust bearing capable of targeting 910,000 times power (80a), turbine blade cross section (4A), turbine blade (8c) Various energy storage cycle coalescing engine that drives vertical all blade water turbine (8B) with vaporization explosive force.   Combined engine combustion section (31X) high-temperature water (52b) injected vertically downward, additional acceleration of gravitational acceleration, thrust bearing capable of targeting 910,000 times power (80a) turbine blade cross section (4A) turbine blade (8c) all injected Various energy storage cycle coalescing engine that drives the bucket turbine water turbine (8b) with vaporization explosive force.   Combined engine combustion part (31Y) High-temperature water (52b) is injected vertically downward to accelerate acceleration of gravity acceleration, thrust bearing capable of aiming for 910,000 times power (80a) turbine blade cross section (4A) turbine blade (8c) all injected Various energy storage cycle coalescing engine that drives the bucket turbine water turbine (8b) with vaporization explosive force.   Whole blade combustion part (32X) high-temperature water (52b) injected vertically downward, acceleration of gravitational acceleration, thrust bearing capable of 910,000 times work rate (80a) turbine blade cross section (4A) turbine blade (8c) A combined energy storage cycle engine that drives a vertical all blade water turbine (8B) with vaporization explosive force and cools its exhaust with cold (52e).   Whole blade combustion part (32Y) High-temperature water (52b) is injected vertically downward to accelerate acceleration of gravitational acceleration, thrust bearing capable of targeting 910,000 times power (80a), turbine blade cross section (4A), turbine blade (8c) A combined energy storage cycle engine that drives a vertical all blade water turbine (8B) with vaporization explosive force and cools its exhaust with cold (52e).   Combined engine combustion section (31X) high-temperature water (52b) injected vertically downward, additional acceleration of gravitational acceleration, thrust bearing capable of targeting 910,000 times power (80a) turbine blade cross section (4A) turbine blade (8c) all injected Various energy storage cycle coalescing engines that drive the bucket turbine water turbine (8b) with vaporization explosive force and cool the exhaust with cold (52e).   Combined engine combustion part (31Y) High-temperature water (52b) is injected vertically downward to accelerate acceleration of gravity acceleration, thrust bearing capable of aiming for 910,000 times power (80a) turbine blade cross section (4A) turbine blade (8c) all injected Various energy storage cycle coalescing engines that drive the bucket turbine water turbine (8b) with vaporization explosive force and cool the exhaust with cold (52e).   Whole blade combustion part (32X) high-temperature water (52b) injected vertically downward, acceleration of gravitational acceleration, thrust bearing capable of 910,000 times work rate (80a) turbine blade cross section (4A) turbine blade (8c) A combined energy storage cycle engine that drives a vertical all blade water turbine (8B) with vaporization explosive force and cools its exhaust with compressed air cooling (52e).   Whole blade combustion part (32Y) High-temperature water (52b) is injected vertically downward to accelerate acceleration of gravitational acceleration, thrust bearing capable of targeting 910,000 times power (80a), turbine blade cross section (4A), turbine blade (8c) A combined energy storage cycle engine that drives a vertical all blade water turbine (8B) with vaporization explosive force and cools its exhaust with compressed air cooling (52e).   Combined engine combustion section (31X) high-temperature water (52b) injected vertically downward, additional acceleration of gravitational acceleration, thrust bearing capable of targeting 910,000 times power (80a) turbine blade cross section (4A) turbine blade (8c) all injected Various energy storage cycle coalescing engines which drive the bucket turbine water turbine (8b) with vaporization explosive force and cool the exhaust with compressed air cooling (52e).   Combined engine combustion part (31Y) High-temperature water (52b) is injected vertically downward to accelerate acceleration of gravity acceleration, thrust bearing capable of aiming for 910,000 times power (80a) turbine blade cross section (4A) turbine blade (8c) all injected Various energy storage cycle coalescing engines which drive the bucket turbine water turbine (8b) with vaporization explosive force and cool the exhaust with compressed air cooling (52e).   Whole blade combustion part (32X) high-temperature water (52b) injected vertically downward, acceleration of gravitational acceleration, thrust bearing capable of 910,000 times work rate (80a) turbine blade cross section (4A) turbine blade (8c) A combined energy storage cycle engine that drives a vertical all-blade water turbine (8B) with vaporization explosive force and cools its exhaust with combustion gas cold (52e).   Whole blade combustion part (32Y) High-temperature water (52b) is injected vertically downward to accelerate acceleration of gravitational acceleration, thrust bearing capable of targeting 910,000 times power (80a), turbine blade cross section (4A), turbine blade (8c) Various energy storage cycle coalescing engines that drive a vertical all-blade water turbine (8B) with vaporization explosive power and cool its exhaust with combustion gas cold (52e).   Combined engine combustion section (31X) high-temperature water (52b) injected vertically downward, additional acceleration of gravitational acceleration, thrust bearing capable of targeting 910,000 times power (80a) turbine blade cross section (4A) turbine blade (8c) all injected Various energy storage cycle coalescing engines which drive the bucket turbine water turbine (8b) with the vaporization explosive force and cool the exhaust with the combustion gas cold (52e).   Combined engine combustion part (31Y) High-temperature water (52b) is injected vertically downward to accelerate acceleration of gravity acceleration, thrust bearing capable of aiming for 910,000 times power (80a) turbine blade cross section (4A) turbine blade (8c) all injected Various energy storage cycle coalescing engines which drive the bucket turbine water turbine (8b) with the vaporization explosive force and cool the exhaust with the combustion gas cold (52e).   Combined engine combustion section (31X) high-temperature water (52b) injected vertically downward, additional acceleration of gravitational acceleration, thrust bearing capable of targeting 910,000 times power (80a) turbine blade cross section (4A) turbine blade (8c) all injected Various energy storage cycle coalescing engines that drive the bucket turbine water turbine (8b) with vaporization explosive force and cool the exhaust with cold combustion gas (52e) and high vacuum.   Combined engine combustion part (31Y) High-temperature water (52b) is injected vertically downward to accelerate acceleration of gravity acceleration, thrust bearing capable of aiming for 910,000 times power (80a) turbine blade cross section (4A) turbine blade (8c) all injected Various energy storage cycle coalescing engines that drive the bucket turbine water turbine (8b) with vaporization explosive force and cool the exhaust with cold combustion gas (52e) and high vacuum.   Whole blade combustion part (32X) high-temperature water (52b) injected vertically downward, acceleration of gravitational acceleration, thrust bearing capable of 910,000 times work rate (80a) turbine blade cross section (4A) turbine blade (8c) A combined energy storage cycle engine that drives a vertical all-blade water turbine (8B) with vaporization explosive power and cools its exhaust with combustion gas cold (52e) to high vacuum.   Whole blade combustion part (32Y) High-temperature water (52b) is injected vertically downward to accelerate acceleration of gravitational acceleration, thrust bearing capable of targeting 910,000 times power (80a), turbine blade cross section (4A), turbine blade (8c) A combined energy storage cycle engine that drives a vertical all-blade water turbine (8B) with vaporization explosive power and cools its exhaust with combustion gas cold (52e) to high vacuum.   Whole blade combustion part (32X) high-temperature water (52b) injected vertically downward, acceleration of gravitational acceleration, thrust bearing capable of 910,000 times work rate (80a) turbine blade cross section (4A) turbine blade (8c) A variety of energy storage cycle coalescence engine that drives a vertical all-blade water turbine (8B) with vaporization explosive force and cools its exhaust with combustion gas cold heat (52e).   Whole blade combustion part (32Y) High-temperature water (52b) is injected vertically downward to accelerate acceleration of gravitational acceleration, thrust bearing capable of targeting 910,000 times power (80a), turbine blade cross section (4A), turbine blade (8c) A variety of energy storage cycle coalescence engine that drives a vertical all-blade water turbine (8B) with vaporization explosive force and cools its exhaust with combustion gas cold heat (52e).   Combined engine combustion section (31X) high-temperature water (52b) injected vertically downward, additional acceleration of gravitational acceleration, thrust bearing capable of targeting 910,000 times power (80a) turbine blade cross section (4A) turbine blade (8c) all injected Various energy storage cycle coalescing engines that drive the bucket turbine water turbine (8b) with the vaporization explosive force and cool the exhaust with the combustion gas cold (52e) to the highest vacuum.   Combined engine combustion part (31Y) High-temperature water (52b) is injected vertically downward to accelerate acceleration of gravity acceleration, thrust bearing capable of aiming for 910,000 times power (80a) turbine blade cross section (4A) turbine blade (8c) all injected Various energy storage cycle coalescing engines that drive the bucket turbine water turbine (8b) with the vaporization explosive force and cool the exhaust with the combustion gas cold (52e) to the highest vacuum.   Combined engine combustion section (31X) high-temperature water (52b) injected vertically downward, additional acceleration of gravitational acceleration, thrust bearing capable of targeting 910,000 times power (80a) turbine blade cross section (4A) turbine blade (8c) all injected Various energy storage cycle coalescing engines that drive the bucket turbine water turbine (8b) with the vaporization explosive force and make the exhaust gas cool with the combustion gas cold (52e) and the maximum rotation output of the maximum vacuum.   Combined engine combustion part (31Y) High-temperature water (52b) is injected vertically downward to accelerate acceleration of gravity acceleration, thrust bearing capable of aiming for 910,000 times power (80a) turbine blade cross section (4A) turbine blade (8c) all injected Various energy storage cycle coalescing engines that drive the bucket turbine water turbine (8b) with the vaporization explosive force and make the exhaust gas cool with the combustion gas cold (52e) and the maximum rotation output of the maximum vacuum.   Whole blade combustion part (32X) high-temperature water (52b) injected vertically downward, acceleration of gravitational acceleration, thrust bearing capable of 910,000 times work rate (80a) turbine blade cross section (4A) turbine blade (8c) A combined energy storage cycle engine that drives a vertical all-blade water turbine (8B) with vaporization explosive force and that exhausts are cooled by combustion gas cold (52e) to achieve maximum vacuum maximum rotation output.   Whole blade combustion part (32Y) High-temperature water (52b) is injected vertically downward to accelerate acceleration of gravitational acceleration, thrust bearing capable of targeting 910,000 times power (80a), turbine blade cross section (4A), turbine blade (8c) A combined energy storage cycle engine that drives a vertical all-blade water turbine (8B) with vaporization explosive force and that exhausts are cooled by combustion gas cold (52e) to achieve maximum vacuum maximum rotation output.   Turbine blade cross section (4B) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, various rotating outputs driven by hydroelectric storage battery Various energy storage cycle coalescing engines as driving equipment.   Turbine blade cross section capable of 910,000 times power (4B) Turbine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine and various rotational outputs driven by hydroelectric storage battery Various energy storage cycle coalescing engines as driving equipment.   Turbine blade cross-section (4B) capable of 910,000 times power, turbine blade (8c), and combined rotor combustion unit (31X) for hydroelectric power generation by all-wheel impeller water turbine A variety of energy conservation cycle coalescence engine.   Turbine blade cross-section (4B) capable of 910,000 times power and turbine blade (8c) and combined engine combustion section (31Y) for hydroelectric power generation with all blade impeller water turbines and various rotational output drive equipment driven by hydroelectric storage battery A variety of energy conservation cycle coalescence engine.   Turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined turbine combustion section (31X) for hydroelectric power generation by heating high temperature means (3B) with all blade impeller water turbine Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power and hydroelectric storage battery having a combined engine combustion section (31Y) for hydroelectric power generation by heating high temperature means (3B) with all blade impeller water turbine with turbine blade (8c) Various energy storage cycle coalescing engines as various rotational output drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a vertical blade-type all-blade water turbine are equipped with a high-temperature heating means (3B) all-blade combustion section (32X) for hydroelectric power generation. Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a vertical blade-type all-blade water turbine are equipped with a heating blade high temperature means (3B) all blade combustion section (32Y) for hydroelectric power generation and water Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Turbine blade cross section (4C) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, and various rotational outputs driven by hydroelectric storage battery Various energy storage cycle coalescing engines as driving equipment.   Turbine blade cross section (4C) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, various rotation output driven by hydroelectric storage battery Various energy storage cycle coalescing engines as driving equipment.   Turbine blade cross-section (4C) capable of 910,000 times power, combined with a combined engine combustion section (31X) for hydroelectric power generation with a turbine blade (8c) and an all-wheel impeller water turbine, various rotational output drive devices driven by hydroelectric storage batteries A variety of energy conservation cycle coalescence engine.   Turbine blade cross-section (4C) capable of 910,000 times power and a combined engine combustion section (31Y) for hydroelectric power generation with a turbine blade (8c) and all-wheel impeller water turbine, and various rotational output drive devices driven by hydroelectric storage batteries A variety of energy conservation cycle coalescence engine.   Turbine blade cross section capable of 910,000 times power (4C) Turbine blade (8c) and All-Boiled Shake Wheel Turbine Water Turbine Combined Engine Combustion Unit (31X) for reducing friction loss and various rotations driven by hydroelectric storage battery Various energy storage cycle coalescence engine as output drive equipment.   Turbine blade cross-section (4C) capable of 910,000 times work rate and turbine blade (8c) and combined rotor combustion unit (31Y) for hydroelectric power generation with reduced friction loss by all blade impeller water turbine, various rotations driven by hydroelectric storage battery Various energy storage cycle coalescence engine as output drive equipment.   Turbine blade cross section (4B) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, various rotating outputs driven by hydroelectric storage battery Various energy storage cycle coalescing engines as driving equipment.   Turbine blade cross section capable of 910,000 times power (4B) Turbine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine and various rotational outputs driven by hydroelectric storage battery Various energy storage cycle coalescing engines as driving equipment.   Turbine blade cross-section (4B) capable of 910,000 times power, turbine blade (8c), and combined rotor combustion unit (31X) for hydroelectric power generation with all-wheel impeller wheel water turbines and various rotational output drive devices driven by hydroelectric storage batteries A variety of energy conservation cycle coalescing engines.   Turbine blade cross-section (4B) capable of 910,000 times power and turbine blade (8c) and combined engine combustion section (31Y) for hydroelectric power generation with all blade impeller water turbines and various rotational output drive equipment driven by hydroelectric storage battery A variety of energy conservation cycle coalescence engine.   Turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined turbine combustion section (31X) for hydroelectric power generation by heating high temperature means (3B) with all blade impeller water turbine Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power and hydroelectric storage battery having a combined engine combustion section (31Y) for hydroelectric power generation by heating high temperature means (3B) with all blade impeller water turbine with turbine blade (8c) Various energy storage cycle coalescing engines as various rotational output drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a vertical blade-type all-blade water turbine are equipped with a high-temperature heating means (3B) all-blade combustion section (32X) for hydroelectric power generation. Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a vertical blade-type all-blade water turbine are equipped with a heating blade high temperature means (3B) all blade combustion section (32Y) for hydroelectric power generation and water Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Turbine blade cross section (4C) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, and various rotational outputs driven by hydroelectric storage battery Various energy storage cycle coalescing engines as driving equipment.   Turbine blade cross section (4C) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, various rotation output driven by hydroelectric storage battery Various energy storage cycle coalescing engines as driving equipment.   Turbine blade cross-section (4C) capable of 910,000 times power, combined with a combined engine combustion section (31X) for hydroelectric power generation with a turbine blade (8c) and an all-wheel impeller water turbine, various rotational output drive devices driven by hydroelectric storage batteries A variety of energy conservation cycle coalescence engine.   Turbine blade cross-section (4C) capable of 910,000 times power and a combined engine combustion section (31Y) for hydroelectric power generation with a turbine blade (8c) and all-wheel impeller water turbine, and various rotational output drive devices driven by hydroelectric storage batteries A variety of energy conservation cycle coalescence engine.   Turbine blade cross section capable of 910,000 times power (4C) Turbine blade (8c) and All-Boiled Shake Wheel Turbine Water Turbine Combined Engine Combustion Unit (31X) for reducing friction loss and various rotations driven by hydroelectric storage battery Various energy storage cycle coalescence engine as output drive equipment.   Turbine blade cross-section (4C) capable of 910,000 times work rate and turbine blade (8c) and combined rotor combustion unit (31Y) for hydroelectric power generation with reduced friction loss by all blade impeller water turbine, various rotations driven by hydroelectric storage battery Various energy storage cycle coalescence engine as output drive equipment.   A turbine blade cross-section (4B) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32X) for hydroelectric power generation using a vertical all-blade water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   A turbine blade cross-section (4B) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation using a fully-rotated blade impeller water turbine. Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation with a fully moving impeller wheel turbine, and includes various types of heating equipment using heat. Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   A turbine blade cross section (4C) capable of 910,000 times power (4C) and a turbine blade (8c) and heating blade high temperature means (3B) coalescence engine combustion section (31X) for hydroelectric power generation with a water turbine and various types of use of heat Various energy storage cycle coalescing engines that are driven by hydroelectric storage batteries, including heating equipment, and various rotational output drive equipment.   Turbine blade cross section (4C) capable of 910,000 times power (4C) and turbine blade (8c) and all blade impeller water turbine with heating high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation Various energy storage cycle coalescing engines that are driven by hydroelectric storage batteries, including heating equipment, and various rotational output drive equipment.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32X) for hydroelectric power generation by heating high temperature means (3B) with a vertical all blade water turbine, Various energy storage cycle coalescing engines that are driven by hydroelectric storage batteries, including various types of heating equipment, and various rotational output drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32Y) for hydroelectric power generation with heating high temperature means (3B) with a vertical all blade water turbine, Various energy storage cycle coalescing engines that are driven by hydroelectric storage batteries, including various types of heating equipment, and various rotational output drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all blade combustion section (32X) that performs hydroelectric power generation using a vertical all blade water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a whole blade combustion section (32Y) for hydroelectric power generation using a vertical all-blade water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   It includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation with a fully-rotated blade impeller water turbine, and includes various types of heating equipment using heat. Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) that performs hydroelectric power generation with a fully-rotated blade impeller water turbine, and includes various types of heating equipment using heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation with reduced friction loss by a turbine blade (8c) and all-wheel impeller water turbine. Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade cross-section (4C) capable of 910,000 times power and a combined engine combustion section (31Y) that generates hydroelectric power with reduced friction loss by using a turbine blade (8c) and an all-wheel impeller water turbine. Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade cross-section (4B) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32X) for hydroelectric power generation using a vertical all-blade water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   A turbine blade cross-section (4B) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation using a fully-rotated blade impeller water turbine. Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation with a fully moving impeller wheel turbine, and includes various types of heating equipment using heat. Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   A turbine blade cross section (4C) capable of 910,000 times power (4C) and a turbine blade (8c) and heating blade high temperature means (3B) coalescence engine combustion section (31X) for hydroelectric power generation with a water turbine and various types of use of heat Various energy storage cycle coalescing engines that are driven by hydroelectric storage batteries, including heating equipment, and various rotational output drive equipment.   Turbine blade cross section (4C) capable of 910,000 times power (4C) and turbine blade (8c) and all blade impeller water turbine with heating high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation Various energy storage cycle coalescing engines that are driven by hydroelectric storage batteries, including heating equipment, and various rotational output drive equipment.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32X) for hydroelectric power generation by heating high temperature means (3B) with a vertical all blade water turbine, Various energy storage cycle coalescing engines that are driven by hydroelectric storage batteries, including various types of heating equipment, and various rotational output drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32Y) for hydroelectric power generation with heating high temperature means (3B) with a vertical all blade water turbine, Various energy storage cycle coalescing engines that are driven by hydroelectric storage batteries, including various types of heating equipment, and various rotational output drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all blade combustion section (32X) that performs hydroelectric power generation using a vertical all blade water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a whole blade combustion section (32Y) for hydroelectric power generation using a vertical all-blade water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   It includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation with a fully-rotated blade impeller water turbine, and includes various types of heating equipment using heat. Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) that performs hydroelectric power generation with a fully-rotated blade impeller water turbine, and includes various types of heating equipment using heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation with reduced friction loss by a turbine blade (8c) and all-wheel impeller water turbine. Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade cross-section (4C) capable of 910,000 times power and a combined engine combustion section (31Y) that generates hydroelectric power with reduced friction loss by using a turbine blade (8c) and an all-wheel impeller water turbine. Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   Turbine blade cross-section (4B) capable of 910,000-fold work efficiency, equipped with turbine blade (8c) and all blade combustion section (32X) for hydroelectric generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Turbine blade cross-section (4B) capable of 910,000-fold work efficiency, equipped with all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, and various cooking equipment using heat Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) for hydroelectric power generation with a fully-rotated blade impeller water turbine, including various cooking equipment and equipment using heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation using a fully-rotated blade impeller water turbine, including various cooking equipment and equipment using heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   A turbine blade cross section (4C) capable of 910,000 times power (4C) and a turbine blade (8c) and heating blade high temperature means (3B) coalescence engine combustion section (31X) for hydroelectric power generation with a water turbine and various types of use of heat Various energy storage cycle coalescing engines with various rotating output drive devices driven by hydroelectric storage batteries including cooking equipment.   Turbine blade cross section (4C) capable of 910,000 times power (4C) and turbine blade (8c) and all blade impeller water turbine with heating high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation Various energy storage cycle coalescing engines with various rotating output drive devices driven by hydroelectric storage batteries including cooking equipment.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32X) for hydroelectric power generation by heating high temperature means (3B) with a vertical all blade water turbine, Various energy storage cycle coalescing engines with various rotating output drive devices driven by hydroelectric storage batteries including various cooking equipment.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32Y) for hydroelectric power generation with heating high temperature means (3B) with a vertical all blade water turbine, Various energy storage cycle coalescing engines with various rotating output drive devices driven by hydroelectric storage batteries including various cooking equipment.   Turbine blade cross-section (4C) capable of 910,000-fold work rate, turbine blade (8c), and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Turbine blade cross-section (4C) capable of 910,000-fold work rate, turbine blade (8c), and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) for hydroelectric power generation using a fully-rotated blade impeller water turbine, and includes various cooking equipment and equipment using heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation using a fully-rotated blade impeller water turbine, including various cooking equipment and equipment using heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation with reduced friction loss with a turbine blade (8c) and a turbine blade turbine, and various cooking equipment using heat Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   Turbine blade cross-section (4C) capable of 910,000 times power and a combined engine combustion unit (31Y) that generates hydroelectric power with reduced friction loss using a turbine blade (8c) and all-blade propulsion wheel water turbines. Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   Turbine blade cross-section (4B) capable of 910,000-fold work efficiency, equipped with turbine blade (8c) and all blade combustion section (32X) for hydroelectric generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Turbine blade cross-section (4B) capable of 910,000-fold work efficiency, equipped with all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, and various cooking equipment using heat Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) for hydroelectric power generation with a fully-rotated blade impeller water turbine, including various cooking equipment and equipment using heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation using a fully-rotated blade impeller water turbine, including various cooking equipment and equipment using heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   A turbine blade cross section (4C) capable of 910,000 times power (4C) and a turbine blade (8c) and heating blade high temperature means (3B) coalescence engine combustion section (31X) for hydroelectric power generation with a water turbine and various types of use of heat Various energy storage cycle coalescing engines with various rotating output drive devices driven by hydroelectric storage batteries including cooking equipment.   Turbine blade cross section (4C) capable of 910,000 times power (4C) and turbine blade (8c) and all blade impeller water turbine with heating high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation Various energy storage cycle coalescing engines with various rotating output drive devices driven by hydroelectric storage batteries including cooking equipment.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32X) for hydroelectric power generation by heating high temperature means (3B) with a vertical all blade water turbine, Various energy storage cycle coalescing engines with various rotating output drive devices driven by hydroelectric storage batteries including various cooking equipment.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32Y) for hydroelectric power generation with heating high temperature means (3B) with a vertical all blade water turbine, Various energy storage cycle coalescing engines with various rotating output drive devices driven by hydroelectric storage batteries including various cooking equipment.   Turbine blade cross-section (4C) capable of 910,000-fold work rate, turbine blade (8c), and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Turbine blade cross-section (4C) capable of 910,000-fold work rate, turbine blade (8c), and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) for hydroelectric power generation using a fully-rotated blade impeller water turbine, and includes various cooking equipment and equipment using heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation using a fully-rotated blade impeller water turbine, including various cooking equipment and equipment using heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation with reduced friction loss with a turbine blade (8c) and a turbine blade turbine, and various cooking equipment using heat Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   Turbine blade cross-section (4C) capable of 910,000 times power and a combined engine combustion unit (31Y) that generates hydroelectric power with reduced friction loss using a turbine blade (8c) and all-blade propulsion wheel water turbines. Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   Turbine blade cross section (4B) capable of 910,000 times work rate and turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Turbine blade cross-section (4B) capable of 910,000 times work rate, equipped with turbine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Includes turbine blade cross section (4B) capable of 910,000 times work rate, turbine blade (8c) and coalescence engine combustion section (31X) for hydroelectric power generation using all blade impeller water turbines, and includes various hot water equipment using hot water Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes turbine blade cross section (4B) capable of 910,000 times work rate, turbine blade (8c) and coalescence engine combustion section (31Y) for hydroelectric power generation with all blade impeller water turbines, including various hot water facility equipment Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   A turbine blade cross section (4C) capable of 910,000 times power (4C) and a turbine blade (8c) and heating blade high temperature means (3B) coalescence engine combustion section (31X) for hydroelectric power generation with a water turbine and various types of use of heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries, including hot water equipment.   Turbine blade cross section (4C) capable of 910,000 times power (4C) and turbine blade (8c) and all blade impeller water turbine with heating high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries, including hot water equipment.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32X) for hydroelectric power generation by heating high temperature means (3B) with a vertical all blade water turbine, Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries, including various hot water equipment.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32Y) for hydroelectric power generation with heating high temperature means (3B) with a vertical all blade water turbine, Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries, including various hot water equipment.   Turbine blade cross-section (4C) capable of 910,000 times work rate, equipped with turbine blade (8c) and all blade combustion section (32X) for hydroelectric generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Turbine blade cross-section (4C) capable of 910,000-fold work rate, equipped with turbine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   It includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation using a fully-rotated blade impeller water turbine, and includes various types of hot water equipment that uses heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) that performs hydroelectric power generation with a fully-rotated blade impeller water turbine, and includes various types of hot water equipment that uses heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31X) that generates hydrodynamic power with reduced friction loss by using a turbine blade (8c) and a fully moving blade propeller water turbine. Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   Turbine blade cross-section (4C) capable of 910,000 times power and a combined engine combustion unit (31Y) for hydroelectric power generation with reduced friction loss by a turbine blade (8c) and a turbine blade spring turbine water turbine Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   Turbine blade cross section (4B) capable of 910,000 times work rate and turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Turbine blade cross-section (4B) capable of 910,000 times work rate, equipped with turbine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Includes turbine blade cross section (4B) capable of 910,000 times work rate, turbine blade (8c) and coalescence engine combustion section (31X) for hydroelectric power generation using all blade impeller water turbines, and includes various hot water equipment using hot water Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes turbine blade cross section (4B) capable of 910,000 times work rate, turbine blade (8c) and coalescence engine combustion section (31Y) for hydroelectric power generation with all blade impeller water turbines, including various hot water facility equipment Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   A turbine blade cross section (4C) capable of 910,000 times power (4C) and a turbine blade (8c) and heating blade high temperature means (3B) coalescence engine combustion section (31X) for hydroelectric power generation with a water turbine and various types of use of heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries, including hot water equipment.   Turbine blade cross section (4C) capable of 910,000 times power (4C) and turbine blade (8c) and all blade impeller water turbine with heating high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries, including hot water equipment.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32X) for hydroelectric power generation by heating high temperature means (3B) with a vertical all blade water turbine, Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries, including various hot water equipment.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32Y) for hydroelectric power generation with heating high temperature means (3B) with a vertical all blade water turbine, Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries, including various hot water equipment.   Turbine blade cross-section (4C) capable of 910,000 times work rate, equipped with turbine blade (8c) and all blade combustion section (32X) for hydroelectric generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Turbine blade cross-section (4C) capable of 910,000-fold work rate, equipped with turbine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   It includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation using a fully-rotated blade impeller water turbine, and includes various types of hot water equipment that uses heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) that performs hydroelectric power generation with a fully-rotated blade impeller water turbine, and includes various types of hot water equipment that uses heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31X) that generates hydrodynamic power with reduced friction loss by using a turbine blade (8c) and a fully moving blade propeller water turbine. Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   Turbine blade cross-section (4C) capable of 910,000 times power and a combined engine combustion unit (31Y) for hydroelectric power generation with reduced friction loss by a turbine blade (8c) and a turbine blade spring turbine water turbine Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   Turbine blade cross-section (4B) capable of 910,000 times work rate and turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   Turbine blade cross-section (4B) capable of 910,000 times work rate, equipped with turbine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation using vertical all blade water turbine, and various dishwashers using heat Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   Turbine blade cross-section (4B) capable of 910,000 times power and water including a combined engine combustion section (31X) for hydroelectric power generation using a turbine blade (8c) and all-wheel impeller water turbine, including various dishwashers using heat Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Turbine blade cross-section (4B) capable of 910,000 times power and water including a combined engine combustion section (31Y) for hydroelectric power generation with all blade impeller water turbines, including various dishwashers using heat Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   A turbine blade cross section (4C) capable of 910,000 times power (4C) and a turbine blade (8c) and heating blade high temperature means (3B) coalescence engine combustion section (31X) for hydroelectric power generation with a water turbine and various types of use of heat Various energy storage cycle coalescing engines that are driven by hydroelectric storage batteries, including dishwashers, and various rotational output drive devices.   Turbine blade cross section (4C) capable of 910,000 times power (4C) and turbine blade (8c) and all blade impeller water turbine with heating high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation Various energy storage cycle coalescing engines that are driven by hydroelectric storage batteries, including dishwashers, and various rotational output drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32X) for hydroelectric power generation by heating high temperature means (3B) with a vertical all blade water turbine, Various energy storage cycle coalescing engines that are driven by hydroelectric storage batteries, including various dishwashers, and various rotational output drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32Y) for hydroelectric power generation with heating high temperature means (3B) with a vertical all blade water turbine, Various energy storage cycle coalescing engines that are driven by hydroelectric storage batteries, including various dishwashers, and various rotational output drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power and turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   Turbine blade cross-section (4C) capable of 910,000 times work rate and turbine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   Turbine blade cross-section (4C) capable of 910,000 times power and water including a combined engine combustion section (31X) for hydroelectric power generation with a turbine blade (8c) and all-wheel impeller water turbine, including various dishwashers using heat Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Turbine blade cross-section (4C) capable of 910,000 times power and water including a combined engine combustion section (31Y) that performs hydroelectric power generation with a turbine blade (8c) and an all-wheel impeller water turbine, including various dishwashers using heat Various energy storage cycle coalescing engines for various rotating output drive devices driven by power storage batteries.   Turbine blade cross-section (4C) capable of 910,000 times power and a combined blade combustion engine (31X) that generates hydroelectric power with reduced friction loss by using a turbine blade (8c) and a turbine blade spring turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Turbine blade cross-section (4C) capable of 910,000 times power and all-blade dishwashers equipped with a combined engine combustion section (31Y) for hydroelectric power generation with reduced friction loss using a turbine blade (8c) and a turbine blade turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Turbine blade cross-section (4B) capable of 910,000 times work rate and turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   Turbine blade cross-section (4B) capable of 910,000 times work rate, equipped with turbine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation using vertical all blade water turbine, and various dishwashers using heat Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   Turbine blade cross-section (4B) capable of 910,000 times power and water including a combined engine combustion section (31X) for hydroelectric power generation using a turbine blade (8c) and all-wheel impeller water turbine, including various dishwashers using heat Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Turbine blade cross-section (4B) capable of 910,000 times power and water including a combined engine combustion section (31Y) for hydroelectric power generation with all blade impeller water turbines, including various dishwashers using heat Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   A turbine blade cross section (4C) capable of 910,000 times power (4C) and a turbine blade (8c) and heating blade high temperature means (3B) coalescence engine combustion section (31X) for hydroelectric power generation with a water turbine and various types of use of heat Various energy storage cycle coalescing engines that are driven by hydroelectric storage batteries, including dishwashers, and various rotational output drive devices.   Turbine blade cross section (4C) capable of 910,000 times power (4C) and turbine blade (8c) and all blade impeller water turbine with heating high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation Various energy storage cycle coalescing engines that are driven by hydroelectric storage batteries, including dishwashers, and various rotational output drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32X) for hydroelectric power generation by heating high temperature means (3B) with a vertical all blade water turbine, Various energy storage cycle coalescing engines that are driven by hydroelectric storage batteries, including various dishwashers, and various rotational output drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32Y) for hydroelectric power generation with heating high temperature means (3B) with a vertical all blade water turbine, Various energy storage cycle coalescing engines that are driven by hydroelectric storage batteries, including various dishwashers, and various rotational output drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power and turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   Turbine blade cross-section (4C) capable of 910,000 times work rate and turbine blades (8c) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   Turbine blade cross-section (4C) capable of 910,000 times power and water including a combined engine combustion section (31X) for hydroelectric power generation with a turbine blade (8c) and all-wheel impeller water turbine, including various dishwashers using heat Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Turbine blade cross-section (4C) capable of 910,000 times power and water including a combined engine combustion section (31Y) for hydroelectric power generation with a turbine blade (8c) and all-wheel impeller water turbine, including various dishwashers using heat Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Turbine blade cross-section (4C) capable of 910,000 times power and a combined blade combustion engine (31X) that generates hydroelectric power with reduced friction loss by using a turbine blade (8c) and a turbine blade spring turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Turbine blade cross-section (4C) capable of 910,000 times power and all-blade dishwashers equipped with a combined engine combustion section (31Y) for hydroelectric power generation with reduced friction loss by using a turbine blade (8c) and a turbine blade turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries including.   A turbine blade cross-section (4B) capable of 910,000 times power and a turbine blade (8c) and a whole blade combustion section (32X) for hydroelectric power generation using a vertical all-blade water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   A turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a whole blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation with a fully-rotating blade impeller water turbine, including various washing and drying machines using heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) that performs hydroelectric power generation with a water turbine impeller water turbine. Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   A turbine blade cross section (4C) capable of 910,000 times power (4C) and a turbine blade (8c) and heating blade high temperature means (3B) coalescence engine combustion section (31X) for hydroelectric power generation with a water turbine and various types of use of heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries, including washing and drying machines.   Turbine blade cross section (4C) capable of 910,000 times power (4C) and turbine blade (8c) and all blade impeller water turbine with heating high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries, including washing and drying machines.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32X) for hydroelectric power generation by heating high temperature means (3B) with a vertical all blade water turbine, Various energy storage cycle coalescing engines as hydroelectric storage battery driven various rotational output driving equipment including various washing dryers.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32Y) for hydroelectric power generation with heating high temperature means (3B) with a vertical all blade water turbine, Various energy storage cycle coalescing engines that are driven by hydroelectric storage batteries, including various washing and drying machines.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a full blade combustion section (32Y) that performs hydroelectric power generation using a vertical all blade water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) for hydroelectric power generation with a fully-rotor impeller water turbine, including various washing and drying machines using heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes a turbine blade cross section (4C) capable of 910,000 times work rate, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation with a water turbine with all blades, including various washing and drying machines using heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   A turbine blade cross section (4C) capable of 910,000 times work and a combined engine combustion section (31X) that generates hydrodynamic power generation with reduced friction loss by a turbine blade (8c) and a turbine blade turbine (8X) Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31Y) for hydroelectric power generation with reduced friction loss by a turbine blade (8c) and a fully moving blade impeller water turbine. Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade cross-section (4B) capable of 910,000 times power and a turbine blade (8c) and a whole blade combustion section (32X) for hydroelectric power generation using a vertical all-blade water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   A turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a whole blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation with a fully-rotating blade impeller water turbine, including various washing and drying machines using heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) that performs hydroelectric power generation with a water turbine impeller water turbine. Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   A turbine blade cross section (4C) capable of 910,000 times power (4C) and a turbine blade (8c) and heating blade high temperature means (3B) coalescence engine combustion section (31X) for hydroelectric power generation with a water turbine and various types of use of heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries, including washing and drying machines.   Turbine blade cross section (4C) capable of 910,000 times power (4C) and turbine blade (8c) and all blade impeller water turbine with heating high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries, including washing and drying machines.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32X) for hydroelectric power generation by heating high temperature means (3B) with a vertical all blade water turbine, Various energy storage cycle coalescing engines as hydroelectric storage battery driven various rotational output driving equipment including various washing dryers.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32Y) for hydroelectric power generation with heating high temperature means (3B) with a vertical all blade water turbine, Various energy storage cycle coalescing engines that are driven by hydroelectric storage batteries, including various washing and drying machines.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a full blade combustion section (32Y) that performs hydroelectric power generation using a vertical all blade water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) for hydroelectric power generation with a fully-rotor impeller water turbine, including various washing and drying machines using heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes a turbine blade cross section (4C) capable of 910,000 times work rate, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation with a water turbine with all blades, including various washing and drying machines using heat Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   A turbine blade cross section (4C) capable of 910,000 times work and a combined engine combustion section (31X) that generates hydrodynamic power generation with reduced friction loss by a turbine blade (8c) and a turbine blade turbine (8X) Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31Y) for hydroelectric power generation with reduced friction loss by a turbine blade (8c) and a fully moving blade impeller water turbine. Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and an all blade combustion section (32X) that performs hydroelectric power generation with a vertical all blade water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   A turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) that performs hydroelectric power generation with a vertical all blade water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   Turbine blade cross-section (4B) capable of 910,000 times power and water including various hot water piping buildings with a combined engine combustion section (31X) that performs hydroelectric power generation with a turbine blade (8c) and all-wheel impeller water turbine Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Turbine blade cross-section (4B) capable of 910,000 times power and water including coal-fired engine combustion section (31Y) for hydroelectric power generation with all blade impeller water turbine and water containing various hot water piping buildings Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heated turbine (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller water turbine, and various types of hot water Various energy storage cycle coalescing engines for various rotating output drive devices driven by hydroelectric storage batteries including piping buildings.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heated turbine (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine, and various types of hot water Various energy storage cycle coalescing engines for various rotating output drive devices driven by hydroelectric storage batteries including piping buildings.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries, including hot water piping buildings.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries, including hot water piping buildings.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all blade combustion section (32X) that performs hydroelectric power generation with a vertical all blade water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all blade combustion section (32Y) that performs hydroelectric power generation with a vertical all blade water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   Turbine blade cross-section (4C) capable of 910,000 times power and water including coal-fired engine combustion section (31X) for hydroelectric power generation with all blade impeller water turbine and water containing various hot water piping buildings Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Turbine blade cross-section (4C) capable of 910,000 times power and water including a combination engine combustion section (31Y) for hydroelectric power generation using a turbine blade (8c) and all-wheel impeller water turbine, including various hot water piping buildings Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Turbine blade cross-section (4C) capable of 910,000 times power and turbine blade (8c) and all-combustion blade bouncing water turbine combined coal combustion engine (31X) for reducing friction loss and various hot water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Turbine blade cross-section (4C) capable of 910,000 times power and turbine blades (8c) and all-combustion blade propeller water turbine combined coal combustion engine (31Y) for reducing friction loss and various hot water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   A turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and an all blade combustion section (32X) that performs hydroelectric power generation with a vertical all blade water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   A turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) that performs hydroelectric power generation with a vertical all blade water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   Turbine blade cross-section (4B) capable of 910,000 times power and water including various hot water piping buildings with a combined engine combustion section (31X) that performs hydroelectric power generation with a turbine blade (8c) and all-wheel impeller water turbine Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Turbine blade cross-section (4B) capable of 910,000 times power and water including coal-fired engine combustion section (31Y) for hydroelectric power generation with all blade impeller water turbine and water containing various hot water piping buildings Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heated turbine (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller water turbine, and various types of hot water Various energy storage cycle coalescing engines for various rotating output drive devices driven by hydroelectric storage batteries including piping buildings.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heated turbine (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine, and various types of hot water Various energy storage cycle coalescing engines for various rotating output drive devices driven by hydroelectric storage batteries including piping buildings.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries, including hot water piping buildings.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries, including hot water piping buildings.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all blade combustion section (32X) that performs hydroelectric power generation with a vertical all blade water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all blade combustion section (32Y) that performs hydroelectric power generation with a vertical all blade water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   Turbine blade cross-section (4C) capable of 910,000 times power and water including coal-fired engine combustion section (31X) for hydroelectric power generation with all blade impeller water turbine and water containing various hot water piping buildings Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Turbine blade cross-section (4C) capable of 910,000 times power and water including a combination engine combustion section (31Y) for hydroelectric power generation using a turbine blade (8c) and all-wheel impeller water turbine, including various hot water piping buildings Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Turbine blade cross-section (4C) capable of 910,000 times power and turbine blade (8c) and all-combustion blade bouncing water turbine combined coal combustion engine (31X) for reducing friction loss and various hot water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Turbine blade cross-section (4C) capable of 910,000 times power and turbine blades (8c) and all-combustion blade propeller water turbine combined coal combustion engine (31Y) for reducing friction loss and various hot water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   A turbine blade cross-section (4B) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32X) for hydroelectric power generation using a vertical all-blade water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   A turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and an all blade combustion section (32Y) that performs hydroelectric power generation with a vertical all blade water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation with a water turbine impeller water turbine, and includes various types of cooling equipment using cold energy. Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation using a fully-rotated blade impeller water turbine, and includes various types of cooling equipment using cold energy. Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heating blade high-speed turbine (3B) coalescence engine combustion section (31X) for hydroelectric power generation with a water turbine and various types of cold heat utilization Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices including cooling equipment.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heated turbine (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine, and various types of cold utilization Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices including cooling equipment.   A turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), a high temperature heating means (3B) with a vertical all blade water turbine, and a whole blade combustion section (32X) for hydroelectric power generation, Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries, including various types of cooling equipment.   A turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a high temperature heating means (3B) all blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries, including various types of cooling equipment.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a whole blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   It includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation with a fully-rotor impeller water turbine, and includes various types of cooling equipment using cold energy. Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   It includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation using a fully-rotated blade impeller water turbine, and includes various types of cooling equipment using cold energy. Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a combined engine combustion section (31X) that generates hydrodynamic power with reduced friction loss by using a turbine blade (8c) and a turbine blade spring turbine. Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade cross-section (4C) capable of 910,000 times power and a combined engine combustion section (31Y) that generates hydrodynamic power with reduced friction loss by using a turbine blade (8c) and a turbine blade spring turbine. Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade cross-section (4B) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32X) for hydroelectric power generation using a vertical all-blade water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   A turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and an all blade combustion section (32Y) that performs hydroelectric power generation with a vertical all blade water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation with a water turbine impeller water turbine, and includes various types of cooling equipment using cold energy. Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation using a fully-rotated blade impeller water turbine, and includes various types of cooling equipment using cold energy. Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heating blade high-speed turbine (3B) coalescence engine combustion section (31X) for hydroelectric power generation with a water turbine and various types of cold heat utilization Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices including cooling equipment.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heated turbine (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine, and various types of cold utilization Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices including cooling equipment.   A turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), a high temperature heating means (3B) with a vertical all blade water turbine, and a whole blade combustion section (32X) for hydroelectric power generation, Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries, including various types of cooling equipment.   A turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a high temperature heating means (3B) all blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries, including various types of cooling equipment.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a whole blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   It includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation with a fully-rotor impeller water turbine, and includes various types of cooling equipment using cold energy. Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   It includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation using a fully-rotated blade impeller water turbine, and includes various types of cooling equipment using cold energy. Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a combined engine combustion section (31X) that generates hydrodynamic power with reduced friction loss by using a turbine blade (8c) and a turbine blade spring turbine. Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade cross-section (4C) capable of 910,000 times power and a combined engine combustion section (31Y) that generates hydrodynamic power with reduced friction loss by using a turbine blade (8c) and a turbine blade spring turbine. Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   Turbine blade cross section (4B) capable of 910,000 times power and water including various generators with a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation using a vertical all blade water turbine Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Turbine blade cross-section (4B) capable of 910,000 times power and water including various generators with a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation using a vertical all blade water turbine Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Turbine blade cross section (4B) capable of 910,000 times power and hydroelectric storage battery including combined generator combustion section (31X) for hydroelectric power generation using all blade impeller water turbine with turbine blade (8c) and various generators Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross-section (4B) capable of 910,000 times power and hydroelectric storage battery including combined generator combustion section (31Y) for hydroelectric power generation with all blade impeller water turbine, and various generators Various energy storage cycle coalescing engines as various rotational output drive devices.   Various generators including a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c) and a combined high temperature heating means (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller water turbine Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   Various generators including a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c) and a combined high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries including generators.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries including generators.   Turbine blade cross section (4C) capable of 910,000 times power and water including various generators with a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Turbine blade cross-section (4C) capable of 910,000 times power and water including various generators with a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation using a vertical all blade water turbine Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Turbine blade cross section (4C) capable of 910,000 times power and hydroelectric storage battery including combined generator combustion section (31X) for hydroelectric power generation with all blade impeller water turbines and various generators Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross section (4C) capable of 910,000 times power and hydroelectric storage battery including combined generator combustion part (31Y) for hydroelectric power generation with all blade impeller water turbine and turbine generator (31Y) Various energy storage cycle coalescing engines as various rotational output drive devices.   Includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that reduces friction loss with all-wheel impeller water turbines and includes various generators Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31Y) for reducing friction loss with a fully-rotating blade impeller water turbine and including various generators Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Turbine blade cross section (4B) capable of 910,000 times power and water including various generators with a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation using a vertical all blade water turbine Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Turbine blade cross-section (4B) capable of 910,000 times power and water including various generators with a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation using a vertical all blade water turbine Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Turbine blade cross section (4B) capable of 910,000 times power and hydroelectric storage battery including combined generator combustion section (31X) for hydroelectric power generation using all blade impeller water turbine with turbine blade (8c) and various generators Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross-section (4B) capable of 910,000 times power and hydroelectric storage battery including combined generator combustion section (31Y) for hydroelectric power generation with all blade impeller water turbine, and various generators Various energy storage cycle coalescing engines as various rotational output drive devices.   Various generators including a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c) and a combined high temperature heating means (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller water turbine Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   Various generators including a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c) and a combined high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries including generators.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries including generators.   Turbine blade cross section (4C) capable of 910,000 times power and water including various generators with a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Turbine blade cross-section (4C) capable of 910,000 times power and water including various generators with a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation using a vertical all blade water turbine Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Turbine blade cross section (4C) capable of 910,000 times power and hydroelectric storage battery including combined generator combustion section (31X) for hydroelectric power generation with all blade impeller water turbines and various generators Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross section (4C) capable of 910,000 times power and hydroelectric storage battery including combined generator combustion part (31Y) for hydroelectric power generation with all blade impeller water turbine and turbine generator (31Y) Various energy storage cycle coalescing engines as various rotational output drive devices.   Includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that reduces friction loss with all-wheel impeller water turbines and includes various generators Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31Y) for reducing friction loss with a fully-rotating blade impeller water turbine and including various generators Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Hydroelectric power generation including various electric motors with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation using a vertical all blade water turbine Various energy storage cycle coalescing engine as storage battery driven various rotational output drive equipment.   Hydropower generation including a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) that performs hydroelectric power generation using a vertical all blade water turbine and various motors Various energy storage cycle coalescing engine as storage battery driven various rotational output drive equipment.   Turbine blade cross-section (4B) capable of 910,000 times power and hydroelectric accumulator drive including various motors with a combined engine combustion section (31X) that performs hydroelectric power generation with a turbine blade (8c) and a full blade impeller water turbine Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross-section (4B) capable of 910,000 times work rate, hydroelectric storage battery drive including various motors with a combined engine combustion section (31Y) that performs hydroelectric power generation with a turbine blade (8c) and all-wheel impeller water turbine Various energy storage cycle coalescing engines as various rotational output drive devices.   Various motors with a turbine blade cross section (4C) capable of 910,000 times power (4C), a turbine blade (8c), and a combined high temperature heating means (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Various motors with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), a combined high temperature heating means (3B) and a combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines that are driven by hydroelectric storage batteries, including electric motors, and various rotational output drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines that are driven by hydroelectric storage batteries, including electric motors, and various rotational output drive devices.   Hydroelectric power generation including various motors with turbine blade cross section (4C) turbine blade (8c) capable of 910,000 times power and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engine as storage battery driven various rotational output drive equipment.   Hydropower generation including a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine and various motors Various energy storage cycle coalescing engine as storage battery driven various rotational output drive equipment.   Turbine blade cross section (4C) capable of 910,000 times work rate and hydroelectric storage battery drive including various motors equipped with a combined engine combustion section (31X) that performs hydroelectric power generation with all blade impeller water turbine Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross-section (4C) capable of 910,000 times work rate and hydroelectric storage battery drive including various motors equipped with combined engine combustion section (31Y) for hydroelectric power generation with all blade impeller water turbine Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power and water including various motors with a combined engine combustion section (31X) for reducing friction loss with a turbine blade (8c) and an all-wheel impeller water turbine. Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Turbine blade cross section (4C) capable of 910,000 times power and water including various electric motors equipped with a combined engine combustion section (31Y) for reducing friction loss hydroelectric power generation with a turbine blade (8c) and an all blade impeller water turbine Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Hydroelectric power generation including various electric motors with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation using a vertical all blade water turbine Various energy storage cycle coalescing engine as storage battery driven various rotational output drive equipment.   Hydropower generation including a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) that performs hydroelectric power generation using a vertical all blade water turbine and various motors Various energy storage cycle coalescing engine as storage battery driven various rotational output drive equipment.   Turbine blade cross-section (4B) capable of 910,000 times power and hydroelectric accumulator drive including various motors with a combined engine combustion section (31X) that performs hydroelectric power generation with a turbine blade (8c) and a full blade impeller water turbine Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross-section (4B) capable of 910,000 times work rate, hydroelectric storage battery drive including various motors with a combined engine combustion section (31Y) that performs hydroelectric power generation with a turbine blade (8c) and all-wheel impeller water turbine Various energy storage cycle coalescing engines as various rotational output drive devices.   Various motors with a turbine blade cross section (4C) capable of 910,000 times power (4C), a turbine blade (8c), and a combined high temperature heating means (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Various motors with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), a combined high temperature heating means (3B) and a combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines that are driven by hydroelectric storage batteries, including electric motors, and various rotational output drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines that are driven by hydroelectric storage batteries, including electric motors, and various rotational output drive devices.   Hydroelectric power generation including various motors with turbine blade cross section (4C) turbine blade (8c) capable of 910,000 times power and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engine as storage battery driven various rotational output drive equipment.   Hydropower generation including a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine and various motors Various energy storage cycle coalescing engine as storage battery driven various rotational output drive equipment.   Turbine blade cross section (4C) capable of 910,000 times work rate and hydroelectric storage battery drive including various motors equipped with a combined engine combustion section (31X) that performs hydroelectric power generation with all blade impeller water turbine Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross-section (4C) capable of 910,000 times work rate and hydroelectric storage battery drive including various motors equipped with combined engine combustion section (31Y) for hydroelectric power generation with all blade impeller water turbine Various energy storage cycle coalescing engines as various rotational output drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power and water including various motors with a combined engine combustion section (31X) for reducing friction loss with a turbine blade (8c) and an all-wheel impeller water turbine. Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Turbine blade cross section (4C) capable of 910,000 times power and water including various electric motors equipped with a combined engine combustion section (31Y) for reducing friction loss hydroelectric power generation with a turbine blade (8c) and an all blade impeller water turbine Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   A turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and an all blade combustion section (32X) that performs hydroelectric power generation with a vertical all blade water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   A turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and an all blade combustion section (32Y) for hydroelectric power generation using a vertical all blade water turbine, and various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   Turbine blade cross-section (4B) capable of 910,000 times power and water including various hot water piping greenhouses equipped with a combined engine combustion section (31X) for hydroelectric power generation with a turbine blade (8c) and a full blade impeller water turbine Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Turbine blade cross section (4B) capable of 910,000 times power and water including various hot water piping greenhouses equipped with a combined engine combustion section (31Y) for hydroelectric power generation with a turbine blade (8c) and a full blade impeller water turbine Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heated turbine (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller water turbine, and various types of hot water Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries, including piping greenhouses.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heated turbine (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine, and various types of hot water Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries, including piping greenhouses.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines for various rotating output drive devices driven by hydroelectric storage batteries including hot water piping greenhouses.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines for various rotating output drive devices driven by hydroelectric storage batteries including hot water piping greenhouses.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine, and various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all blade combustion section (32Y) for hydroelectric power generation using a vertical all blade water turbine, and various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   Turbine blade cross-section (4C) capable of 910,000 times power and water including various hot water piping greenhouses equipped with a combined engine combustion section (31X) that performs hydroelectric power generation with a turbine blade (8c) and a full blade impeller water turbine Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Turbine blade cross-section (4C) capable of 910,000 times power and water including various hot water piping greenhouses with a combined engine combustion section (31Y) for hydroelectric power generation with a turbine blade (8c) and a full blade impeller water turbine Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Turbine blade cross-section (4C) capable of 910,000 times power and turbine blade (8c) and a combined engine combustion section (31X) for reducing friction loss hydroelectric power generation with all blade impeller water turbines and various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Turbine blade cross-section (4C) capable of 910,000 times power and turbine blade (8c) and all-combustion blade spring vehicle water turbine with coalescence engine combustion section (31Y) for reducing friction loss and various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   A turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and an all blade combustion section (32X) that performs hydroelectric power generation with a vertical all blade water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   A turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and an all blade combustion section (32Y) for hydroelectric power generation using a vertical all blade water turbine, and various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   Turbine blade cross-section (4B) capable of 910,000 times power and water including various hot water piping greenhouses equipped with a combined engine combustion section (31X) for hydroelectric power generation with a turbine blade (8c) and a full blade impeller water turbine Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Turbine blade cross section (4B) capable of 910,000 times power and water including various hot water piping greenhouses equipped with a combined engine combustion section (31Y) for hydroelectric power generation with a turbine blade (8c) and a full blade impeller water turbine Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heated turbine (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller water turbine, and various types of hot water Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries, including piping greenhouses.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heated turbine (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine, and various types of hot water Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries, including piping greenhouses.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines for various rotating output drive devices driven by hydroelectric storage batteries including hot water piping greenhouses.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines for various rotating output drive devices driven by hydroelectric storage batteries including hot water piping greenhouses.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine, and various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all blade combustion section (32Y) for hydroelectric power generation using a vertical all blade water turbine, and various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   Turbine blade cross-section (4C) capable of 910,000 times power and water including various hot water piping greenhouses equipped with a combined engine combustion section (31X) that performs hydroelectric power generation with a turbine blade (8c) and a full blade impeller water turbine Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Turbine blade cross-section (4C) capable of 910,000 times power and water including various hot water piping greenhouses with a combined engine combustion section (31Y) for hydroelectric power generation with a turbine blade (8c) and a full blade impeller water turbine Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Turbine blade cross-section (4C) capable of 910,000 times power and turbine blade (8c) and a combined engine combustion section (31X) for reducing friction loss hydroelectric power generation with all blade impeller water turbines and various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Turbine blade cross-section (4C) capable of 910,000 times power and turbine blade (8c) and all-combustion blade propeller water turbine combined coal combustion unit (31Y) for reducing friction loss hydroelectric power generation and various hot water piping greenhouses Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Turbine blade cross-section (4B) capable of 910,000 times work rate and turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Turbine blade cross-section (4B) capable of 910,000-fold work efficiency, equipped with turbine blade (8c) and all blade combustion section (32Y) for hydroelectric generation with vertical all blade water turbine, and various hot water storage equipment Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation with a fully moving impeller wheel turbine, and includes various hot water storage equipment. Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31Y) for hydroelectric power generation with a full bucket impeller water turbine, including various hot water storage equipment Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heated turbine (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller water turbine, and various types of hot water Various energy storage cycle coalescing engines that are driven by hydroelectric storage batteries, including storage equipment, and various rotational output drive equipment.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heated turbine (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine, and various types of hot water Various energy storage cycle coalescing engines that are driven by hydroelectric storage batteries, including storage equipment, and various rotational output drive equipment.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Various energy conservation cycle coalescing engines that are driven by hydroelectric storage batteries, including hot water storage equipment, and various rotational output drive equipment.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Various energy conservation cycle coalescing engines that are driven by hydroelectric storage batteries, including hot water storage equipment, and various rotational output drive equipment.   Turbine blade cross-section (4C) capable of 910,000 times power and turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Turbine blade cross-section (4C) capable of 910,000 times work rate, turbine blade (8c), and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, various hot water storage equipment Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   It includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation with a fully moving impeller wheel turbine, and includes various types of hot water storage equipment. Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   It includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) that performs hydroelectric power generation with a full blade impeller water turbine, including various hot water storage equipment. Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31X) for reducing friction loss with all blade impeller water turbines and various hot water storage equipment Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   Turbine blade cross section (4C) capable of 910,000 times work rate and various hot water storage equipment equipped with a combined engine combustion section (31Y) that generates hydrodynamic power with reduced friction loss by using a turbine blade (8c) and a turbine blade turbine. Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   Turbine blade cross-section (4B) capable of 910,000 times work rate and turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Turbine blade cross-section (4B) capable of 910,000-fold work efficiency, equipped with turbine blade (8c) and all blade combustion section (32Y) for hydroelectric generation with vertical all blade water turbine, and various hot water storage equipment Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation with a fully moving impeller wheel turbine, and includes various hot water storage equipment. Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31Y) for hydroelectric power generation with a full bucket impeller water turbine, including various hot water storage equipment Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heated turbine (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller water turbine, and various types of hot water Various energy storage cycle coalescing engines that are driven by hydroelectric storage batteries, including storage equipment, and various rotational output drive equipment.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heated turbine (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine, and various types of hot water Various energy storage cycle coalescing engines that are driven by hydroelectric storage batteries, including storage equipment, and various rotational output drive equipment.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Various energy conservation cycle coalescing engines that are driven by hydroelectric storage batteries, including hot water storage equipment, and various rotational output drive equipment.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Various energy conservation cycle coalescing engines that are driven by hydroelectric storage batteries, including hot water storage equipment, and various rotational output drive equipment.   Turbine blade cross-section (4C) capable of 910,000 times power and turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Turbine blade cross-section (4C) capable of 910,000 times work rate, turbine blade (8c), and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, various hot water storage equipment Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   It includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation with a fully moving impeller wheel turbine, and includes various types of hot water storage equipment. Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   It includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) that performs hydroelectric power generation with a full blade impeller water turbine, including various hot water storage equipment. Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31X) for reducing friction loss with all blade impeller water turbines and various hot water storage equipment Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   Turbine blade cross section (4C) capable of 910,000 times work rate and various hot water storage equipment equipped with a combined engine combustion section (31Y) that generates hydrodynamic power with reduced friction loss by using a turbine blade (8c) and a turbine blade turbine. Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   Turbine blade cross-section (4B) capable of 910,000 times work rate and turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Turbine blade cross-section (4B) capable of 910,000 times work rate, equipped with turbine blade (8c) and all blade combustion section (32Y) for hydroelectric generation with vertical all blade water turbine, and various hot water piping equipment Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation with a fully-rotor impeller water turbine, including various hot water piping equipment Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) that performs hydroelectric power generation with a fully moving impeller wheel turbine, including various hot water piping equipment Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heated turbine (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller water turbine, and various types of hot water Various energy storage cycle coalescing engines that are driven by hydroelectric storage batteries, including piping equipment, and various rotational output drive equipment.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heated turbine (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine, and various types of hot water Various energy storage cycle coalescing engines that are driven by hydroelectric storage batteries, including piping equipment, and various rotational output drive equipment.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines for various rotary output drive devices driven by hydroelectric storage batteries including hot water piping equipment.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines for various rotary output drive devices driven by hydroelectric storage batteries including hot water piping equipment.   Turbine blade cross-section (4C) capable of 910,000 times power and turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation using vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Turbine blade cross-section (4C) capable of 910,000 times power, and turbine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) for hydroelectric power generation with a fully-rotated blade impeller water turbine, including various hot water piping equipment Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation with a fully moving impeller wheel turbine, including various hot water piping equipment Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31X) for hydroelectric power generation with reduced friction loss by a fully-rotated blade impeller water turbine, and various hot water piping equipment Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   Turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31Y) that generates hydrodynamic power with reduced friction loss with a fully moving blade spring turbine water turbine. Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   Turbine blade cross-section (4B) capable of 910,000 times work rate and turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Turbine blade cross-section (4B) capable of 910,000 times work rate, equipped with turbine blade (8c) and all blade combustion section (32Y) for hydroelectric generation with vertical all blade water turbine, and various hot water piping equipment Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation with a fully-rotor impeller water turbine, including various hot water piping equipment Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) that performs hydroelectric power generation with a fully moving impeller wheel turbine, including various hot water piping equipment Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heated turbine (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller water turbine, and various types of hot water Various energy storage cycle coalescing engines that are driven by hydroelectric storage batteries, including piping equipment, and various rotational output drive equipment.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heated turbine (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine, and various types of hot water Various energy storage cycle coalescing engines that are driven by hydroelectric storage batteries, including piping equipment, and various rotational output drive equipment.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines for various rotary output drive devices driven by hydroelectric storage batteries including hot water piping equipment.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines for various rotary output drive devices driven by hydroelectric storage batteries including hot water piping equipment.   Turbine blade cross-section (4C) capable of 910,000 times power and turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation using vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Turbine blade cross-section (4C) capable of 910,000 times power, and turbine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) for hydroelectric power generation with a fully-rotated blade impeller water turbine, including various hot water piping equipment Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation with a fully moving impeller wheel turbine, including various hot water piping equipment Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31X) for hydroelectric power generation with reduced friction loss by a fully-rotated blade impeller water turbine, and various hot water piping equipment Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   Turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31Y) that generates hydrodynamic power with reduced friction loss with a fully moving blade spring turbine water turbine. Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   A turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and an all blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine, and various cold water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   A turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and an all blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, and various cold water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   Turbine blade cross-section (4B) capable of 910,000 times power and water including coal-cooled engine combustion section (31X) for hydroelectric power generation with all blade impeller water turbine and water including various cold water piping buildings Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Turbine blade cross-section (4B) capable of 910,000 times power and water including coal-cooled engine combustion part (31Y) for hydroelectric power generation with all blade impeller water turbine and water containing various cold water piping buildings Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   A turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) with a combined turbine combustion section (31X) for hydroelectric power generation with all blade impeller water turbines. Various energy storage cycle coalescing engines for various rotating output drive devices driven by hydroelectric storage batteries including piping buildings.   A turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature heating means (3B) combined coal combustion section (31Y) for hydroelectric power generation with all blade impeller water turbines, and various cold and hot water Various energy storage cycle coalescing engines for various rotating output drive devices driven by hydroelectric storage batteries including piping buildings.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines as hydroelectric storage battery driven various rotating output driving equipment including cold water piping buildings.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines as hydroelectric storage battery driven various rotating output driving equipment including cold water piping buildings.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all blade combustion section (32Y) that performs hydroelectric power generation with a vertical all blade water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   Turbine blade cross-section (4C) capable of 910,000 times power and water including coal-cooled engine combustion part (31X) for hydroelectric power generation with all blade impeller water turbines and various cold water piping buildings Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Turbine blade cross section (4C) capable of 910,000 times power and water including coal-cooled engine combustion section (31Y) for hydroelectric generation with all blade impeller water turbine with water turbine including various cold water piping buildings Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Turbine blade cross-section (4C) capable of 910,000 times power and turbine blades (8c) and a combined engine combustion section (31X) for hydroelectric power generation with reduced friction loss by all-wheel impeller water turbines and various cold water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Turbine blade cross-section (4C) capable of 910,000-fold work efficiency, combined with a combined engine combustion section (31Y) for reducing friction loss hydroelectric power generation with a turbine blade (8c) and all-blade propulsion wheel water turbine, and various chilled water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   A turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and an all blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine, and various cold water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   A turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and an all blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, and various cold water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   Turbine blade cross-section (4B) capable of 910,000 times power and water including coal-cooled engine combustion section (31X) for hydroelectric power generation with all blade impeller water turbine and water including various cold water piping buildings Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Turbine blade cross-section (4B) capable of 910,000 times power and water including coal-cooled engine combustion part (31Y) for hydroelectric power generation with all blade impeller water turbine and water containing various cold water piping buildings Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   A turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) with a combined turbine combustion section (31X) for hydroelectric power generation with all blade impeller water turbines. Various energy storage cycle coalescing engines for various rotating output drive devices driven by hydroelectric storage batteries including piping buildings.   A turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature heating means (3B) combined coal combustion section (31Y) for hydroelectric power generation with all blade impeller water turbines, and various cold and hot water Various energy storage cycle coalescing engines for various rotating output drive devices driven by hydroelectric storage batteries including piping buildings.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines as hydroelectric storage battery driven various rotating output driving equipment including cold water piping buildings.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines as hydroelectric storage battery driven various rotating output driving equipment including cold water piping buildings.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all blade combustion section (32Y) that performs hydroelectric power generation with a vertical all blade water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   Turbine blade cross-section (4C) capable of 910,000 times power and water including coal-cooled engine combustion part (31X) for hydroelectric power generation with all blade impeller water turbines and various cold water piping buildings Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Turbine blade cross section (4C) capable of 910,000 times power and water including coal-cooled engine combustion section (31Y) for hydroelectric generation with all blade impeller water turbine with water turbine including various cold water piping buildings Various energy storage cycle coalescing engines for various types of rotating output drive devices driven by power storage batteries.   Turbine blade cross-section (4C) capable of 910,000 times power and turbine blades (8c) and a combined engine combustion section (31X) for hydroelectric power generation with reduced friction loss by all-wheel impeller water turbines and various cold water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Turbine blade cross-section (4C) capable of 910,000-fold work efficiency, combined with a combined engine combustion section (31Y) for reducing friction loss hydroelectric power generation with a turbine blade (8c) and all-blade propulsion wheel water turbine, and various chilled water piping buildings Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Various refrigeration equipment using cold heat with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation using a vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Various refrigeration equipment using cold heat with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation using a fully-rotated blade impeller water turbine, and includes various refrigeration equipment using cold energy Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) that performs hydroelectric power generation using a fully-rotor impeller water turbine, and includes various refrigeration equipment utilizing cold energy. Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heating blade high-speed turbine (3B) coalescence engine combustion section (31X) for hydroelectric power generation with a water turbine and various types of cold heat utilization Various energy storage cycle coalescing engines that are driven by hydroelectric storage batteries, including refrigeration equipment.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heated turbine (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine, and various types of cold utilization Various energy storage cycle coalescing engines that are driven by hydroelectric storage batteries, including refrigeration equipment.   A turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), a high temperature heating means (3B) with a vertical all blade water turbine, and a whole blade combustion section (32X) for hydroelectric power generation, Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries including various types of refrigeration equipment.   A turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a high temperature heating means (3B) all blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries including various types of refrigeration equipment.   Various refrigeration equipment using cold heat with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation using a vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Various refrigeration equipment using cold energy with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   It includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation with a fully-rotated blade impeller water turbine, and includes various refrigeration equipment using cold energy Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   It includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation with a fully-rotor impeller water turbine, including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Various refrigeration equipment using cold energy with a turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation with reduced friction loss with a turbine blade (8c) and a turbine blade turbine Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   Various refrigeration equipment using cold heat with a turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31Y) for hydroelectric power generation with reduced friction loss with a turbine blade (8c) and a turbine blade turbine Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   Various refrigeration equipment using cold heat with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation using a vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Various refrigeration equipment using cold heat with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation using a fully-rotated blade impeller water turbine, and includes various refrigeration equipment using cold energy Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) that performs hydroelectric power generation using a fully-rotor impeller water turbine, and includes various refrigeration equipment utilizing cold energy. Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heating blade high-speed turbine (3B) coalescence engine combustion section (31X) for hydroelectric power generation with a water turbine and various types of cold heat utilization Various energy storage cycle coalescing engines that are driven by hydroelectric storage batteries, including refrigeration equipment.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heated turbine (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine, and various types of cold utilization Various energy storage cycle coalescing engines that are driven by hydroelectric storage batteries, including refrigeration equipment.   A turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), a high temperature heating means (3B) with a vertical all blade water turbine, and a whole blade combustion section (32X) for hydroelectric power generation, Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries including various types of refrigeration equipment.   A turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a high temperature heating means (3B) all blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries including various types of refrigeration equipment.   Various refrigeration equipment using cold heat with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation using a vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   Various refrigeration equipment using cold energy with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric power storage batteries.   It includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation with a fully-rotated blade impeller water turbine, and includes various refrigeration equipment using cold energy Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   It includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation with a fully-rotor impeller water turbine, including various refrigeration equipment using cold energy Various energy storage cycle coalescing engines that are driven by hydroelectric power storage batteries and various rotational output drive devices.   Various refrigeration equipment using cold energy with a turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation with reduced friction loss with a turbine blade (8c) and a turbine blade turbine Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   Various refrigeration equipment using cold heat with a turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31Y) for hydroelectric power generation with reduced friction loss with a turbine blade (8c) and a turbine blade turbine Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including   Water including various generators with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine Various energy storage cycle coalescing engines as jet (79M) various water suction jet drive devices.   Turbine blade cross section (4B) capable of 910,000 times power and water including various generators with a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation using a vertical all blade water turbine Various energy storage cycle coalescing engines as jet (79M) various water suction jet drive devices.   Water jet including various generators, including a turbine blade cross section (4B) capable of 910,000 times work rate (4B), a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation with a water turbine impeller 79M) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Water jet including various generators with a turbine blade cross section (4B) capable of 910,000 times power and a combined engine combustion section (31Y) for hydroelectric power generation with a turbine blade (8c) and an all-wheel impeller water turbine 79M) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Various generators including a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c) and a combined high temperature heating means (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller water turbine Water-jet (79M) including various types of various energy storage cycle coalescing engines as various water suction / injection drive devices.   Various generators including a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c) and a combined high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine Water-jet (79M) including various types of various energy storage cycle coalescing engines as various water suction / injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines as water jet (79M) various water suction / injection drive devices including generators.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines as water jet (79M) various water suction / injection drive devices including generators.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation using a vertical all-blade water turbine and water including various generators Various energy storage cycle coalescing engines as jet (79M) various water suction jet drive devices.   Water including various generators with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine Various energy storage cycle coalescing engines as jet (79M) various water suction jet drive devices.   Water jet including various generators with a combined turbine combustion section (31X) for hydroelectric generation with a turbine blade cross section (4C) turbine blade (8c) capable of 910,000 times work rate and a full blade impeller water turbine 79M) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   A turbine jet section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined jet combustion section (31Y) that performs hydroelectric power generation with a fully-rotor impeller water turbine, a water jet including various generators ( 79M) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that reduces friction loss with all-wheel impeller water turbines and includes various generators Water Jet (79M) Various energy storage cycle coalescing engines as various water suction jet drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31Y) for reducing friction loss with a fully-rotating blade impeller water turbine and including various generators Water Jet (79M) Various energy storage cycle coalescing engines as various water suction jet drive devices.   Water including various generators with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine Various energy storage cycle coalescing engines as jet (79M) various water suction jet drive devices.   Turbine blade cross section (4B) capable of 910,000 times power and water including various generators with a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation using a vertical all blade water turbine Various energy storage cycle coalescing engines as jet (79M) various water suction jet drive devices.   Water jet including various generators, including a turbine blade cross section (4B) capable of 910,000 times work rate (4B), a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation with a water turbine impeller 79M) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Water jet including various generators with a turbine blade cross section (4B) capable of 910,000 times power and a combined engine combustion section (31Y) for hydroelectric power generation with a turbine blade (8c) and an all-wheel impeller water turbine 79M) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Various generators including a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c) and a combined high temperature heating means (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller water turbine Water-jet (79M) including various types of various energy storage cycle coalescing engines as various water suction / injection drive devices.   Various generators including a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c) and a combined high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine Water-jet (79M) including various types of various energy storage cycle coalescing engines as various water suction / injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines as water jet (79M) various water suction / injection drive devices including generators.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines as water jet (79M) various water suction / injection drive devices including generators.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation using a vertical all-blade water turbine and water including various generators Various energy storage cycle coalescing engines as jet (79M) various water suction jet drive devices.   Water including various generators with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine Various energy storage cycle coalescing engines as jet (79M) various water suction jet drive devices.   Water jet including various generators with a combined turbine combustion section (31X) for hydroelectric generation with a turbine blade cross section (4C) turbine blade (8c) capable of 910,000 times work rate and a full blade impeller water turbine 79M) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   A turbine jet section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined jet combustion section (31Y) that performs hydroelectric power generation with a fully-rotor impeller water turbine, a water jet including various generators ( 79M) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that reduces friction loss with all-wheel impeller water turbines and includes various generators Water Jet (79M) Various energy storage cycle coalescing engines as various water suction jet drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31Y) for reducing friction loss with a fully-rotating blade impeller water turbine and including various generators Water Jet (79M) Various energy storage cycle coalescing engines as various water suction jet drive devices.   Water jet including various electric motors with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine (79M) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Water jet including various electric motors with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine (79M) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Water jet (79M) including various motors with a turbine blade cross section (4B) capable of 910,000 times power and a combined engine combustion part (31X) for hydroelectric power generation with a turbine blade (8c) and a turbine blade turbine ) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Water jet (79M) including various electric motors, including a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation using a fully-rotor impeller water turbine ) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Various motors with a turbine blade cross section (4C) capable of 910,000 times power (4C), a turbine blade (8c), and a combined high temperature heating means (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller Water-jet (79M) including various energy storage cycle coalescing engines as various water suction / injection drive devices.   Various motors with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), a combined high temperature heating means (3B) and a combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller Water-jet (79M) including various energy storage cycle coalescing engines as various water suction / injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines as water jet (79M) various water suction jet drive devices including electric motors.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines as water jet (79M) various water suction jet drive devices including electric motors.   Water jet including various motors with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation using a vertical all blade water turbine (79M) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Water jet including various electric motors having a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation using a vertical all blade water turbine (79M) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Water jet (79M) including various electric motors, including a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) for hydroelectric power generation with a water turbine and a turbine moving turbine. ) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Water jet (79M) including various electric motors, including a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation with a fully moving blade impeller water turbine ) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Turbine blade cross section (4C) capable of 910,000 times power and water including various motors equipped with a combined engine combustion section (31X) for reducing friction loss hydroelectric power generation with a turbine blade (8c) and a turbine blade impeller water turbine Various energy storage cycle coalescing engines as jet (79M) various water suction jet drive devices.   Turbine blade cross section (4C) capable of 910,000 times power and water including various electric motors equipped with a combined engine combustion section (31Y) for reducing friction loss water power generation with a turbine blade (8c) and a full blade impeller water turbine Various energy storage cycle coalescing engines as jet (79M) various water suction jet drive devices.   Water jet including various electric motors with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine (79M) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Water jet including various electric motors with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine (79M) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Water jet (79M) including various electric motors, including a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation with a water turbine impeller ) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Water jet (79M) including various electric motors, including a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation using a fully-rotor impeller water turbine ) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Various motors with a turbine blade cross section (4C) capable of 910,000 times power (4C), a turbine blade (8c), and a combined high temperature heating means (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller Water-jet (79M) including various energy storage cycle coalescing engines as various water suction / injection drive devices.   Various motors with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), a combined high temperature heating means (3B) and a combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller Water-jet (79M) including various energy storage cycle coalescing engines as various water suction / injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines as water jet (79M) various water suction jet drive devices including electric motors.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines as water jet (79M) various water suction jet drive devices including electric motors.   Water jet including various motors with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation using a vertical all blade water turbine (79M) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Water jet including various electric motors having a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation using a vertical all blade water turbine (79M) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Water jet (79M) including various electric motors, including a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) for hydroelectric power generation with a water turbine and a turbine moving turbine. ) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Water jet (79M) including various electric motors, including a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) that performs hydroelectric power generation with a water turbine impeller ) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Turbine blade cross section (4C) capable of 910,000 times power and water including various motors equipped with a combined engine combustion section (31X) for reducing friction loss hydroelectric power generation with a turbine blade (8c) and a turbine blade impeller water turbine Various energy storage cycle coalescing engines as jet (79M) various water suction jet drive devices.   Turbine blade cross section (4C) capable of 910,000 times power and water including various electric motors equipped with a combined engine combustion section (31Y) for reducing friction loss water power generation with a turbine blade (8c) and a full blade impeller water turbine Various energy storage cycle coalescing engines as jet (79M) various water suction jet drive devices.   Turbine blade cross section (4B) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Turbine blade cross section (4B) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   A turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation using a full-rotor impeller water turbine and various types of combined engine injection section (79K) Various energy storage cycle coalescing engines as suction injection drive devices.   A turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) that performs hydroelectric power generation with a fully-rotor impeller water turbine and various types of combined engine injection section (79K) Various energy storage cycle coalescing engines as suction injection drive devices.   Combined engine injection with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined high temperature heating means (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), a combined high temperature heating means (3B) and a combined engine combustion section (31Y) for hydroelectric power generation by a water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined with turbine blade cross section (4C) capable of 910,000 times power and turbine blade (8c) and vertical bladed water turbine heating high temperature means (3B) all blade combustion part (32X) for hydroelectric power generation Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined with turbine blade cross section (4C) capable of 910,000 times power and turbine blade (8c) and vertical rotor blade water turbine, heating high temperature means (3B) all blade combustion section (32Y) for hydroelectric power generation Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation using a turbine blade (8c) and an all-wheel impeller water turbine and various types of combined engine injection section (79K) Various energy storage cycle coalescing engines as suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31Y) for hydroelectric power generation using a turbine blade (8c) and an all-wheel impeller water turbine and various types of combined engine injection section (79K) Various energy storage cycle coalescing engines as suction injection drive devices.   Turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation with reduced friction loss by a turbine blade (8c) and all blade impeller water turbine, combined engine injection section (79K ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31Y) for reducing friction loss hydroelectric power generation with a turbine blade (8c) and a fully moving blade propeller water turbine, and a combined engine injection section (79K) ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Turbine blade cross section (4B) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Turbine blade cross section (4B) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   A turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation using a full-rotor impeller water turbine and various types of combined engine injection section (79K) Various energy storage cycle coalescing engines as suction injection drive devices.   A turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) that performs hydroelectric power generation with a fully-rotor impeller water turbine and various types of combined engine injection section (79K) Various energy storage cycle coalescing engines as suction injection drive devices.   Combined engine injection with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined high temperature heating means (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), a combined high temperature heating means (3B) and a combined engine combustion section (31Y) for hydroelectric power generation by a water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined with turbine blade cross section (4C) capable of 910,000 times power and turbine blade (8c) and vertical bladed water turbine heating high temperature means (3B) all blade combustion part (32X) for hydroelectric power generation Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined with turbine blade cross section (4C) capable of 910,000 times power and turbine blade (8c) and vertical rotor blade water turbine, heating high temperature means (3B) all blade combustion section (32Y) for hydroelectric power generation Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation using a turbine blade (8c) and an all-wheel impeller water turbine and various types of combined engine injection section (79K) Various energy storage cycle coalescing engines as suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31Y) for hydroelectric power generation using a turbine blade (8c) and an all-wheel impeller water turbine and various types of combined engine injection section (79K) Various energy storage cycle coalescing engines as suction injection drive devices.   Turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation with reduced friction loss by a turbine blade (8c) and all blade impeller water turbine, combined engine injection section (79K ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31Y) for reducing friction loss hydroelectric power generation with a turbine blade (8c) and a fully moving blade propeller water turbine, and a combined engine injection section (79K) ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   A turbine blade cross-section (4B) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32X) for hydroelectric power generation using a vertical all-blade water turbine. Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4B) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation using a fully-rotated blade impeller water turbine. Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation with a fully moving impeller wheel turbine, and includes various types of heating equipment using heat. Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power (4C) and a turbine blade (8c) and heating blade high temperature means (3B) coalescence engine combustion section (31X) for hydroelectric power generation with a water turbine and various types of use of heat Combined engine injection unit (79K) including various heating equipment and various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross section (4C) capable of 910,000 times power (4C) and turbine blade (8c) and all blade impeller water turbine with heating high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation Combined engine injection unit (79K) including various heating equipment and various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32X) for hydroelectric power generation by heating high temperature means (3B) with a vertical all blade water turbine, Combined engine injection unit (79K) including various heating equipment and various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32Y) for hydroelectric power generation with heating high temperature means (3B) with a vertical all blade water turbine, Combined engine injection unit (79K) including various heating equipment and various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all blade combustion section (32X) that performs hydroelectric power generation using a vertical all blade water turbine. Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a whole blade combustion section (32Y) for hydroelectric power generation using a vertical all-blade water turbine. Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   It includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation with a fully-rotated blade impeller water turbine, and includes various types of heating equipment using heat. Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) that performs hydroelectric power generation with a fully-rotated blade impeller water turbine, and includes various types of heating equipment using heat Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation with reduced friction loss by a turbine blade (8c) and all-wheel impeller water turbine. Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a combined engine combustion section (31Y) that generates hydroelectric power with reduced friction loss by using a turbine blade (8c) and an all-wheel impeller water turbine. Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross-section (4B) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32X) for hydroelectric power generation using a vertical all-blade water turbine. Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4B) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation using a fully-rotated blade impeller water turbine. Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation with a fully moving impeller wheel turbine, and includes various types of heating equipment using heat. Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power (4C) and a turbine blade (8c) and heating blade high temperature means (3B) coalescence engine combustion section (31X) for hydroelectric power generation with a water turbine and various types of use of heat Combined engine injection unit (79K) including various heating equipment and various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross section (4C) capable of 910,000 times power (4C) and turbine blade (8c) and all blade impeller water turbine with heating high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation Combined engine injection unit (79K) including various heating equipment and various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32X) for hydroelectric power generation by heating high temperature means (3B) with a vertical all blade water turbine, Combined engine injection unit (79K) including various heating equipment and various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32Y) for hydroelectric power generation with heating high temperature means (3B) with a vertical all blade water turbine, Combined engine injection unit (79K) including various heating equipment and various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all blade combustion section (32X) that performs hydroelectric power generation using a vertical all blade water turbine. Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a whole blade combustion section (32Y) for hydroelectric power generation using a vertical all-blade water turbine. Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   It includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation with a fully-rotated blade impeller water turbine, and includes various types of heating equipment using heat. Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) that performs hydroelectric power generation with a fully-rotated blade impeller water turbine, and includes various types of heating equipment using heat Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation with reduced friction loss by a turbine blade (8c) and all-wheel impeller water turbine. Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a combined engine combustion section (31Y) that generates hydroelectric power with reduced friction loss by using a turbine blade (8c) and an all-wheel impeller water turbine. Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   Turbine blade cross-section (4B) capable of 910,000 times power, combined with turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, including various generators Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blade cross-section (4B) capable of 910,000 times power, combined with turbine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, including various generators Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection including various generators, including a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) for hydroelectric power generation with a fully moving impeller wheel turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including various generators with a combined turbine combustion section (31Y) for hydroelectric power generation with a turbine blade cross-section (4B) turbine blade (8c) capable of 910,000 times work rate and a fully-rotated blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Various generators including a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c) and a combined high temperature heating means (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller water turbine Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   Various generators including a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c) and a combined high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection unit (79K) including various generators Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection unit (79K) including various generators Various energy storage cycle combined engines as various air suction injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times power, turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, including various generators Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power, combined with turbine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, including various generators Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection including various generators with a combined turbine combustion section (31X) for hydroelectric power generation with a turbine blade cross section (4C) turbine blade (8c) capable of 910,000 times work rate and a fully moving blade spring turbine water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including various generators with a combined turbine combustion section (31Y) that performs hydroelectric power generation with a turbine blade cross section (4C) turbine blade (8c) capable of 910,000 times power and a full blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that reduces friction loss with all-wheel impeller water turbines and includes various generators Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31Y) for reducing friction loss with a fully-rotating blade impeller water turbine and including various generators Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross-section (4B) capable of 910,000 times power, combined with turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, including various generators Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blade cross-section (4B) capable of 910,000 times power, combined with turbine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, including various generators Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection including various generators, including a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) for hydroelectric power generation with a fully moving impeller wheel turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including various generators with a combined turbine combustion section (31Y) for hydroelectric power generation with a turbine blade cross-section (4B) turbine blade (8c) capable of 910,000 times work rate and a fully-rotated blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Various generators including a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c) and a combined high temperature heating means (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller water turbine Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   Various generators including a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c) and a combined high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection unit (79K) including various generators Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection unit (79K) including various generators Various energy storage cycle combined engines as various air suction injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times power, turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, including various generators Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power, combined with turbine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, including various generators Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection including various generators with a combined turbine combustion section (31X) for hydroelectric power generation with a turbine blade cross section (4C) turbine blade (8c) capable of 910,000 times work rate and a fully moving blade spring turbine water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including various generators with a combined turbine combustion section (31Y) that performs hydroelectric power generation with a turbine blade cross section (4C) turbine blade (8c) capable of 910,000 times power and a full blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that reduces friction loss with all-wheel impeller water turbines and includes various generators Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31Y) for reducing friction loss with a fully-rotating blade impeller water turbine and including various generators Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Combined engine including various motors with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine including various motors with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection section including various motors with a combined turbine combustion section (31X) for hydroelectric power generation with a turbine blade cross section (4B) turbine blade (8c) capable of 910,000 times work rate and a fully moving blade spring turbine water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section including various motors with a combined turbine combustion section (31Y) for hydroelectric power generation with a turbine blade cross section (4B) turbine blade (8c) capable of 910,000 times work rate and all-rotor impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Various motors with a turbine blade cross section (4C) capable of 910,000 times power (4C), a turbine blade (8c), and a combined high temperature heating means (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Various motors with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), a combined high temperature heating means (3B) and a combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection unit (79K) including electric motors Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection unit (79K) including electric motors Various energy storage cycle combined engines as various air suction injection drive devices.   Combined engine including various motors with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine including various motors with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation using a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection section including various motors with a combined turbine combustion section (31X) for hydroelectric power generation with a turbine blade cross section (4C) turbine blade (8c) capable of 910,000 times power and all-blade propeller wheel water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section including various motors with a combined turbine combustion section (31Y) for hydroelectric power generation with a turbine blade cross section (4C) turbine blade (8c) capable of 910,000 times work rate and all blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31X) that generates hydrodynamic power with reduced friction loss by a turbine blade (8c) and a fully driven blade water turbine, and includes various motors Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power and combined blade combustion unit (31Y) for reducing friction loss and hydroelectric power generation with all blade impeller water turbines and combining various motors Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine including various motors with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine including various motors with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection section including various motors with a combined turbine combustion section (31X) for hydroelectric power generation with a turbine blade cross section (4B) turbine blade (8c) capable of 910,000 times work rate and a fully moving blade spring turbine water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section including various motors with a combined turbine combustion section (31Y) for hydroelectric power generation with a turbine blade cross section (4B) turbine blade (8c) capable of 910,000 times work rate and all-rotor impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Various motors with a turbine blade cross section (4C) capable of 910,000 times power (4C), a turbine blade (8c), and a combined high temperature heating means (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Various motors with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), a combined high temperature heating means (3B) and a combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection unit (79K) including electric motors Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection unit (79K) including electric motors Various energy storage cycle combined engines as various air suction injection drive devices.   Combined engine including various motors with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine including various motors with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation using a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection section including various motors with a combined turbine combustion section (31X) for hydroelectric power generation with a turbine blade cross section (4C) turbine blade (8c) capable of 910,000 times power and all-blade propeller wheel water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section including various motors with a combined turbine combustion section (31Y) for hydroelectric power generation with a turbine blade cross section (4C) turbine blade (8c) capable of 910,000 times work rate and all blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31X) that generates hydrodynamic power with reduced friction loss by a turbine blade (8c) and a fully driven blade water turbine, and includes various motors Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power and combined blade combustion unit (31Y) for reducing friction loss and hydroelectric power generation with all blade impeller water turbines and combining various motors Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blade cross-section (4B) capable of 910,000 times work rate and turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross-section (4B) capable of 910,000-fold work efficiency, equipped with turbine blade (8c) and all blade combustion section (32Y) for hydroelectric generation with vertical all blade water turbine, and various hot water storage equipment Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation with a fully moving impeller wheel turbine, and includes various hot water storage equipment. Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Includes a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31Y) for hydroelectric power generation with a full bucket impeller water turbine, including various hot water storage equipment Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heated turbine (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller water turbine, and various types of hot water Combined engine injection unit (79K) including storage equipment and various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heated turbine (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine, and various types of hot water Combined engine injection unit (79K) including storage equipment and various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection unit (79K) including various hot water storage equipment and various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection unit (79K) including various hot water storage equipment and various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power and turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross-section (4C) capable of 910,000 times work rate, turbine blade (8c), and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, various hot water storage equipment Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   It includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation with a fully moving impeller wheel turbine, and includes various types of hot water storage equipment. Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   It includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) that performs hydroelectric power generation with a full blade impeller water turbine, including various hot water storage equipment. Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31X) for reducing friction loss with all blade impeller water turbines and various hot water storage equipment Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   Turbine blade cross section (4C) capable of 910,000 times work rate and various hot water storage equipment equipped with a combined engine combustion section (31Y) that generates hydrodynamic power with reduced friction loss by using a turbine blade (8c) and a turbine blade turbine. Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   Turbine blade cross-section (4B) capable of 910,000 times work rate and turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross-section (4B) capable of 910,000-fold work efficiency, equipped with turbine blade (8c) and all blade combustion section (32Y) for hydroelectric generation with vertical all blade water turbine, and various hot water storage equipment Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation with a fully moving impeller wheel turbine, and includes various hot water storage equipment. Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Includes a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31Y) for hydroelectric power generation with a full bucket impeller water turbine, including various hot water storage equipment Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heated turbine (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller water turbine, and various types of hot water Combined engine injection unit (79K) including storage equipment and various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heated turbine (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine, and various types of hot water Combined engine injection unit (79K) including storage equipment and various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection unit (79K) including various hot water storage equipment and various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection unit (79K) including various hot water storage equipment and various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power and turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross-section (4C) capable of 910,000 times work rate, turbine blade (8c), and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, various hot water storage equipment Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   It includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation with a fully moving impeller wheel turbine, and includes various types of hot water storage equipment. Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   It includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) that performs hydroelectric power generation with a full blade impeller water turbine, including various hot water storage equipment. Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31X) for reducing friction loss with all blade impeller water turbines and various hot water storage equipment Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   Turbine blade cross section (4C) capable of 910,000 times work rate and various hot water storage equipment equipped with a combined engine combustion section (31Y) that generates hydrodynamic power with reduced friction loss by using a turbine blade (8c) and a turbine blade turbine. Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   Includes turbine blade cross section (4B) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, including various rocket fuels Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Includes turbine blade cross section (4B) capable of 910,000 times power, turbine blade (8c) and full blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, including various rocket fuels Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Combined engine including a turbine blade cross-section (4B) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation using a turbine blade (8c) and all-wheel impeller water turbine, and mounting various rocket fuels Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine including a turbine blade cross-section (4B) capable of 910,000 times power and a combined engine combustion section (31Y) for hydroelectric power generation using a turbine blade (8c) and a fully-rotated impeller water turbine, including various rocket fuels Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Various rocket fuels equipped with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c) and a combined high temperature heating means (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller water turbine Combined engine injection part (79K) including various types of various energy storage cycle combined engines as various air suction injection drive devices.   Various rocket fuels with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), a combined high temperature heating means (3B) and a combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine Combined engine injection part (79K) including various types of various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection unit (79K) including various rocket fuels. Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection unit (79K) including various rocket fuels. Various energy storage cycle combined engines as various air suction injection drive devices.   Includes turbine blade cross section (4C) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, including various rocket fuels Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Includes turbine blade cross section (4C) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, including various rocket fuels Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Combined engine including a turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation using a turbine blade (8c) and an all-wheel impeller water turbine, including various rocket fuels Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine including various rocket fuels equipped with a combined turbine combustion section (31Y) for hydroelectric power generation with a turbine blade cross section (4C) turbine blade (8c) capable of 910,000 times power and all-blade propeller water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blade cross section (4C) capable of 910,000 times power (4C), turbine blade (8c), and combined rotor combustion unit (31X) for reducing friction loss with all blade impeller water turbine and equipped with various rocket fuels Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31Y) that reduces hydrodynamic power generation by reducing the friction loss with all-wheel impeller water turbines and equipped with various rocket fuels Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Includes turbine blade cross section (4B) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, including various rocket fuels Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Includes turbine blade cross section (4B) capable of 910,000 times power, turbine blade (8c) and full blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, including various rocket fuels Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Combined engine including a turbine blade cross-section (4B) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation using a turbine blade (8c) and all-wheel impeller water turbine, and mounting various rocket fuels Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine including a turbine blade cross-section (4B) capable of 910,000 times power and a combined engine combustion section (31Y) for hydroelectric power generation using a turbine blade (8c) and a fully-rotated impeller water turbine, including various rocket fuels Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Various rocket fuels equipped with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c) and a combined high temperature heating means (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller water turbine Combined engine injection part (79K) including various types of various energy storage cycle combined engines as various air suction injection drive devices.   Various rocket fuels with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), a combined high temperature heating means (3B) and a combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine Combined engine injection part (79K) including various types of various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection unit (79K) including various rocket fuels. Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection unit (79K) including various rocket fuels. Various energy storage cycle combined engines as various air suction injection drive devices.   Includes turbine blade cross section (4C) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, including various rocket fuels Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Includes turbine blade cross section (4C) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, including various rocket fuels Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Combined engine including a turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation using a turbine blade (8c) and an all-wheel impeller water turbine, including various rocket fuels Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine including various rocket fuels equipped with a combined turbine combustion section (31Y) for hydroelectric power generation with a turbine blade cross section (4C) turbine blade (8c) capable of 910,000 times power and all-blade propeller water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blade cross section (4C) capable of 910,000 times power (4C), turbine blade (8c), and combined rotor combustion unit (31X) for reducing friction loss with all blade impeller water turbine and equipped with various rocket fuels Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31Y) that reduces hydrodynamic power generation by reducing the friction loss with all-wheel impeller water turbines and equipped with various rocket fuels Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Various refrigeration equipment using cold heat with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation using a vertical all blade water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Various refrigeration equipment using cold heat with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation using a vertical all blade water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation using a fully-rotated blade impeller water turbine, and includes various refrigeration equipment using cold energy. Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation with a fully-rotor impeller water turbine, including various refrigeration equipment using cold energy Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heating blade high-speed turbine (3B) coalescence engine combustion section (31X) for hydroelectric power generation with a water turbine and various types of cold heat utilization Combined engine injection unit including refrigeration equipment (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heated turbine (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine, and various types of cold utilization Combined engine injection unit including refrigeration equipment (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), a high temperature heating means (3B) with a vertical all blade water turbine, and a whole blade combustion section (32X) for hydroelectric power generation, Combined engine injection part (79K) including various refrigeration equipment used Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a high temperature heating means (3B) all blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, Combined engine injection part (79K) including various refrigeration equipment used Various energy storage cycle combined engine as various air suction injection drive devices.   Various refrigeration equipment using cold heat with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all blade combustion section (32Y) that performs hydroelectric power generation with a vertical all blade water turbine. Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Includes a turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) for hydroelectric power generation using a fully-rotating blade impeller water turbine, including various refrigeration equipment using cold energy Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   It includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation using a fully-rotated blade impeller water turbine, including various refrigeration equipment using cold energy Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Refrigeration equipment using cold energy with a turbine blade cross-section (4C) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation with reduced friction loss using a turbine blade (8c) and a turbine blade turbine Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31Y) that generates hydroelectric power with reduced friction loss using a full blade impeller water turbine. Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   Various refrigeration equipment using cold heat with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation using a vertical all blade water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Various refrigeration equipment using cold heat with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation using a vertical all blade water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation using a fully-rotated blade impeller water turbine, and includes various refrigeration equipment using cold energy. Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation with a fully-rotor impeller water turbine, including various refrigeration equipment using cold energy Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heating blade high-speed turbine (3B) coalescence engine combustion section (31X) for hydroelectric power generation with a water turbine and various types of cold heat utilization Combined engine injection unit including refrigeration equipment (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heated turbine (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine, and various types of cold utilization Combined engine injection unit including refrigeration equipment (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), a high temperature heating means (3B) with a vertical all blade water turbine, and a whole blade combustion section (32X) for hydroelectric power generation, Combined engine injection part (79K) including various refrigeration equipment used Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a high temperature heating means (3B) all blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, Combined engine injection part (79K) including various refrigeration equipment used Various energy storage cycle combined engine as various air suction injection drive devices.   Various refrigeration equipment using cold heat with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all blade combustion section (32Y) that performs hydroelectric power generation with a vertical all blade water turbine. Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Includes a turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) for hydroelectric power generation using a fully-rotating blade impeller water turbine, including various refrigeration equipment using cold energy Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   It includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation using a fully-rotated blade impeller water turbine, including various refrigeration equipment using cold energy Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Refrigeration equipment using cold energy with a turbine blade cross-section (4C) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation with reduced friction loss using a turbine blade (8c) and a turbine blade turbine Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31Y) that generates hydroelectric power with reduced friction loss using a full blade impeller water turbine. Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   Turbine blade cross-section (4B) capable of 910,000 times work rate and turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross-section (4B) capable of 910,000 times work rate, equipped with turbine blade (8c) and all blade combustion section (32Y) for hydroelectric generation with vertical all blade water turbine, and various hot water piping equipment Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation with a fully-rotor impeller water turbine, including various hot water piping equipment Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) that performs hydroelectric power generation with a fully moving impeller wheel turbine, including various hot water piping equipment Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heated turbine (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller water turbine, and various types of hot water Combined engine injection unit (79K) including piping equipment and other various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heated turbine (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine, and various types of hot water Combined engine injection unit (79K) including piping equipment and other various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection unit (79K) including various hot water piping equipment equipment Various energy storage cycle combined engine as various air suction injection drive equipment.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection unit (79K) including various hot water piping equipment equipment Various energy storage cycle combined engine as various air suction injection drive equipment.   Turbine blade cross-section (4C) capable of 910,000 times power and turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation using vertical all blade water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power, and turbine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) for hydroelectric power generation with a fully-rotated blade impeller water turbine, including various hot water piping equipment Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation with a fully moving impeller wheel turbine, including various hot water piping equipment Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31X) for hydroelectric power generation with reduced friction loss by a fully-rotated blade impeller water turbine, and various hot water piping equipment Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31Y) that generates hydrodynamic power with reduced friction loss with a fully moving blade spring turbine water turbine. Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   Turbine blade cross-section (4B) capable of 910,000 times work rate and turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross-section (4B) capable of 910,000 times work rate, equipped with turbine blade (8c) and all blade combustion section (32Y) for hydroelectric generation with vertical all blade water turbine, and various hot water piping equipment Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation with a fully-rotor impeller water turbine, including various hot water piping equipment Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) that performs hydroelectric power generation with a fully moving impeller wheel turbine, including various hot water piping equipment Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heated turbine (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller water turbine, and various types of hot water Combined engine injection unit (79K) including piping equipment and other various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heated turbine (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine, and various types of hot water Combined engine injection unit (79K) including piping equipment and other various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection unit (79K) including various hot water piping equipment equipment Various energy storage cycle combined engine as various air suction injection drive equipment.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection unit (79K) including various hot water piping equipment equipment Various energy storage cycle combined engine as various air suction injection drive equipment.   Turbine blade cross-section (4C) capable of 910,000 times power and turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation using vertical all blade water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power, and turbine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) for hydroelectric power generation with a fully-rotated blade impeller water turbine, including various hot water piping equipment Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation with a fully moving impeller wheel turbine, including various hot water piping equipment Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31X) for hydroelectric power generation with reduced friction loss by a fully-rotated blade impeller water turbine, and various hot water piping equipment Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31Y) that generates hydrodynamic power with reduced friction loss with a fully moving blade spring turbine water turbine. Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   Combined turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine, including various vertical rise and fall Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined turbine blade cross section (4B) capable of 910,000 times power, turbine blade (8c) and full blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, including various vertical rise and fall Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection including a turbine blade cross section (4B) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation using a turbine blade (8c) and an all-wheel impeller water turbine, including various vertical rise and fall (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including a turbine blade cross section (4B) capable of 910,000 times power and a combined engine combustion section (31Y) for hydroelectric power generation using a turbine blade (8c) and a full blade impeller water turbine, and including various vertical rise and fall (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4C) capable of 910,000 times power (4C), turbine blade (8c) and all-blade impeller water turbine with heating high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation and various vertical rises Combined engine injection part (79K) including descent Various energy storage cycle combined engine as various air suction injection drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power (4C), turbine blade (8c), and all-blade propeller wheel water turbine with heating high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation, various vertical rises Combined engine injection part (79K) including descent Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) including vertical ascent and descent Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) including vertical ascent and descent Various energy storage cycle combined engines as various air suction injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, including various vertical rise and fall Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times power and turbine blade (8c) and all blade combustor (32Y) for hydroelectric power generation with vertical all blade water turbine, including various vertical rise and fall Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection including a turbine blade cross-section (4C) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation with a turbine blade (8c) and an all-wheel impeller water turbine, and including various vertical rise and fall (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation using a full-rotor impeller water turbine, including various vertical rise and fall (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined rotor combustion unit (31X) for hydroelectric power generation with reduced friction loss at all blade impeller water turbines, including various vertical rise and fall Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined rotor combustion unit (31Y) for hydroelectric power generation with reduced friction loss by all blade impeller water turbine, including various vertical rise and fall Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Combined turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine, including various vertical rise and fall Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined turbine blade cross section (4B) capable of 910,000 times power, turbine blade (8c) and full blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, including various vertical rise and fall Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection including a turbine blade cross section (4B) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation using a turbine blade (8c) and an all-wheel impeller water turbine, including various vertical rise and fall (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including a turbine blade cross section (4B) capable of 910,000 times power and a combined engine combustion section (31Y) for hydroelectric power generation using a turbine blade (8c) and a full blade impeller water turbine, and including various vertical rise and fall (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4C) capable of 910,000 times power (4C), turbine blade (8c) and all-blade impeller water turbine with heating high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation and various vertical rises Combined engine injection part (79K) including descent Various energy storage cycle combined engine as various air suction injection drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power (4C), turbine blade (8c), and all-blade propeller wheel water turbine with heating high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation, various vertical rises Combined engine injection part (79K) including descent Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) including vertical ascent and descent Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) including vertical ascent and descent Various energy storage cycle combined engines as various air suction injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, including various vertical rise and fall Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times power and turbine blade (8c) and all blade combustor (32Y) for hydroelectric power generation with vertical all blade water turbine, including various vertical rise and fall Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection including a turbine blade cross-section (4C) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation with a turbine blade (8c) and an all-wheel impeller water turbine, and including various vertical rise and fall (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation using a full-rotor impeller water turbine, including various vertical rise and fall (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined rotor combustion unit (31X) for hydroelectric power generation with reduced friction loss at all blade impeller water turbines, including various vertical rise and fall Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined rotor combustion unit (31Y) for hydroelectric power generation with reduced friction loss by all blade impeller water turbine, including various vertical rise and fall Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross-section (4B) capable of 910,000 times power, combined with turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, including various supersonic flight Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blade cross-section (4B) capable of 910,000 times power, combined with turbine blade (8c) and full blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, including various supersonic flight Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection including a supersonic flight including a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) for hydroelectric power generation with a water turbine. (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including a supersonic flight including a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation using a water turbine. (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   The turbine blade cross section (4C) capable of 910,000 times power and the supersonic blades (8c) and the combined high temperature heating means (3B) coalescence engine combustion section (31X) for hydroelectric power generation with all the moving blades impeller water turbine, and various supersonic speeds Combined engine injection unit including flight (79K) Various energy storage cycle combined engine as various air suction injection drive devices.   The turbine blade cross section (4C) capable of 910,000 times power and the supersonic blades (8c) and the combined high temperature heating means (3B) combined engine combustion section (31Y) for hydroelectric power generation with all blade impeller water turbines and various supersonic speeds Combined engine injection unit including flight (79K) Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) including supersonic flight Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) including supersonic flight Various energy storage cycle combined engine as various air suction injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times power and turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, including various supersonic flight Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, including various supersonic flight Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection including a supersonic flight with a turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion part (31X) for hydroelectric power generation with a turbine blade (8c) and a turbine blade turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including a supersonic flight including a turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31Y) for hydroelectric power generation with a turbine blade (8c) and a turbine blade turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   The turbine blade cross-section (4C) capable of 910,000 times power and the combined blades (8c) and the combined rotor combustion unit (31X) for reducing friction loss with all-wheel impeller water turbines, including various supersonic flights Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion part (31Y) for hydroelectric power generation with reduced friction loss at all blade impeller water turbines, including various supersonic flights Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross-section (4B) capable of 910,000 times power, combined with turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, including various supersonic flight Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blade cross-section (4B) capable of 910,000 times power, combined with turbine blade (8c) and full blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, including various supersonic flight Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection including a supersonic flight including a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) for hydroelectric power generation with a water turbine. (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including a supersonic flight including a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion unit (31Y) for hydroelectric power generation with a full-rotor impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   The turbine blade cross section (4C) capable of 910,000 times power and the supersonic blades (8c) and the combined high temperature heating means (3B) coalescence engine combustion section (31X) for hydroelectric power generation with all the moving blades impeller water turbine, and various supersonic speeds Combined engine injection unit including flight (79K) Various energy storage cycle combined engine as various air suction injection drive devices.   The turbine blade cross section (4C) capable of 910,000 times power and the supersonic blades (8c) and the combined high temperature heating means (3B) combined engine combustion section (31Y) for hydroelectric power generation with all blade impeller water turbines and various supersonic speeds Combined engine injection unit including flight (79K) Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) including supersonic flight Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) including supersonic flight Various energy storage cycle combined engine as various air suction injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times power and turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, including various supersonic flight Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, including various supersonic flight Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection including a supersonic flight with a turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion part (31X) for hydroelectric power generation with a turbine blade (8c) and a turbine blade turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including a supersonic flight including a turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31Y) for hydroelectric power generation with a turbine blade (8c) and a turbine blade turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   The turbine blade cross-section (4C) capable of 910,000 times power and the combined blades (8c) and the combined rotor combustion unit (31X) for reducing friction loss with all-wheel impeller water turbines, including various supersonic flights Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion part (31Y) for hydroelectric power generation with reduced friction loss at all blade impeller water turbines, including various supersonic flights Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Combined engine including various space flights with turbine blade cross section (4B) capable of 910,000 times power and turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blade cross section (4B) capable of 910,000 times power, combined turbine engine (8B) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, including various space flight Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection section including various space flights with turbine blade cross section (4B) capable of 910,000 times power, combined with turbine blade (8c) and combined engine combustion section (31X) for hydroelectric power generation with all blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section including various space flights with turbine blade cross section (4B) capable of 910,000 times power, combined with turbine blade (8c) and combined engine combustion section (31Y) for hydroelectric power generation with all blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   A variety of spaceflights equipped with a turbine blade cross section (4C) capable of 910,000 times power (4C), turbine blade (8c), and a combined high temperature heating means (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine. Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A variety of spaceflights equipped with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined high temperature heating means (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection unit (79K) including space flight Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection unit (79K) including space flight Various energy storage cycle combined engine as various air suction injection drive devices.   Combined engine including various spaceflights with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine including various spaceflights with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection section including various space flights with turbine blade cross section (4C) turbine blade (8c) capable of 910,000 times work and combined engine combustion section (31X) for hydroelectric power generation with all blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section including various space flights with a combined turbine combustion section (31Y) for hydroelectric power generation with a turbine blade cross section (4C) turbine blade (8c) capable of 910,000 times work rate and a fully moving blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times power, combined with a combined engine combustion section (31X) for reducing friction loss hydroelectric power generation with a turbine blade (8c) and all blade impeller water turbine, including various space flights Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times power, combined with a combined engine combustion section (31Y) that generates hydrodynamic power with reduced friction loss with a turbine blade (8c) and all-blade flywheel water turbine, including various space flights Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine including various space flights with turbine blade cross section (4B) capable of 910,000 times power and turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blade cross section (4B) capable of 910,000 times power, combined turbine engine (8B) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, including various space flight Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection section including various space flights with turbine blade cross section (4B) capable of 910,000 times power, combined with turbine blade (8c) and combined engine combustion section (31X) for hydroelectric power generation with all blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section including various space flights with turbine blade cross section (4B) capable of 910,000 times power, combined with turbine blade (8c) and combined engine combustion section (31Y) for hydroelectric power generation with all blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   A variety of spaceflights equipped with a turbine blade cross section (4C) capable of 910,000 times power (4C), turbine blade (8c), and a combined high temperature heating means (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine. Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A variety of spaceflights equipped with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined high temperature heating means (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection unit (79K) including space flight Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection unit (79K) including space flight Various energy storage cycle combined engine as various air suction injection drive devices.   Combined engine including various spaceflights with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine including various spaceflights with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times power, combined with a combined engine combustion section (31X) for reducing friction loss hydroelectric power generation with a turbine blade (8c) and all blade impeller water turbine, including various space flights Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times power, combined with a combined engine combustion section (31Y) that generates hydrodynamic power with reduced friction loss with a turbine blade (8c) and all-blade flywheel water turbine, including various space flights Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Various refrigeration equipment using cold heat with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation using a vertical all blade water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Various refrigeration equipment using cold heat with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation using a vertical all blade water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation using a fully-rotated blade impeller water turbine, and includes various refrigeration equipment using cold energy. Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation with a fully-rotor impeller water turbine, including various refrigeration equipment using cold energy Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heating blade high-speed turbine (3B) coalescence engine combustion section (31X) for hydroelectric power generation with a water turbine and various types of cold heat utilization Combined engine injection unit including refrigeration equipment (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heated turbine (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine, and various types of cold utilization Combined engine injection unit including refrigeration equipment (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), a high temperature heating means (3B) with a vertical all blade water turbine, and a whole blade combustion section (32X) for hydroelectric power generation, Combined engine injection part (79K) including various refrigeration equipment used Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a high temperature heating means (3B) all blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, Combined engine injection part (79K) including various refrigeration equipment used Various energy storage cycle combined engine as various air suction injection drive devices.   Various refrigeration equipment using cold heat with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all blade combustion section (32Y) that performs hydroelectric power generation with a vertical all blade water turbine. Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Includes a turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) for hydroelectric power generation using a fully-rotating blade impeller water turbine, including various refrigeration equipment using cold energy Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   It includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation using a fully-rotated blade impeller water turbine, including various refrigeration equipment using cold energy Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Refrigeration equipment using cold energy with a turbine blade cross-section (4C) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation with reduced friction loss using a turbine blade (8c) and a turbine blade turbine Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31Y) that generates hydroelectric power with reduced friction loss using a full blade impeller water turbine. Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   Various refrigeration equipment using cold heat with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation using a vertical all blade water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Various refrigeration equipment using cold heat with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation using a vertical all blade water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation using a fully-rotated blade impeller water turbine, and includes various refrigeration equipment using cold energy. Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation with a fully-rotor impeller water turbine, including various refrigeration equipment using cold energy Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heating blade high-speed turbine (3B) coalescence engine combustion section (31X) for hydroelectric power generation with a water turbine and various types of cold heat utilization Combined engine injection unit including refrigeration equipment (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heated turbine (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine, and various types of cold utilization Combined engine injection unit including refrigeration equipment (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), a high temperature heating means (3B) with a vertical all blade water turbine, and a whole blade combustion section (32X) for hydroelectric power generation, Combined engine injection part (79K) including various refrigeration equipment used Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a high temperature heating means (3B) all blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, Combined engine injection part (79K) including various refrigeration equipment used Various energy storage cycle combined engine as various air suction injection drive devices.   Various refrigeration equipment using cold heat with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all blade combustion section (32Y) that performs hydroelectric power generation with a vertical all blade water turbine. Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Includes a turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) for hydroelectric power generation using a fully-rotating blade impeller water turbine, including various refrigeration equipment using cold energy Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   It includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation using a fully-rotated blade impeller water turbine, including various refrigeration equipment using cold energy Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Refrigeration equipment using cold energy with a turbine blade cross-section (4C) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation with reduced friction loss using a turbine blade (8c) and a turbine blade turbine Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31Y) that generates hydroelectric power with reduced friction loss using a full blade impeller water turbine. Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross-section (4B) capable of 910,000 times power and a turbine blade (8c) and a whole blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and an all blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, and various cooling equipment using cold energy Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation with a fully-rotor impeller water turbine, and includes various types of cooling equipment using cold energy. Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation using a fully-rotated blade impeller water turbine, and includes various types of cooling equipment using cold energy. Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heating blade high-speed turbine (3B) coalescence engine combustion section (31X) for hydroelectric power generation with a water turbine and various types of cold heat utilization Combined engine injection unit (79K) including various cooling equipment and various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heated turbine (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine, and various types of cold utilization Combined engine injection unit (79K) including various cooling equipment and various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), a high temperature heating means (3B) with a vertical all blade water turbine, and a whole blade combustion section (32X) for hydroelectric power generation, Combined engine injection unit (79K) including various cooling equipments used Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a high temperature heating means (3B) all blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, Combined engine injection unit (79K) including various cooling equipments used Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all blade combustion section (32X) for hydroelectric power generation using a vertical all blade water turbine, and various cooling equipment using cold energy Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32Y) for hydroelectric power generation using a vertical all-blade water turbine. Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   It includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation with a water turbine impeller water turbine, and includes various types of cooling equipment using cold energy. Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   It includes a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31Y) for hydroelectric power generation using a fully-rotated blade impeller water turbine, and includes various types of cooling equipment using cold energy. Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a combined engine combustion section (31X) that reduces hydrodynamic power generation by reducing friction loss with a turbine blade spring turbine (8c) and various cooling equipment using cold energy Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a combined engine combustion section (31Y) that generates hydroelectric power with reduced friction loss by using a turbine blade (8c) and an all-wheel impeller water turbine. Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross-section (4B) capable of 910,000 times power and a turbine blade (8c) and a whole blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and an all blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, and various cooling equipment using cold energy Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation with a fully-rotor impeller water turbine, and includes various types of cooling equipment using cold energy. Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   It includes a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation using a fully-rotated blade impeller water turbine, and includes various types of cooling equipment using cold energy. Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heating blade high-speed turbine (3B) coalescence engine combustion section (31X) for hydroelectric power generation with a water turbine and various types of cold heat utilization Combined engine injection unit (79K) including various cooling equipment and various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a heated turbine (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine, and various types of cold utilization Combined engine injection unit (79K) including various cooling equipment and various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), a high temperature heating means (3B) with a vertical all blade water turbine, and a whole blade combustion section (32X) for hydroelectric power generation, Combined engine injection unit (79K) including various cooling equipments used. Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a high temperature heating means (3B) all blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine, Combined engine injection unit (79K) including various cooling equipments used Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all blade combustion section (32X) for hydroelectric power generation using a vertical all blade water turbine, and various cooling equipment using cold energy Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32Y) for hydroelectric power generation using a vertical all-blade water turbine. Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   It includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation with a water turbine impeller water turbine, and includes various types of cooling equipment using cold energy. Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   It includes a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31Y) for hydroelectric power generation using a fully-rotated blade impeller water turbine, and includes various types of cooling equipment using cold energy. Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a combined engine combustion section (31X) that reduces hydrodynamic power generation by reducing friction loss with a turbine blade spring turbine (8c) and various cooling equipment using cold energy Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a combined engine combustion section (31Y) that generates hydroelectric power with reduced friction loss by using a turbine blade (8c) and an all-wheel impeller water turbine. Engine unit (79K) including various types of energy storage cycle combined engine as various air suction injection drive devices.   Combined turbine blade cross section (4B) capable of 910,000 times power and turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, including various satellite installations Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blade cross-section (4B) capable of 910,000 times power (4B) and turbine blade (8c) and all-blade combustion section (32Y) for hydroelectric power generation with vertical all-blade water turbine, including various satellite installations Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection including a turbine blade cross section (4B) capable of 910,000 times power (4B) turbine blade (8c) and a combined engine combustion unit (31X) for hydroelectric power generation with a fully moving blade impeller water turbine, including various satellite installations (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including a turbine blade cross section (4B) capable of 910,000 times power and a combined blade combustion unit (31Y) for hydroelectric power generation using a turbine blade (8c) and a full blade impeller water turbine, including various satellite installations (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Various artificial satellites equipped with turbine blade cross section (4C) capable of 910,000 times power (4C), turbine blade (8c) and heating blade high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation with water turbine Combined engine injection part (79K) including installation Various energy storage cycle combined engine as various air suction injection drive devices.   Various artificial satellites equipped with turbine blade cross section (4C) capable of 910,000 times power (4C), turbine blade (8c) and all-rotor impeller water turbine heating high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation Combined engine injection part (79K) including installation Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a vertical blade-type all-blade water turbine with a high temperature heating means (3B) all blade combustion section (32X) for hydroelectric power generation Combined engine injection unit (79K) including artificial satellite installation Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection unit (79K) including artificial satellite installation Various energy storage cycle combined engine as various air suction injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times power, turbine blade (8c) and full blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, including various satellite installations Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times power and turbine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation by vertical all blade water turbine, including various satellite installations Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection, including a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller water turbine, including various satellite installations (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection, including a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation with a fully moving blade impeller water turbine, including various satellite installations (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that generates hydroelectric power with reduced friction loss using a fully-rotor impeller water turbine, including various satellite installations Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) that reduces hydrodynamic power generation by reducing the loss of friction with all-wheel impeller water turbines, including various satellite installations Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Combined turbine blade cross section (4B) capable of 910,000 times power and turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, including various satellite installations Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blade cross-section (4B) capable of 910,000 times power (4B) and turbine blade (8c) and all-blade combustion section (32Y) for hydroelectric power generation with vertical all-blade water turbine, including various satellite installations Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection including a turbine blade cross section (4B) capable of 910,000 times power (4B) turbine blade (8c) and a combined engine combustion unit (31X) for hydroelectric power generation with a fully moving blade impeller water turbine, including various satellite installations (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including a turbine blade cross section (4B) capable of 910,000 times power and a combined blade combustion unit (31Y) for hydroelectric power generation using a turbine blade (8c) and a full blade impeller water turbine, including various satellite installations (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Various artificial satellites equipped with turbine blade cross section (4C) capable of 910,000 times power (4C), turbine blade (8c) and heating blade high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation with water turbine Combined engine injection part (79K) including installation Various energy storage cycle combined engine as various air suction injection drive devices.   Various artificial satellites equipped with turbine blade cross section (4C) capable of 910,000 times power (4C), turbine blade (8c) and all-rotor impeller water turbine heating high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation Combined engine injection part (79K) including installation Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a vertical blade-type all-blade water turbine with a high temperature heating means (3B) all blade combustion section (32X) for hydroelectric power generation Combined engine injection unit (79K) including artificial satellite installation Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection unit (79K) including artificial satellite installation Various energy storage cycle combined engine as various air suction injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times power, turbine blade (8c) and full blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, including various satellite installations Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times power and turbine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation by vertical all blade water turbine, including various satellite installations Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection, including a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller water turbine, including various satellite installations (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection, including a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation with a fully moving blade impeller water turbine, including various satellite installations (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that generates hydroelectric power with reduced friction loss using a fully-rotor impeller water turbine, including various satellite installations Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) that reduces hydrodynamic power generation by reducing the loss of friction with all-wheel impeller water turbines, including various satellite installations Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Water including various generators with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine Various energy storage cycle coalescing engines as jet (79M) various water suction jet drive devices.   Turbine blade cross section (4B) capable of 910,000 times power and water including various generators with a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation using a vertical all blade water turbine Various energy storage cycle coalescing engines as jet (79M) various water suction jet drive devices.   Water jet including various generators, including a turbine blade cross section (4B) capable of 910,000 times work rate (4B), a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation with a water turbine impeller 79M) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Water jet including various generators with a turbine blade cross section (4B) capable of 910,000 times power and a combined engine combustion section (31Y) for hydroelectric power generation with a turbine blade (8c) and an all-wheel impeller water turbine 79M) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Various generators including a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c) and a combined high temperature heating means (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller water turbine Water-jet (79M) including various types of various energy storage cycle coalescing engines as various water suction / injection drive devices.   Various generators including a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c) and a combined high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine Water-jet (79M) including various types of various energy storage cycle coalescing engines as various water suction / injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines as water jet (79M) various water suction / injection drive devices including generators.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines as water jet (79M) various water suction / injection drive devices including generators.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation using a vertical all-blade water turbine and water including various generators Various energy storage cycle coalescing engines as jet (79M) various water suction jet drive devices.   Water including various generators with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine Various energy storage cycle coalescing engines as jet (79M) various water suction jet drive devices.   Water jet including various generators with a combined turbine combustion section (31X) for hydroelectric generation with a turbine blade cross section (4C) turbine blade (8c) capable of 910,000 times work rate and a full blade impeller water turbine 79M) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   A turbine jet section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined jet combustion section (31Y) that performs hydroelectric power generation with a fully-rotor impeller water turbine, a water jet including various generators ( 79M) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that reduces friction loss with all-wheel impeller water turbines and includes various generators Water Jet (79M) Various energy storage cycle coalescing engines as various water suction jet drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31Y) for reducing friction loss with a fully-rotating blade impeller water turbine and including various generators Water Jet (79M) Various energy storage cycle coalescing engines as various water suction jet drive devices.   Water including various generators with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine Various energy storage cycle coalescing engines as jet (79M) various water suction jet drive devices.   Turbine blade cross section (4B) capable of 910,000 times power and water including various generators with a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation using a vertical all blade water turbine Various energy storage cycle coalescing engines as jet (79M) various water suction jet drive devices.   Water jet including various generators, including a turbine blade cross section (4B) capable of 910,000 times work rate (4B), a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation with a water turbine impeller 79M) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Water jet including various generators with a turbine blade cross section (4B) capable of 910,000 times power and a combined engine combustion section (31Y) for hydroelectric power generation with a turbine blade (8c) and an all-wheel impeller water turbine 79M) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Various generators including a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c) and a combined high temperature heating means (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller water turbine Water-jet (79M) including various types of various energy storage cycle coalescing engines as various water suction / injection drive devices.   Various generators including a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c) and a combined high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine Water-jet (79M) including various types of various energy storage cycle coalescing engines as various water suction / injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines as water jet (79M) various water suction / injection drive devices including generators.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines as water jet (79M) various water suction / injection drive devices including generators.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation using a vertical all-blade water turbine and water including various generators Various energy storage cycle coalescing engines as jet (79M) various water suction jet drive devices.   Water including various generators with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine Various energy storage cycle coalescing engines as jet (79M) various water suction jet drive devices.   Water jet including various generators with a combined turbine combustion section (31X) for hydroelectric generation with a turbine blade cross section (4C) turbine blade (8c) capable of 910,000 times work rate and a full blade impeller water turbine 79M) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   A turbine jet section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined jet combustion section (31Y) that performs hydroelectric power generation with a fully-rotor impeller water turbine, a water jet including various generators ( 79M) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that reduces friction loss with all-wheel impeller water turbines and includes various generators Water Jet (79M) Various energy storage cycle coalescing engines as various water suction jet drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31Y) for reducing friction loss with a fully-rotating blade impeller water turbine and including various generators Water Jet (79M) Various energy storage cycle coalescing engines as various water suction jet drive devices.   Water jet including various electric motors with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation using a vertical all blade water turbine (79M) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Water jet including various electric motors with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine (79M) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Water jet (79M) including various motors with a turbine blade cross section (4B) capable of 910,000 times power and a combined engine combustion part (31X) for hydroelectric power generation with a turbine blade (8c) and a turbine blade turbine ) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Water jet (79M) including various electric motors, including a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation using a fully-rotor impeller water turbine ) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Various motors with a turbine blade cross section (4C) capable of 910,000 times power (4C), a turbine blade (8c), and a combined high temperature heating means (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller Water-jet (79M) including various energy storage cycle coalescing engines as various water suction / injection drive devices.   Various motors with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), a combined high temperature heating means (3B) and a combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller Water-jet (79M) including various energy storage cycle coalescing engines as various water suction / injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines as water jet (79M) various water suction jet drive devices including electric motors.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines as water jet (79M) various water suction jet drive devices including electric motors.   Water jet including various motors with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation using a vertical all blade water turbine (79M) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Water jet including various electric motors having a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation using a vertical all blade water turbine (79M) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Water jet (79M) including various electric motors, including a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) for hydroelectric power generation with a water turbine and a turbine moving turbine. ) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Water jet (79M) including various electric motors, including a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation with a fully moving blade impeller water turbine ) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Turbine blade cross section (4C) capable of 910,000 times power and water including various motors equipped with a combined engine combustion section (31X) for reducing friction loss hydroelectric power generation with a turbine blade (8c) and a turbine blade impeller water turbine Various energy storage cycle coalescing engines as jet (79M) various water suction jet drive devices.   Turbine blade cross section (4C) capable of 910,000 times power and water including various electric motors equipped with a combined engine combustion section (31Y) for reducing friction loss water power generation with a turbine blade (8c) and a full blade impeller water turbine Various energy storage cycle coalescing engines as jet (79M) various water suction jet drive devices.   Water jet including various electric motors with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine (79M) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Water jet including various electric motors with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine (79M) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Water jet (79M) including various motors with a turbine blade cross section (4B) capable of 910,000 times power and a combined engine combustion part (31X) for hydroelectric power generation with a turbine blade (8c) and a turbine blade turbine ) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Water jet (79M) including various electric motors, including a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation using a fully-rotor impeller water turbine ) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Various motors with a turbine blade cross section (4C) capable of 910,000 times power (4C), a turbine blade (8c), and a combined high temperature heating means (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller Water-jet (79M) including various energy storage cycle coalescing engines as various water suction / injection drive devices.   Various motors with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), a combined high temperature heating means (3B) and a combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller Water-jet (79M) including various energy storage cycle coalescing engines as various water suction / injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines as water jet (79M) various water suction jet drive devices including electric motors.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines as water jet (79M) various water suction jet drive devices including electric motors.   Water jet including various motors with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation using a vertical all blade water turbine (79M) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Water jet including various electric motors having a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation using a vertical all blade water turbine (79M) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Water jet (79M) including various electric motors, including a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) for hydroelectric power generation with a water turbine and a turbine moving turbine. ) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Water jet (79M) including various electric motors, including a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation with a fully moving blade impeller water turbine ) Various energy storage cycle coalescing engines as various water suction / injection drive devices.   Turbine blade cross section (4C) capable of 910,000 times power and water including various motors equipped with a combined engine combustion section (31X) for reducing friction loss hydroelectric power generation with a turbine blade (8c) and a turbine blade impeller water turbine Various energy storage cycle coalescing engines as jet (79M) various water suction jet drive devices.   Turbine blade cross section (4C) capable of 910,000 times power and water including various electric motors equipped with a combined engine combustion section (31Y) for reducing friction loss water power generation with a turbine blade (8c) and a full blade impeller water turbine Various energy storage cycle coalescing engines as jet (79M) various water suction jet drive devices.   Turbine blade cross section (4B) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Turbine blade cross section (4B) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   A turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation using a full-rotor impeller water turbine and various types of combined engine injection section (79K) Various energy storage cycle coalescing engines as suction injection drive devices.   A turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) that performs hydroelectric power generation with a fully-rotor impeller water turbine and various types of combined engine injection section (79K) Various energy storage cycle coalescing engines as suction injection drive devices.   Combined engine injection with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined high temperature heating means (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), a combined high temperature heating means (3B) and a combined engine combustion section (31Y) for hydroelectric power generation by a water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined with turbine blade cross section (4C) capable of 910,000 times power and turbine blade (8c) and vertical bladed water turbine heating high temperature means (3B) all blade combustion part (32X) for hydroelectric power generation Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined with turbine blade cross section (4C) capable of 910,000 times power and turbine blade (8c) and vertical rotor blade water turbine, heating high temperature means (3B) all blade combustion section (32Y) for hydroelectric power generation Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation using a turbine blade (8c) and an all-wheel impeller water turbine and various types of combined engine injection section (79K) Various energy storage cycle coalescing engines as suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31Y) for hydroelectric power generation using a turbine blade (8c) and an all-wheel impeller water turbine and various types of combined engine injection section (79K) Various energy storage cycle coalescing engines as suction injection drive devices.   Turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation with reduced friction loss by a turbine blade (8c) and all blade impeller water turbine, combined engine injection section (79K ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31Y) for reducing friction loss hydroelectric power generation with a turbine blade (8c) and a fully moving blade propeller water turbine, and a combined engine injection section (79K) ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Turbine blade cross section (4B) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Turbine blade cross section (4B) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   A turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that performs hydroelectric power generation using a full-rotor impeller water turbine and various types of combined engine injection section (79K) Various energy storage cycle coalescing engines as suction injection drive devices.   A turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) that performs hydroelectric power generation with a fully-rotor impeller water turbine and various types of combined engine injection section (79K) Various energy storage cycle coalescing engines as suction injection drive devices.   Combined engine injection with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined high temperature heating means (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), a combined high temperature heating means (3B) and a combined engine combustion section (31Y) for hydroelectric power generation by a water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined with turbine blade cross section (4C) capable of 910,000 times power and turbine blade (8c) and vertical bladed water turbine heating high temperature means (3B) all blade combustion part (32X) for hydroelectric power generation Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined with turbine blade cross section (4C) capable of 910,000 times power and turbine blade (8c) and vertical rotor blade water turbine, heating high temperature means (3B) all blade combustion section (32Y) for hydroelectric power generation Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, combined engine injection section (79K) Various energy storage cycle coalescing engines as various air suction jet drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation using a turbine blade (8c) and an all-wheel impeller water turbine and various types of combined engine injection section (79K) Various energy storage cycle coalescing engines as suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31Y) for hydroelectric power generation using a turbine blade (8c) and an all-wheel impeller water turbine and various types of combined engine injection section (79K) Various energy storage cycle coalescing engines as suction injection drive devices.   Turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation with reduced friction loss by a turbine blade (8c) and all blade impeller water turbine, combined engine injection section (79K ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31Y) for reducing friction loss hydroelectric power generation with a turbine blade (8c) and a fully moving blade propeller water turbine, and a combined engine injection section (79K) ) Various energy storage cycle coalescing engine as various air suction jet drive equipment.   Combined engine with various fighting abilities with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine with various fighting abilities with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) that performs hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection unit with various fighting capabilities, including a turbine blade cross section (4B) capable of 910,000 times power and a combined engine combustion unit (31X) for hydroelectric power generation with a turbine blade (8c) and all-wheel impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section including a combined engine combustion section (31Y) for hydroelectric power generation with a turbine blade cross section (4B) turbine blade (8c) capable of 910,000 times power and all-blade propeller wheel water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power (4C), a turbine blade (8c), a high-temperature heating means (3B) and a combined engine combustion section (31X) for hydroelectric power generation with all-wheel impeller water turbines and various combat capabilities Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   The turbine blade cross-section (4C) capable of 910,000 times power (4C) and the turbine blade (8c) and the all-wing blade impeller water turbine is equipped with a combined high-temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation and various combat capabilities Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) including combat capability Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) including combat capability Various energy storage cycle combined engine as various air suction injection drive devices.   Combined engine with various fighting abilities with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) that hydroelectrically generates power with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine with various fighting abilities with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) that performs hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection section including a combined blade combustion section (31X) for hydroelectric power generation with a turbine blade cross section (4C) turbine blade (8c) capable of 910,000 times work rate and a water turbine with all rotor blades. (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section including a combined blade combustion section (31Y) for hydroelectric power generation with a turbine blade cross section (4C) turbine blade (8c) capable of 910,000 times work rate and all-wheel impeller water turbine, and various combat capabilities (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times power and combined blade combustion unit (31X) for hydroelectric power generation with reduced friction loss with all blade impeller water turbines and combined with various combat capabilities Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined turbine blade cross-section (4C) capable of 910,000 times power and combined engine combustion section (31Y) for hydrodynamic power generation with reduced friction loss with all blade impeller wheel turbines (8C) and combined with various combat capabilities Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine with various fighting abilities with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine with various fighting abilities with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) that performs hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection unit with various fighting capabilities, including a turbine blade cross section (4B) capable of 910,000 times power and a combined engine combustion unit (31X) for hydroelectric power generation with a turbine blade (8c) and all-wheel impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section including a combined engine combustion section (31Y) for hydroelectric power generation with a turbine blade cross section (4B) turbine blade (8c) capable of 910,000 times power and all-blade propeller wheel water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power (4C), a turbine blade (8c), a high-temperature heating means (3B) and a combined engine combustion section (31X) for hydroelectric power generation with all-wheel impeller water turbines and various combat capabilities Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   The turbine blade cross-section (4C) capable of 910,000 times power (4C) and the turbine blade (8c) and the all-wing blade impeller water turbine is equipped with a combined high-temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation and various combat capabilities Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) including combat capability Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) including combat capability Various energy storage cycle combined engine as various air suction injection drive devices.   Combined engine with various fighting abilities with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) that hydroelectrically generates power with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine with various fighting abilities with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) that performs hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection section including a combined blade combustion section (31X) for hydroelectric power generation with a turbine blade cross section (4C) turbine blade (8c) capable of 910,000 times work rate and a water turbine with all rotor blades. (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section including a combined blade combustion section (31Y) for hydroelectric power generation with a turbine blade cross section (4C) turbine blade (8c) capable of 910,000 times work rate and all-wheel impeller water turbine, and various combat capabilities (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion part (31X) that reduces hydrodynamic power generation with reduced friction loss by using a turbine blade (8c) and a full blade driven water turbine. Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined turbine blade cross-section (4C) capable of 910,000 times power and combined engine combustion section (31Y) for hydrodynamic power generation with reduced friction loss with all blade impeller wheel turbines (8C) and combined with various combat capabilities Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined turbine blade cross section (4B) capable of 910,000 times power and turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, including various air combat capabilities Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blade cross-section (4B) capable of 910,000 times work rate, combined with turbine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, including various air combat capabilities Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection with various aerial warfare capabilities, including a turbine blade cross section (4B) capable of 910,000 times power and a combined engine combustion section (31X) that hydroelectrically generates power with a turbine blade (8c) and a full blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection with various aerial warfare capabilities, including a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation with a fully moving blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Various aerial battles with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined high temperature heating means (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller Combined engine injection unit (79K) including various types of various energy storage cycle combined engines as various air suction injection drive devices.   Various aerial battles with a turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined high temperature heating means (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine Combined engine injection unit (79K) including various types of various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) including air combat capability. Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) including air combat capability. Various energy storage cycle combined engine as various air suction injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times work rate, turbine blade (8c), and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, including various air combat capabilities Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times work rate and turbine blade (8c) and all blade combustion section (32Y) that performs hydroelectric power generation with vertical all blade water turbine, including various air combat capabilities Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection with various aerial warfare capabilities, including a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) for hydroelectric power generation with a water turbine. (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including a turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31Y) for hydroelectric power generation using a turbine blade (8c) and an all-wheel impeller water turbine, including various air combat capabilities (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that reduces friction loss with all-wheel impeller water turbines and includes various air combat capabilities Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   It includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) that reduces hydrodynamic power generation with all blade impeller water turbines and includes various air combat capabilities. Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Combined turbine blade cross section (4B) capable of 910,000 times power and turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, including various air combat capabilities Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blade cross-section (4B) capable of 910,000 times work rate, combined with turbine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, including various air combat capabilities Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection with various aerial warfare capabilities, including a turbine blade cross section (4B) capable of 910,000 times power and a combined engine combustion section (31X) that hydroelectrically generates power with a turbine blade (8c) and a full blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection with various aerial warfare capabilities, including a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation with a fully moving blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Various aerial battles with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined high temperature heating means (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller Combined engine injection unit (79K) including various types of various energy storage cycle combined engines as various air suction injection drive devices.   Various aerial battles with a turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined high temperature heating means (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine Combined engine injection unit (79K) including various types of various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) including air combat capability. Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) including air combat capability. Various energy storage cycle combined engine as various air suction injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times work rate, turbine blade (8c), and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, including various air combat capabilities Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times work rate and turbine blade (8c) and all blade combustion section (32Y) that performs hydroelectric power generation with vertical all blade water turbine, including various air combat capabilities Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection with various aerial warfare capabilities, including a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) for hydroelectric power generation with a water turbine. (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including a turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31Y) for hydroelectric power generation using a turbine blade (8c) and an all-wheel impeller water turbine, including various air combat capabilities (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that reduces friction loss with all-wheel impeller water turbines and includes various air combat capabilities Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   It includes a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) that reduces hydrodynamic power generation with all blade impeller water turbines and includes various air combat capabilities. Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Combined engine including various cockpits with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine including various cockpits with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection section including various cockpits with a combined turbine combustion section (31X) for hydroelectric power generation with a turbine blade cross section (4B) turbine blade (8c) capable of 910,000 times work rate and all-blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection unit including various cockpits with a combined turbine combustion section (31Y) for hydroelectric power generation by a turbine blade cross section (4B) turbine blade (8c) capable of 910,000 times power and all blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Various cockpits equipped with a turbine blade cross section (4C) capable of 910,000 times power (4C), turbine blade (8c), and combined high temperature heating means (3B) combined engine combustion section (31X) for hydroelectric power generation with water turbine impeller Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Various cockpits equipped with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a high temperature heating means (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection unit (79K) including cockpit, various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection unit (79K) including cockpit, various energy storage cycle combined engines as various air suction injection drive devices.   Combined engine including various cockpits with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine including various cockpits with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection part including various cockpits with a combined turbine combustion section (31X) for hydroelectric power generation with a turbine blade cross section (4C) turbine blade (8c) capable of 910,000 times work rate and all-rotor impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection unit including various cockpits with a combined turbine combustion section (31Y) for hydroelectric power generation with a turbine blade cross section (4C) turbine blade (8c) capable of 910,000 times work rate and a full blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times power, combined turbine combustion section (31X) for hydrodynamic power generation with reduced friction loss with all blade impeller wheel turbines (8C), combined with various cockpits Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times power and combined with a combined engine combustion section (31Y) for hydroelectric power generation with reduced friction loss with a turbine blade (8c) and all-blade propulsion wheel water turbine, including various cockpits Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine including various cockpits with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine including various cockpits with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection section including various cockpits with a combined turbine combustion section (31X) for hydroelectric power generation with a turbine blade cross section (4B) turbine blade (8c) capable of 910,000 times work rate and all-blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection unit including various cockpits with a combined turbine combustion section (31Y) for hydroelectric power generation by a turbine blade cross section (4B) turbine blade (8c) capable of 910,000 times power and all blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Various cockpits equipped with a turbine blade cross section (4C) capable of 910,000 times power (4C), turbine blade (8c), and combined high temperature heating means (3B) combined engine combustion section (31X) for hydroelectric power generation with water turbine impeller Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Various cockpits equipped with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a high temperature heating means (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection unit (79K) including cockpit, various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection unit (79K) including cockpit, various energy storage cycle combined engines as various air suction injection drive devices.   Combined engine including various cockpits with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine including various cockpits with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection part including various cockpits with a combined turbine combustion section (31X) for hydroelectric power generation with a turbine blade cross section (4C) turbine blade (8c) capable of 910,000 times work rate and all-rotor impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection unit including various cockpits with a combined turbine combustion section (31Y) for hydroelectric power generation with a turbine blade cross section (4C) turbine blade (8c) capable of 910,000 times work rate and a full blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times power, combined turbine combustion section (31X) for hydrodynamic power generation with reduced friction loss with all blade impeller wheel turbines (8C), combined with various cockpits Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times power, combined with a combined engine combustion section (31Y) for hydroelectric power generation with reduced friction loss with a turbine blade (8c) and all-wheel impeller spur water turbine, including various cockpits Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine including various control chambers with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine including various control chambers with turbine blade cross section (4B) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection unit including various control chambers, including a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion unit (31X) that performs hydroelectric power generation with a fully-rotor impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section including various control chambers, including a turbine blade cross section (4B) capable of 910,000 times power, a combined turbine combustion section (31Y) for hydroelectric power generation with a turbine blade (8c) and a full blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Various control chambers with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Various control chambers with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), a combined high temperature heating means (3B) and a combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) including control room Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) including control room Various energy storage cycle combined engine as various air suction injection drive devices.   Combined engine including various control chambers with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine including various control chambers with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection section including various control chambers with a combined turbine combustion section (31X) for hydroelectric power generation with a turbine blade cross section (4C) turbine blade (8c) capable of 910,000 times work rate and a fully moving blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section including various control chambers, including a turbine blade section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation using a fully-rotor impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined turbine blade section (4C) capable of 910,000 times power and combined blade combustion unit (31X) for reducing friction loss with all blade impeller water turbine and combined with various control chambers. Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times work rate, combined with a combined engine combustion section (31Y) for reducing friction loss hydroelectric power generation with a turbine blade (8c) and an all-blade propulsion wheel water turbine, including various control chambers Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine including various control chambers with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine including various control chambers with turbine blade cross section (4B) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection unit including various control chambers, including a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion unit (31X) that performs hydroelectric power generation with a fully-rotor impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section including various control chambers, including a turbine blade cross section (4B) capable of 910,000 times power, a combined turbine combustion section (31Y) for hydroelectric power generation with a turbine blade (8c) and a full blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Various control chambers with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Various control chambers with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), a combined high temperature heating means (3B) and a combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) including control room Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) including control room Various energy storage cycle combined engine as various air suction injection drive devices.   Combined engine including various control chambers with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine including various control chambers with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection section including various control chambers with a combined turbine combustion section (31X) for hydroelectric power generation with a turbine blade cross section (4C) turbine blade (8c) capable of 910,000 times work rate and a fully moving blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section including various control chambers, including a turbine blade section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation using a fully-rotor impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined turbine blade section (4C) capable of 910,000 times power and combined blade combustion unit (31X) for reducing friction loss with all blade impeller water turbine and combined with various control chambers. Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times work rate, combined with a combined engine combustion section (31Y) for reducing friction loss hydroelectric power generation with a turbine blade (8c) and an all-blade propulsion wheel water turbine, including various control chambers Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blade cross section (4B) capable of 910,000 times power (4B) Combined engine including various space trips with turbine blade (8c) and full blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine including various space travels with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection unit including various space travels, including a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion unit (31X) that performs hydroelectric power generation with a full blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection part including various space travels, equipped with turbine blade cross section (4B) turbine blade (8c) capable of 910,000 times work rate and combined engine combustion part (31Y) for hydroelectric power generation with all blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Various space travels with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined high temperature heating means (3B) combined combustion unit (31X) for hydroelectric power generation with a water turbine impeller Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Various space travels with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined high temperature heating means (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection unit (79K) including space travel Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection unit (79K) including space travel Various energy storage cycle combined engine as various air suction injection drive devices.   Combined engine including various space travels with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine including various space travels, equipped with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection part including various space travels, equipped with turbine blade cross section (4C) capable of 910,000 times power (4C), turbine blade (8c) and combined engine combustion unit (31X) for hydroelectric power generation with all blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section including various space travels, equipped with turbine blade cross section (4C) capable of 910,000 times power (4C) turbine blade (8c) and combined engine combustion section (31Y) for hydroelectric power generation with all-wheel impeller wheel turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined turbine blade cross-section (4C) capable of 910,000 times power and combined turbine combustion unit (31X) for reducing friction loss and hydroelectric power generation with all-blade propeller wheel water turbine, including various space trips Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined with a turbine blade cross-section (4C) capable of 910,000 times power and a combined engine combustion section (31Y) for hydroelectric power generation with reduced friction loss by a turbine blade (8c) and all-wheel impeller water turbine, including various space trips Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blade cross section (4B) capable of 910,000 times power (4B) Combined engine including various space trips with turbine blade (8c) and full blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine including various space travels with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection unit including various space travels, including a turbine blade cross section (4B) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion unit (31X) that performs hydroelectric power generation with a full blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection part including various space travels, equipped with turbine blade cross section (4B) turbine blade (8c) capable of 910,000 times work rate and combined engine combustion part (31Y) for hydroelectric power generation with all blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Various space travels with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined high temperature heating means (3B) combined combustion unit (31X) for hydroelectric power generation with a water turbine impeller Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Various space travels with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined high temperature heating means (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection unit (79K) including space travel Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection unit (79K) including space travel Various energy storage cycle combined engine as various air suction injection drive devices.   Combined engine including various space travels with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine including various space travels, equipped with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection part including various space travels, equipped with turbine blade cross section (4C) capable of 910,000 times power (4C), turbine blade (8c) and combined engine combustion unit (31X) for hydroelectric power generation with all blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section including various space travels, equipped with turbine blade cross section (4C) capable of 910,000 times power (4C) turbine blade (8c) and combined engine combustion section (31Y) for hydroelectric power generation with all-wheel impeller wheel turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined turbine blade cross-section (4C) capable of 910,000 times power and combined turbine combustion unit (31X) for reducing friction loss and hydroelectric power generation with all-blade propeller wheel water turbine, including various space trips Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined with a turbine blade cross-section (4C) capable of 910,000 times power and a combined engine combustion section (31Y) for hydroelectric power generation with reduced friction loss by a turbine blade (8c) and all-wheel impeller water turbine, including various space trips Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection including various cabins with turbine blade cross section (4B) capable of 910,000 times power and turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including various cabins with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection part including various cabins with a turbine blade cross section (4B) capable of 910,000 times power and a combined engine combustion part (31X) for hydroelectric power generation with a turbine blade (8c) and a full bucket impeller water turbine 79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section including various cabins equipped with a turbine blade cross section (4B) capable of 910,000 times power (4B) and a combined engine combustion section (31Y) for hydroelectric power generation with a fully moving blade impeller water turbine ( 79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and heating blade high-temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation in all turbines and various cabins Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and heating blade high-temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation in all turbines and various cabins Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) including guest rooms Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) including guest rooms Various energy storage cycle combined engines as various air suction injection drive devices.   Combined engine injection including various cabins with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including various cabins with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section including various cabins with a turbine blade cross section (4C) capable of 910,000 times work rate and a combined engine combustion section (31X) for hydroelectric power generation with a turbine blade (8c) and a full blade impeller water turbine 79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section including various cabins with a turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31Y) for hydroelectric power generation with a turbine blade (8c) and all-wheel impeller water turbine 79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine including various cabins with a turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31X) that generates hydrodynamic power with reduced friction loss using a turbine blade (8c) and a turbine blade turbine. Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine including various cabins equipped with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion unit (31Y) for reducing friction loss with all-wheel impeller water turbines and hydroelectric power generation Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection including various cabins with turbine blade cross section (4B) capable of 910,000 times power and turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including various cabins with a turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection part including various cabins with a turbine blade cross section (4B) capable of 910,000 times power and a combined engine combustion part (31X) for hydroelectric power generation with a turbine blade (8c) and a full bucket impeller water turbine 79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section including various cabins equipped with a turbine blade cross section (4B) capable of 910,000 times power (4B) and a combined engine combustion section (31Y) for hydroelectric power generation with a fully moving blade impeller water turbine ( 79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and heating blade high-temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation in all turbines and various cabins Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and heating blade high-temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation in all turbines and various cabins Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) including guest rooms Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) including guest rooms Various energy storage cycle combined engines as various air suction injection drive devices.   Combined engine injection including various cabins with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including various cabins with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) for hydroelectric power generation with a vertical all blade water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section including various cabins with a turbine blade cross section (4C) capable of 910,000 times work rate and a combined engine combustion section (31X) for hydroelectric power generation with a turbine blade (8c) and a full blade impeller water turbine 79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section including various cabins with a turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31Y) for hydroelectric power generation with a turbine blade (8c) and all-wheel impeller water turbine 79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine including various cabins with a turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31X) that generates hydrodynamic power with reduced friction loss using a turbine blade (8c) and a turbine blade turbine. Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine including various cabins equipped with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion unit (31Y) for reducing friction loss with all-wheel impeller water turbines and hydroelectric power generation Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blade cross section capable of 910,000 times power (4B) Combined engine including various cargo chambers with turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blade cross section capable of 910,000 times power (4B) Combined engine including various cargo compartments with turbine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection section including various cargo compartments with a combined turbine combustion section (31X) for hydroelectric power generation with a turbine blade cross section (4B) turbine blade (8c) capable of 910,000 times work rate and a full blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4B) capable of 910,000 times power and combined engine combustion section (31Y) for hydroelectric power generation with all blade impeller water turbines and combined engine injection section including various cargo chambers (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Various cargo compartments with turbine blade cross-section (4C) capable of 910,000 times power (4C), turbine blade (8c) and heating blade high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation with water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Various cargo compartments with turbine blade cross-section (4C) capable of 910,000 times power (4C), turbine blade (8c), all-wheel impeller water turbine, heating high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) including cargo compartments Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) including cargo compartments Various energy storage cycle combined engines as various air suction injection drive devices.   Combined engine including various cargo compartments with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power, combined engine with various blades equipped with turbine blade (8c) and full blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection section including various cargo compartments with a combined turbine combustion section (31X) for hydroelectric power generation with a turbine blade cross section (4C) turbine blade (8c) capable of 910,000 times power and all-blade propeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section including various cargo compartments with a combined turbine combustion section (31Y) for hydroelectric power generation with a turbine blade cross section (4C) turbine blade (8c) capable of 910,000 times work rate and all-rotor impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31X) that generates hydrodynamic power with reduced friction loss by using a turbine blade (8c) and an all-bladed flywheel water turbine. Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined turbine blade section (4C) capable of 910,000 times power, combined with a combined engine combustion section (31Y) for hydroelectric power generation with reduced friction loss with a turbine blade (8c) and all-blade propeller wheel water turbine, including various cargo chambers Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blade cross section capable of 910,000 times power (4B) Combined engine including various cargo chambers with turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blade cross section capable of 910,000 times power (4B) Combined engine including various cargo compartments with turbine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection section including various cargo compartments with a combined turbine combustion section (31X) for hydroelectric power generation with a turbine blade cross section (4B) turbine blade (8c) capable of 910,000 times work rate and a full blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4B) capable of 910,000 times power and combined engine combustion section (31Y) for hydroelectric power generation with all blade impeller water turbines and combined engine injection section including various cargo chambers (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Various cargo compartments with turbine blade cross-section (4C) capable of 910,000 times power (4C), turbine blade (8c) and heating blade high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation with water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Various cargo compartments with turbine blade cross-section (4C) capable of 910,000 times power (4C), turbine blade (8c), all-wheel impeller water turbine, heating high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) including cargo compartments Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) including cargo compartments Various energy storage cycle combined engines as various air suction injection drive devices.   Combined engine including various cargo compartments with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power, combined engine with various blades equipped with turbine blade (8c) and full blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection section including various cargo compartments with a combined turbine combustion section (31X) for hydroelectric power generation with a turbine blade cross section (4C) turbine blade (8c) capable of 910,000 times power and all-blade propeller wheel water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section including various cargo compartments with a combined turbine combustion section (31Y) for hydroelectric power generation with a turbine blade cross section (4C) turbine blade (8c) capable of 910,000 times work rate and all-rotor impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31X) that generates hydrodynamic power with reduced friction loss by using a turbine blade (8c) and an all-bladed flywheel water turbine. Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined turbine blade section (4C) capable of 910,000 times power, combined with a combined engine combustion section (31Y) for hydroelectric power generation with reduced friction loss with a turbine blade (8c) and all-blade propeller wheel water turbine, including various cargo chambers Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine, including various vertical rise and fall Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined turbine blade cross section (4B) capable of 910,000 times power, turbine blade (8c) and full blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, including various vertical rise and fall Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection including a turbine blade cross section (4B) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation using a turbine blade (8c) and an all-wheel impeller water turbine, including various vertical rise and fall (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including a turbine blade cross section (4B) capable of 910,000 times power and a combined engine combustion section (31Y) for hydroelectric power generation using a turbine blade (8c) and a full blade impeller water turbine, and including various vertical rise and fall (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4C) capable of 910,000 times power (4C), turbine blade (8c) and all-blade impeller water turbine with heating high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation and various vertical rises Combined engine injection part (79K) including descent Various energy storage cycle combined engine as various air suction injection drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power (4C), turbine blade (8c), and all-blade propeller wheel water turbine with heating high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation, various vertical rises Combined engine injection part (79K) including descent Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) including vertical ascent and descent Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) including vertical ascent and descent Various energy storage cycle combined engines as various air suction injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, including various vertical rise and fall Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times power and turbine blade (8c) and all blade combustor (32Y) for hydroelectric power generation with vertical all blade water turbine, including various vertical rise and fall Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection including a turbine blade cross-section (4C) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation with a turbine blade (8c) and an all-wheel impeller water turbine, and including various vertical rise and fall (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation using a full-rotor impeller water turbine, including various vertical rise and fall (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined rotor combustion unit (31X) for hydroelectric power generation with reduced friction loss at all blade impeller water turbines, including various vertical rise and fall Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined rotor combustion unit (31Y) for hydroelectric power generation with reduced friction loss by all blade impeller water turbine, including various vertical rise and fall Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Combined turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine, including various vertical rise and fall Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined turbine blade cross section (4B) capable of 910,000 times power, turbine blade (8c) and full blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, including various vertical rise and fall Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection including a turbine blade cross section (4B) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation using a turbine blade (8c) and an all-wheel impeller water turbine, including various vertical rise and fall (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including a turbine blade cross section (4B) capable of 910,000 times power and a combined engine combustion section (31Y) for hydroelectric power generation using a turbine blade (8c) and a full blade impeller water turbine, and including various vertical rise and fall (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Turbine blade cross section (4C) capable of 910,000 times power (4C), turbine blade (8c) and all-blade impeller water turbine with heating high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation and various vertical rises Combined engine injection part (79K) including descent Various energy storage cycle combined engine as various air suction injection drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power (4C), turbine blade (8c), and all-blade propeller wheel water turbine with heating high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation, various vertical rises Combined engine injection part (79K) including descent Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) including vertical ascent and descent Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) including vertical ascent and descent Various energy storage cycle combined engines as various air suction injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, including various vertical rise and fall Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times power and turbine blade (8c) and all blade combustor (32Y) for hydroelectric power generation with vertical all blade water turbine, including various vertical rise and fall Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection including a turbine blade cross-section (4C) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation with a turbine blade (8c) and an all-wheel impeller water turbine, and including various vertical rise and fall (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31Y) for hydroelectric power generation using a full-rotor impeller water turbine, including various vertical rise and fall (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined rotor combustion unit (31X) for hydroelectric power generation with reduced friction loss at all blade impeller water turbines, including various vertical rise and fall Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined rotor combustion unit (31Y) for hydroelectric power generation with reduced friction loss by all blade impeller water turbine, including various vertical rise and fall Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross section (4B) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross section (4B) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, various vertical ascending and descending airfield anywhere Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4B) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31X) for hydroelectric power generation with a fully-rotor impeller water turbine and various vertical ascent and descent locations including airfields Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31Y) that performs hydroelectric power generation with a fully-rotor impeller water turbine, and includes aerodrome anywhere in various vertical ascent and descent Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross section (4C) capable of 910,000 times power (4C), turbine blade (8c) and all-blade impeller water turbine with heating high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation and various vertical rises Combined engine injection part (79K) including airfields everywhere in the descent Various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross-section (4C) capable of 910,000 times power (4C), turbine blade (8c), and all-blade propeller wheel water turbine with heating high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation, various vertical rises Combined engine injection part (79K) including airfields everywhere in the descent Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) with various air suction injection drive devices including vertical airfields wherever vertical ascending and descending various energy storage cycle combined engines.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) with various air suction injection drive devices including vertical airfields wherever vertical ascending and descending various energy storage cycle combined engines.   Turbine blade cross-section (4C) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32X) for hydroelectric power generation with vertical all-blade water turbine. Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross section (4C) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31X) that performs hydroelectric power generation with a full-rotor impeller water turbine, including an airfield anywhere in various vertical ascent and descent Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31Y) that performs hydroelectric power generation with a fully moving blade impeller water turbine, and includes various aerodrome every vertical up and down Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   It has a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that reduces friction loss with all-wheel impeller water turbine, and various vertical rise and fall Combined engine injection unit (79K) including airfield Various energy storage cycle combined engine as various air suction injection drive devices.   The turbine blade cross section (4C) capable of 910,000 times power and the combined blade combustion unit (31Y) that reduces hydrodynamic power generation by reducing the friction loss with the turbine blade (8c) and the all-blade propulsion wheel water turbine. Combined engine injection unit (79K) including airfield Various energy storage cycle combined engine as various air suction injection drive devices.   Turbine blade cross section (4B) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross section (4B) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, various vertical ascending and descending airfield anywhere Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4B) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31X) for hydroelectric power generation with a fully-rotor impeller water turbine and various vertical ascent and descent locations including airfields Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31Y) that performs hydroelectric power generation with a fully-rotor impeller water turbine, and includes aerodrome anywhere in various vertical ascent and descent Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross section (4C) capable of 910,000 times power (4C), turbine blade (8c) and all-blade impeller water turbine with heating high temperature means (3B) combined engine combustion section (31X) for hydroelectric power generation and various vertical rises Combined engine injection part (79K) including airfields everywhere in the descent Various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross section (4C) capable of 910,000 times power (4C), turbine blade (8c), and all-blade propeller wheel water turbine equipped with heating high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation, various vertical rises Combined engine injection part (79K) including airfields anywhere in the descent Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) with various air suction injection drive devices including vertical airfields wherever vertical ascending and descending various energy storage cycle combined engines.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) with various air suction injection drive devices including vertical airfields wherever vertical ascending and descending various energy storage cycle combined engines.   Turbine blade cross-section (4C) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32X) for hydroelectric power generation with vertical all-blade water turbine. Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross section (4C) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31X) that performs hydroelectric power generation with a full-rotor impeller water turbine, including an airfield anywhere in various vertical ascent and descent Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31Y) that performs hydroelectric power generation with a fully moving blade impeller water turbine, and includes various aerodrome every vertical up and down Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   It has a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) that reduces friction loss with all-wheel impeller water turbine, and various vertical rise and fall Combined engine injection unit (79K) including airfield Various energy storage cycle combined engine as various air suction injection drive devices.   The turbine blade cross section (4C) capable of 910,000 times power and the combined blade combustion unit (31Y) that reduces hydrodynamic power generation by reducing the friction loss with the turbine blade (8c) and the all-blade propulsion wheel water turbine. Combined engine injection unit (79K) including airfield Various energy storage cycle combined engine as various air suction injection drive devices.   Turbine blade cross section (4B) capable of 910,000 times power, combined with a blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine, and a combined engine including various asteroid landings Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine including various asteroid landings with turbine blade cross section (4B) capable of 910,000 times power and turbine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection part including various asteroid landings, equipped with turbine blade cross section (4B) capable of 910,000 times power (4B), turbine blade (8c), and combined engine combustion part (31X) for hydroelectric power generation with all-wheel impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection part including various asteroid landings, equipped with turbine blade cross section (4B) capable of 910,000 times power, combined with turbine blade (8c) and combined engine combustion part (31Y) for hydroelectric power generation with all blade impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Various asteroid landings equipped with a turbine blade cross section (4C) capable of 910,000 times power (4C), turbine blade (8c), and combined high temperature heating means (3B) combined engine combustion section (31X) for hydroelectric power generation with water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Various asteroid landings with turbine blade cross-section (4C) capable of 910,000 times power (4C), turbine blade (8c), all-wheel impeller wheel turbine and heating high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) including asteroid landing Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) including asteroid landing Various energy storage cycle combined engine as various air suction injection drive devices.   Combined engine including various asteroid landings with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine including various asteroid landings with turbine blade cross section (4C) capable of 910,000 times work and turbine blade (8c) and all blade combustion section (32Y) hydroelectric power generation with vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection section including various asteroid landings with a combined turbine combustion section (31X) for hydroelectric power generation with a turbine blade cross section (4C) turbine blade (8c) and all-wheel impeller wheel turbine capable of 910,000 times power (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section including various asteroid landings with a combined turbine combustion section (31Y) for hydroelectric power generation with a turbine blade cross section (4C) turbine blade (8c) and all blade impeller water turbine capable of 910,000 times power (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times power and combined blade combustion unit (31X) for hydrodynamic power generation with reduced friction loss with all blade impeller water turbines, including various asteroid landings Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times work rate, combined turbine combustion section (31Y) for hydroelectric power generation with reduced friction loss with all blade impeller wheel turbines (8C), including various asteroid landings Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Turbine blade cross section (4B) capable of 910,000 times power, combined with a blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine, and a combined engine including various asteroid landings Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine including various asteroid landings with turbine blade cross section (4B) capable of 910,000 times power and turbine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection part including various asteroid landings, equipped with turbine blade cross section (4B) capable of 910,000 times power (4B), turbine blade (8c), and combined engine combustion part (31X) for hydroelectric power generation with all-wheel impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection section including various asteroid landings, including a turbine blade cross section (4B) capable of 910,000 times power, a combined turbine combustion section (31Y) for hydroelectric power generation with a turbine blade (8c) and an all-wheel impeller water turbine (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Various asteroid landings equipped with a turbine blade cross section (4C) capable of 910,000 times power (4C), turbine blade (8c), and combined high temperature heating means (3B) combined engine combustion section (31X) for hydroelectric power generation with water turbine Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Various asteroid landings with a turbine blade cross section (4C) capable of 910,000 times power (4C), turbine blade (8c), and a high temperature heating means (3B) combined engine combustion section (31Y) for hydroelectric power generation with a water turbine impeller Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) including asteroid landing Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection part (79K) including asteroid landing Various energy storage cycle combined engine as various air suction injection drive devices.   Combined engine including various asteroid landings with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine including various asteroid landings with turbine blade cross section (4C) capable of 910,000 times work and turbine blade (8c) and all blade combustion section (32Y) hydroelectric power generation with vertical all blade water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times power and combined blade combustion unit (31X) for hydrodynamic power generation with reduced friction loss with all blade impeller water turbines, including various asteroid landings Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times work rate, combined turbine combustion section (31Y) for hydroelectric power generation with reduced friction loss with all blade impeller wheel turbines (8C), including various asteroid landings Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   A turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) that performs hydroelectric power generation with a vertical all blade water turbine, including various lunar landing starts Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) that performs hydroelectric power generation with a vertical all-blade water turbine, including various lunar landing starts Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Combined engine with various lunar landing starts, equipped with turbine blade cross section (4B) capable of 910,000 times work rate, combined with turbine blade (8c) and combined engine combustion section (31X) for hydroelectric power generation with all blade impeller water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine including various lunar landing starts with a turbine blade cross section (4B) capable of 910,000 times power and a combined engine combustion section (31Y) for hydroelectric power generation with a turbine blade (8c) and a turbine blade turbine. Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Various lunar surfaces with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined high temperature heating means (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller water turbine Combined engine injection unit (79K) including landing start Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a heating blade high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation with various rotor blades and various lunar surfaces Combined engine injection unit (79K) including landing start Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection section (79K) including various types of energy storage cycle combined engines including various types of air suction injection drive devices including lunar landing start.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection section (79K) including various types of energy storage cycle combined engines including various types of air suction injection drive devices including lunar landing start.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a full-blade combustion section (32X) for hydroelectric power generation using a vertical all-blade water turbine, including various lunar landing starts Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a full-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, including various lunar landing starts Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Combined engine including various lunar landing starts with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) for hydroelectric power generation using a water turbine. Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine including various lunar landing starts with a combined turbine combustion section (31Y) for hydroelectric power generation with a turbine blade cross section (4C) turbine blade (8c) capable of 910,000 times power and all-blade propeller water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   It is equipped with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31X) that generates hydrodynamic power with reduced friction loss using a fully-rotor impeller water turbine. Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   It has a turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31Y) that reduces friction loss with a turbine blade (8c) and an all-wheel impeller water turbine to start various lunar landings. Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) that performs hydroelectric power generation with a vertical all blade water turbine, including various lunar landing starts Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32Y) that performs hydroelectric power generation with a vertical all-blade water turbine, including various lunar landing starts Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Combined engine with various lunar landing starts, equipped with turbine blade cross section (4B) capable of 910,000 times work rate, combined with turbine blade (8c) and combined engine combustion section (31X) for hydroelectric power generation with all blade impeller water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine including various lunar landing starts with a turbine blade cross section (4B) capable of 910,000 times power and a combined engine combustion section (31Y) for hydroelectric power generation with a turbine blade (8c) and a turbine blade turbine. Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Various lunar surfaces with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined high temperature heating means (3B) combined engine combustion section (31X) for hydroelectric power generation with a water turbine impeller water turbine Combined engine injection unit (79K) including landing start Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a heating blade high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation with various rotor blades and various lunar surfaces Combined engine injection unit (79K) including landing start Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection section (79K) including various types of energy storage cycle combined engines including various types of air suction injection drive devices including lunar landing start.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection section (79K) including various types of energy storage cycle combined engines including various types of air suction injection drive devices including lunar landing start.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a full-blade combustion section (32X) for hydroelectric power generation using a vertical all-blade water turbine, including various lunar landing starts Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a full-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, including various lunar landing starts Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Combined engine including various lunar landing starts with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined engine combustion section (31X) for hydroelectric power generation using a water turbine. Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine including various lunar landing starts with a combined turbine combustion section (31Y) for hydroelectric power generation with a turbine blade cross section (4C) turbine blade (8c) capable of 910,000 times power and all-blade propeller water turbine Injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   It is equipped with a turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined engine combustion section (31X) that generates hydrodynamic power with reduced friction loss using a fully-rotor impeller water turbine. Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   It has a turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31Y) that reduces friction loss with a turbine blade (8c) and an all-wheel impeller water turbine to start various lunar landings. Combined engine injection unit (79K) including various energy storage cycle combined engines as various air suction injection drive devices.   Combined turbine blade cross section (4B) capable of 910,000 times power, turbine blade (8c) and full blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, including various solar system escape rates Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined turbine blade cross section (4B) capable of 910,000 times work rate, turbine blade (8c), and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, including various solar system escape rates Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection including a turbine blade cross-section (4B) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation using a turbine blade (8c) and an all-wheel impeller water turbine, and including various solar system escape speeds (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including a turbine blade cross section (4B) capable of 910,000 times power and a combined engine combustion section (31Y) for hydroelectric power generation using a turbine blade (8c) and an all-wheel impeller water turbine, and including various solar system escape speeds (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Equipped with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a high temperature heating means (3B) combined engine combustion section (31X) for hydroelectric power generation with all blade impeller wheel turbines to escape various solar systems Combined engine injection part (79K) including speed Various energy storage cycle combined engine as various air suction injection drive devices.   Equipped with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined high temperature heating means (3B) combined engine combustion section (31Y) for hydroelectric power generation with all blade impeller wheel turbines to escape various solar systems Combined engine injection part (79K) including speed Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection unit (79K) including various solar system escape speeds Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection unit (79K) including various solar system escape speeds Various energy storage cycle combined engines as various air suction injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times power, turbine blade (8c) and full blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, including various solar system escape rates Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined turbine blade cross-section (4C) capable of 910,000 times power and turbine blade (8c) and full blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, including various solar system escape rates Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection including a turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation with a turbine blade (8c) and an all-wheel impeller water turbine and including various solar system escape speeds (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including a turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31Y) for hydroelectric power generation with a turbine blade (8c) and an all-wheel impeller water turbine and including various solar system escape speeds (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined rotor combustion unit (31X) for hydroelectric power generation with reduced friction loss by a full blade impeller water turbine, including various solar system escape speeds Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined rotor combustion unit (31Y) for reducing friction loss with all blade impeller water turbines and including various solar system escape speeds Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Combined turbine blade cross section (4B) capable of 910,000 times power, turbine blade (8c) and full blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, including various solar system escape rates Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined turbine blade cross section (4B) capable of 910,000 times work rate, turbine blade (8c), and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, including various solar system escape rates Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection including a turbine blade cross-section (4B) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation using a turbine blade (8c) and an all-wheel impeller water turbine, and including various solar system escape speeds (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including a turbine blade cross section (4B) capable of 910,000 times power and a combined engine combustion section (31Y) for hydroelectric power generation using a turbine blade (8c) and an all-wheel impeller water turbine, and including various solar system escape speeds (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Equipped with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a high temperature heating means (3B) combined engine combustion section (31X) for hydroelectric power generation with all blade impeller wheel turbines to escape various solar systems Combined engine injection part (79K) including speed Various energy storage cycle combined engine as various air suction injection drive devices.   Equipped with a turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a combined high temperature heating means (3B) combined engine combustion section (31Y) for hydroelectric power generation with all blade impeller wheel turbines to escape various solar systems Combined engine injection part (79K) including speed Various energy storage cycle combined engine as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection unit (79K) including various solar system escape speeds Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Combined engine injection unit (79K) including various solar system escape speeds Various energy storage cycle combined engines as various air suction injection drive devices.   Combined turbine blade cross section (4C) capable of 910,000 times power, turbine blade (8c) and full blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine, including various solar system escape rates Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined turbine blade cross-section (4C) capable of 910,000 times power and turbine blade (8c) and full blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, including various solar system escape rates Engine injection unit (79K) Various energy storage cycle coalescing engines as various air suction injection drive devices.   Combined engine injection including a turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation with a turbine blade (8c) and an all-wheel impeller water turbine and including various solar system escape speeds (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   Combined engine injection including a turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31Y) for hydroelectric power generation with a turbine blade (8c) and an all-wheel impeller water turbine and including various solar system escape speeds (79K) Various energy storage cycle coalescing engines as various air suction / injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined rotor combustion unit (31X) for hydroelectric power generation with reduced friction loss by a full blade impeller water turbine, including various solar system escape speeds Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and a combined rotor combustion unit (31Y) for reducing friction loss with all blade impeller water turbines and including various solar system escape speeds Combined engine injection unit (79K) Various energy storage cycle combined engines as various air suction injection drive devices.   Turbine blade cross-section (4B) capable of 910,000 times power, turbine blade (8c), and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by mercury power storage battery including recovery.   Turbine blade cross-section (4B) capable of 910,000 times work rate and turbine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation with vertical all-blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by mercury power storage battery including recovery.   Turbine blade cross section (4B) capable of 910,000 times power (4B) and a combined engine combustion section (31X) for hydroelectric power generation with all blade impeller water turbines, and various methane hydrate vaporization recovery using heat Various energy storage cycle coalescing engines, including various rotating output drive devices driven by mercury power storage batteries.   A turbine blade cross-section (4B) capable of 910,000 times power and a combined engine combustion section (31Y) for hydroelectric power generation using a turbine blade (8c) and an all-wheel impeller water turbine for various thermal methane hydrate vaporization recovery Various energy storage cycle coalescing engines, including various rotating output drive devices driven by mercury power storage batteries.   A turbine blade cross section (4C) capable of 910,000 times power (4C) and a turbine blade (8c) and heating blade high temperature means (3B) coalescence engine combustion section (31X) for hydroelectric power generation with a water turbine and various types of use of heat Various energy storage cycle coalescing engines as hydroelectric storage battery driven various rotational output drive equipment including methane hydrate vaporization recovery.   Turbine blade cross section (4C) capable of 910,000 times power (4C) and turbine blade (8c) and all blade impeller water turbine with heating high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation Various energy storage cycle coalescing engines as hydroelectric storage battery driven various rotational output drive equipment including methane hydrate vaporization recovery.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32X) for hydroelectric power generation by heating high temperature means (3B) with a vertical all blade water turbine, Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including various methane hydrate vaporization recovery.   A turbine blade cross section (4C) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32Y) for hydroelectric power generation with heating high temperature means (3B) with a vertical all blade water turbine, Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including various methane hydrate vaporization recovery.   Turbine blade cross-section (4C) capable of 910,000 times power, turbine blade (8c) and all blade combustion section (32X) for hydroelectric power generation with vertical all blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries including recovery.   Turbine blade cross-section (4C) capable of 910,000 times work rate, turbine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation with vertical all-blade water turbine Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries including recovery.   It has a turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation using a turbine blade (8c) and a full blade impeller water turbine, and is capable of vaporizing and recovering various methane hydrates using heat. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   A turbine blade cross-section (4C) capable of 910,000 times power and a combined engine combustion section (31Y) for hydroelectric power generation using a turbine blade (8c) and an all-wheel impeller water turbine for various thermal methane hydrate vaporization recovery Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   Turbine blade cross-section (4C) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation with reduced friction loss by a turbine blade (8c) and a full blade impeller water turbine. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries including vaporization recovery.   Turbine blade cross-section (4C) capable of 910,000 times power and a combined engine combustion section (31Y) that reduces friction loss with all blade impeller water turbines with a turbine blade turbine (8Y) and uses various heat methane hydrates Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries including vaporization recovery.   A turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine, and hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotational output drive devices driven by mercury power storage battery including injection.   Turbine blade cross-section (4B) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, and hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotational output drive devices driven by mercury power storage battery including injection.   A turbine blade cross section (4B) capable of 910,000 times power and a combined blade combustion unit (31X) for hydroelectric power generation using a turbine blade (8c) and a full blade impeller water turbine to inject hot water into various methane hydrates Various energy storage cycle coalescing engines, including various rotating output drive devices driven by mercury power storage batteries.   A turbine blade cross section (4B) capable of 910,000 times power and a combined blade combustion unit (31Y) for hydroelectric power generation with a turbine blade (8c) and a full blade impeller water turbine to inject hot water into various methane hydrates Various energy storage cycle coalescing engines, including various rotating output drive devices driven by mercury power storage batteries.   A turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature heating means (3B) coalescence engine combustion section (31X) for hydroelectric power generation using all blade impeller water turbines and various methane hydrides Various energy storage cycle coalescing engines as hydroelectric storage battery driven various rotational output drive equipment including hot water injection in the rate.   Various methane hydride with turbine blade cross section (4C) capable of 910,000 times power, turbine blade (8c) and all blade impeller water turbine heating high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation Various energy storage cycle coalescing engines as hydroelectric storage battery driven various rotational output drive equipment including hot water injection in the rate.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including hot water injection into methane hydrate.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including hot water injection into methane hydrate.   Turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine, and hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries including injection.   Turbine blade cross-section (4C) capable of 910,000 times power and turbine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, and hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries including injection.   A turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation with a turbine blade (8c) and an all-wheel impeller water turbine injects hot water into various methane hydrates. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   A turbine blade cross section (4C) capable of 910,000 times power and a combined blade combustion unit (31Y) for hydroelectric power generation with a turbine blade (8c) and a full blade impeller water turbine to inject hot water into various methane hydrates Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   A turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation with reduced friction loss by a turbine blade (8c) and a full blade impeller water turbine, and heat to various methane hydrates Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries including water injection.   A turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31Y) for hydroelectric power generation with reduced friction loss with a turbine blade (8c) and a turbine blade impeller water turbine to heat various methane hydrates Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries including water injection.   A turbine blade cross section (4B) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine, and hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotational output drive devices driven by mercury power storage battery including injection.   Turbine blade cross-section (4B) capable of 910,000 times power and a turbine blade (8c) and an all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine, and hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotational output drive devices driven by mercury power storage battery including injection.   A turbine blade cross section (4B) capable of 910,000 times power and a combined blade combustion unit (31X) for hydroelectric power generation using a turbine blade (8c) and a full blade impeller water turbine to inject hot water into various methane hydrates Various energy storage cycle coalescing engines, including various rotating output drive devices driven by mercury power storage batteries.   A turbine blade cross section (4B) capable of 910,000 times power and a combined blade combustion unit (31Y) for hydroelectric power generation with a turbine blade (8c) and a full blade impeller water turbine to inject hot water into various methane hydrates Various energy storage cycle coalescing engines, including various rotating output drive devices driven by mercury power storage batteries.   A turbine blade cross section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature heating means (3B) coalescence engine combustion section (31X) for hydroelectric power generation using all blade impeller water turbines and various methane hydrides Various energy storage cycle coalescing engines as hydroelectric storage battery driven various rotational output drive equipment including hot water injection in the rate.   Various methane hydride with turbine blade cross section (4C) capable of 910,000 times power, turbine blade (8c) and all blade impeller water turbine heating high temperature means (3B) combined engine combustion section (31Y) for hydroelectric power generation Various energy storage cycle coalescing engines as hydroelectric storage battery driven various rotational output drive equipment including hot water injection in the rate.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high-temperature means (3B) all-blade combustion section (32X) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including hot water injection into methane hydrate.   A turbine blade cross-section (4C) capable of 910,000 times power, a turbine blade (8c), and a high-temperature high temperature means (3B) all-blade combustion section (32Y) for hydroelectric power generation with a vertical all-blade water turbine. Various energy storage cycle coalescing engines as various rotating output drive devices driven by hydroelectric storage batteries including hot water injection into methane hydrate.   Turbine blade cross-section (4C) capable of 910,000 times power and a turbine blade (8c) and a full blade combustion section (32X) for hydroelectric power generation with a vertical all blade water turbine, and hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries including injection.   Turbine blade cross-section (4C) capable of 910,000 times power and turbine blade (8c) and all blade combustion section (32Y) for hydroelectric power generation with vertical all blade water turbine, and hot water in various methane hydrates Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries including injection.   A turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation with a turbine blade (8c) and an all-wheel impeller water turbine injects hot water into various methane hydrates. Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   A turbine blade cross section (4C) capable of 910,000 times power and a combined blade combustion unit (31Y) for hydroelectric power generation with a turbine blade (8c) and a full blade impeller water turbine to inject hot water into various methane hydrates Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries.   A turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31X) for hydroelectric power generation with reduced friction loss by a turbine blade (8c) and a full blade impeller water turbine, and heat to various methane hydrates Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries including water injection.   A turbine blade cross section (4C) capable of 910,000 times power and a combined engine combustion section (31Y) for hydroelectric power generation with reduced friction loss with a turbine blade (8c) and a turbine blade impeller water turbine to heat various methane hydrates Various energy storage cycle coalescing engines as various rotational output drive devices driven by hydroelectric storage batteries including water injection.   The turbine blade cross section (4D) all-blade combustion section (32X) vertical all-blade gas turbine (8A) is provided with a bearing (80) thrust bearing (80a) to drive and supply heat, electricity and cold. Various energy conservation cycle coalescence engine.   The turbine blade cross section (4D) all-blade combustion section (32Y) vertical all-blade gas turbine (8A) is provided with a bearing (80) thrust bearing (80a) to drive and supply heat, electricity and cold. Various energy conservation cycle coalescence engine.   Combined engine combustion section (31Y) full blade impeller gas turbine (8a) with turbine blade cross section (4D) provided with bearing (80) thrust bearing (80a) and various energy used as heat, electricity and cold supply equipment Conservation cycle coalescence organization.   Combined engine combustion section (31X) turbine blade cross section (4D) turbine blade cross section (4D) all-wheel impeller gas turbine (8a) with bearing (80) thrust bearing (80a) to drive and use various energy as heat, electricity and cold supply equipment Conservation cycle coalescence organization.   Heat and electricity to be driven by providing a bearing (80) thrust bearing (80a) and a cold energy recovery means (3C) to the all blade combustion section (32X) vertical blade gas turbine (8A) of the turbine blade cross section (4D) Various energy conservation cycle coalescing engine as a cold supply facility.   Heat and electricity to be driven by providing a bearing (80) thrust bearing (80a) and a cold energy recovery means (3C) in the all blade combustion section (32Y) vertical all blade gas turbine (8A) of the turbine blade cross section (4D) Various energy conservation cycle coalescing engine as a cold supply facility.   Combined engine combustion section (31Y) full blade impeller gas turbine (8a) of turbine blade cross section (4D) is provided with bearing (80) thrust bearing (80a) cold energy recovery means (3C) to drive heat, electricity and cold Various energy storage cycle coalescing engines as supply facilities.   Combined engine combustion section (31X) full blade impeller gas turbine (8a) with turbine blade cross section (4D) provided with bearing (80) thrust bearing (80a) cold energy recovery means (3C) to drive heat, electricity and cold energy Various energy storage cycle coalescing engines as supply facilities.   Heat and electricity to be driven by providing a bearing (80) thrust bearing (80a) and a cold recovery unit (103) in a turbine blade cross section (4D) all blade combustion part (32X) vertical all blade gas turbine (8A) Various energy conservation cycle coalescing engine as a cold supply facility.   Heat and electricity to be driven by providing a bearing (80) thrust bearing (80a) and a cold recovery unit (103) in the all blade combustion section (32Y) vertical all blade gas turbine (8A) of the turbine blade cross section (4D) Various energy conservation cycle coalescing engine as a cold supply facility.   Combined engine combustion section (31X) full blade impeller gas turbine (8a) of turbine blade cross section (4D) is provided with bearing (80) thrust bearing (80a) cold heat recovery device (103) to drive heat, electricity and cold heat Various energy storage cycle coalescing engines as supply facilities.   Combined engine combustion section (31Y) full blade impeller gas turbine (8a) of turbine blade cross section (4D) is provided with bearing (80) thrust bearing (80a) cold heat recovery device (103) to drive heat, electricity and cold Various energy storage cycle coalescing engines as supply facilities.   Heat that is driven by providing a bearing (80) thrust bearing (80a) and a cold recovery unit (103) (103) to the all-blade combustion section (32X) vertical all-blade gas turbine (8A) of the turbine blade cross section (4D) Combined with various energy storage cycle engines that use electricity and cold energy.   Heat that is driven by providing a bearing (80) thrust bearing (80a) and a cold recovery unit (103) (103) to the all-blade combustion section (32Y) vertical all-blade gas turbine (8A) of the turbine blade cross section (4D) Combined with various energy storage cycle engines that use electricity and cold energy.   Combined engine combustion section (31X) full blade impeller gas turbine (8a) with turbine blade cross section (4D) provided with bearing (80) thrust bearing (80a) cold heat recovery device (103) (103) and drive heat and electricity Combined with various energy conservation cycle facilities that use cold and hot energy.   Combined engine combustion section (31Y) full blade impeller gas turbine (8a) with turbine blade cross section (4D) provided with bearing (80) thrust bearing (80a) cold heat recovery device (103) (103) and drive heat and electricity Combined with various energy conservation cycle facilities that use cold and hot energy.   Combined engine combustion section (31X) full blade impeller gas turbine (8a) of turbine blade cross section (4D) is provided with bearing (80) thrust bearing (80a) cold heat recovery device (103) (103) and around 50 degrees Various energy storage cycle coalescing engines with heat, electricity and cold supply equipment driven by 300MPa combustion gas (49).   Combined engine combustion section (31Y) full rotor blade propeller gas turbine (8a) of turbine blade cross section (4D) is provided with bearing (80) thrust bearing (80a) cold heat recovery device (103) (103) and around 50 degrees 24- Various energy storage cycle coalescing engines with heat, electricity and cold supply equipment driven by 300MPa combustion gas (49).   A turbine blade cross section (4D) full rotor blade combustion section (32X) vertical all blade gas turbine (8A) is provided with a bearing (80) thrust bearing (80a) cold heat recovery device (103) (103) and around 50 degrees Various energy storage cycle coalescing engines with heat, electricity and cold supply equipment driven by 24-300MPa combustion gas (49).   A turbine blade cross section (4D) full blade combustion part (32Y) vertical all blade gas turbine (8A) is provided with a bearing (80) thrust bearing (80a) cold heat recovery device (103) (103) and around 50 degrees Various energy storage cycle coalescing engines with heat, electricity and cold supply equipment driven by 24-300MPa combustion gas (49).   Combined engine combustion section (31X) full blade impeller gas turbine (8a) of turbine blade cross section (4D) is provided with bearing (80) thrust bearing (80a) cold heat recovery device (103) (103) and around 80 degrees 24- Various energy storage cycle coalescing engines with heat, electricity and cold supply equipment driven by 300MPa combustion gas (49).   Combined engine combustion section (31Y) full rotor blade propeller gas turbine (8a) of turbine blade cross section (4D) is provided with bearing (80) thrust bearing (80a) cold heat recovery device (103) (103) and around 80 degrees 24- Various energy storage cycle coalescing engines with heat, electricity and cold supply equipment driven by 300MPa combustion gas (49).   A turbine blade cross section (4D) full rotor blade combustion section (32X) vertical all rotor blade gas turbine (8A) is provided with a bearing (80) thrust bearing (80a) cold heat recovery device (103) (103) and around 80 degrees Various energy storage cycle coalescing engines with heat, electricity and cold supply equipment driven by 24-300MPa combustion gas (49).   A turbine blade cross section (4D) full blade combustion section (32Y) vertical blade gas turbine (8A) is provided with a bearing (80) thrust bearing (80a) cold heat recovery device (103) (103) and around 80 degrees Various energy storage cycle coalescing engines with heat, electricity and cold supply equipment driven by 24-300MPa combustion gas (49).   A turbine blade cross section (4D) full rotor blade combustion section (32X) vertical all blade gas turbine (8A) is provided with a bearing (80) thrust bearing (80a) cold heat recovery device (103) (103) and around 100 degrees Various energy storage cycle coalescing engines with heat, electricity and cold supply equipment driven by 24-300MPa combustion gas (49).   A turbine blade cross section (4D) full rotor blade combustion section (32Y) vertical rotor blade gas turbine (8A) is provided with a bearing (80) thrust bearing (80a) cold heat recovery device (103) (103) and around 100 degrees Various energy storage cycle coalescing engines with heat, electricity and cold supply equipment driven by 24-300MPa combustion gas (49).   Combined engine combustion section (31X) full blade impeller gas turbine (8a) of turbine blade cross section (4D) is provided with bearing (80) thrust bearing (80a) cold heat recovery device (103) (103) and around 100 degrees 24- Various energy storage cycle coalescing engines with heat, electricity and cold supply equipment driven by 300MPa combustion gas (49).   A combined engine combustion section (31Y) full blade impeller gas turbine (8a) with a turbine blade cross section (4D) is provided with a bearing (80) thrust bearing (80a) and a cold heat recovery device (103) (103). Various energy storage cycle coalescing engines with heat, electricity and cold supply equipment driven by 300MPa combustion gas (49).   Combined engine combustion section (31X) high-temperature mercury (1d) of turbine blade cross section (4D) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for a 166,000 times work rate below the critical temperature. Various energy storage cycle coalescing engines with heat, electricity, and cold supply facilities that reduce the amount of heat consumed to approximately 1/72.   Combined engine combustion section (31Y) high-temperature mercury (1d) of turbine blade cross section (4D) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for a 166,000 times work rate below the critical temperature. Various energy storage cycle coalescing engines with heat, electricity, and cold supply facilities that reduce the amount of heat consumed to approximately 1/72.   The turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 166,000 times the workforce below the critical temperature. Various energy storage cycle coalescence engines with heat, electricity, and cold supply facilities that reduce the amount of heat consumed to approximately 1/72.   The turbine blade cross section (4D) full blade combustion part (32Y) high-temperature mercury (1d) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for a 166,000 times work efficiency below the critical temperature. Various energy storage cycle coalescence engines with heat, electricity, and cold supply facilities that reduce the amount of heat consumed to approximately 1/72.   High-pressure turbine drive provided with a bearing (80) thrust bearing (80a) aiming at a 166,000 times work efficiency at 1000 degrees Celsius or less for all rotor blade combustion section (32X) high-temperature mercury (1d) of turbine blade cross section (4D) Various energy storage cycle coalescence engines with heat, electricity, and cold supply facilities that reduce the amount of heat consumed to approximately 1/72.   High-pressure turbine drive provided with a bearing (80) thrust bearing (80a) aiming at a 166,000 times work rate at 1000 degrees Celsius or less for all rotor blade combustion section (32Y) high-temperature mercury (1d) of turbine blade cross section (4D) Various energy storage cycle coalescence engines with heat, electricity, and cold supply facilities that reduce the amount of heat consumed to approximately 1/72.   Combined engine combustion section (31X) high-temperature mercury (1d) of turbine blade cross section (4D) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 166,000 times power at 1000 degrees Celsius or less. Various energy storage cycle coalescence engines with heat, electricity, and cold supply facilities that reduce the amount of heat consumed to approximately 1/72.   Combined engine combustion section (31Y) high-temperature mercury (1d) of turbine blade cross section (4D) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 166,000 times power at 1000 degrees Celsius or less. Various energy storage cycle coalescence engines with heat, electricity, and cold supply facilities that reduce the amount of heat consumed to approximately 1/72.   Combined engine combustion section (31X) high-temperature mercury (1d) of turbine blade cross section (4D) is driven by a high pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 166,000 times power at 800 degrees Celsius or less. Various energy storage cycle coalescence engines with heat, electricity, and cold supply facilities that reduce the amount of heat consumed to approximately 1/72.   Combined engine combustion section (31Y) high-temperature mercury (1d) of turbine blade cross section (4D) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 166,000 times power at 800 degrees Celsius or less. Various energy storage cycle coalescence engines with heat, electricity, and cold supply facilities that reduce the amount of heat consumed to approximately 1/72.   High-pressure turbine drive provided with a bearing (80) thrust bearing (80a) aiming for a 166,000 times work at 800 degrees Celsius or less for all rotor blade combustion section (32X) high temperature mercury (1d) of turbine blade cross section (4D) Various energy storage cycle coalescence engines with heat, electricity, and cold supply facilities that reduce the amount of heat consumed to approximately 1/72.   High-pressure turbine drive provided with a bearing (80) thrust bearing (80a) aiming at a 166,000 times work rate at 800 degrees Celsius or less for all rotor blade combustion section (32Y) high temperature mercury (1d) of turbine blade cross section (4D) Various energy storage cycle coalescence engines with heat, electricity, and cold supply facilities that reduce the amount of heat consumed to approximately 1/72.   High-pressure turbine drive provided with a bearing (80) thrust bearing (80a) aiming at a 166,000 times work rate at 600 degrees Celsius or less for all blade combustion section (32X) high-temperature mercury (1d) of turbine blade cross section (4D) Various energy storage cycle coalescence engines with heat, electricity, and cold supply facilities that reduce the amount of heat consumed to approximately 1/72.   High-pressure turbine drive provided with a bearing (80) thrust bearing (80a) aiming at a work of 166,000 times at 600 degrees Celsius or less for all blade combustion section (32Y) high-temperature mercury (1d) of turbine blade cross section (4D) Various energy storage cycle coalescence engines with heat, electricity, and cold supply facilities that reduce the amount of heat consumed to approximately 1/72.   Combined engine combustion section (31X) high-temperature mercury (1d) of turbine blade cross section (4D) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 166,000 times power at 600 degrees Celsius or less. Various energy storage cycle coalescence engines with heat, electricity, and cold supply facilities that reduce the amount of heat consumed to approximately 1/72.   Combined engine combustion section (31Y) high-temperature mercury (1d) of turbine blade cross section (4D) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 166,000 times power at 600 degrees Celsius or less. Various energy storage cycle coalescence engines with heat, electricity, and cold supply facilities that reduce the amount of heat consumed to approximately 1/72.   Combined engine combustion section (31X) high-temperature water (52b) of turbine blade cross section (4D) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 910,000 times lower than critical temperature. Various energy storage cycle coalescing engines that use heat, electricity, and cold supply equipment to reduce the power to approximately 1/539.   Combined engine combustion section (31Y) high-temperature water (52b) of turbine blade cross section (4D) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 910,000 times lower than the critical temperature and consumes heat. Various energy storage cycle coalescing engines that use heat, electricity, and cold supply equipment to reduce the power to approximately 1/539.   The turbine blade cross section (4D) full blade combustion part (32X) high-temperature water (52b) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 910,000 times lower than the critical temperature. Various energy storage cycle coalescing engines with heat, electricity, and cold supply facilities that reduce the amount of heat to approximately 1/539.   The turbine blade cross section (4D) full blade combustion part (32Y) high-temperature water (52b) is consumed by driving a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 910,000 times lower than the critical temperature. Various energy storage cycle coalescing engines with heat, electricity, and cold supply facilities that reduce the amount of heat to approximately 1/539.   The turbine blade cross section (4D) full blade combustion part (32X) high-temperature water (52b) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for a 910,000-fold power, and the amount of heat consumed is approximately / Energy conservation cycle coalescence engine with heat / electricity / cold heat supply facilities to 539 etc.   The turbine blade cross section (4D) full blade combustion section (32Y) high temperature water (52b) is driven by a high pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for 910,000 times the power, and the heat consumption is reduced to about 1 / Energy conservation cycle coalescence engine with heat / electricity / cold heat supply facilities to 539 etc.   Combined engine combustion section (31X) high temperature water (52b) of turbine blade cross section (4D) is driven by a high pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for 910,000 times power, and heat consumption is reduced to about 1 / Various energy storage cycle coalescence engine with heat, electricity and cold power supply facilities to 539 etc.   Combined engine combustion section (31Y) high temperature water (52b) of turbine blade cross section (4D) is driven by a high pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for 910,000 times power, and heat consumption is reduced to about 1 / Various energy storage cycle coalescence engine with heat, electricity and cold power supply facilities to 539 etc.   Combined engine combustion section (31X) high temperature water (52b) with turbine blade cross section (4D) driven by high pressure turbine with bearing (80) thrust bearing (80a) aiming for 910,000 times power, and output at the same pressure at atmospheric pressure Various energy storage cycle coalescence engine with heat, electricity, and cold supply facilities that make steam-driven 1,700 times the weight of m / sec.   Combined combustion section (31Y) of turbine blade cross section (4D) with high temperature water (52b), bearing (80) thrust bearing (80a) aiming for 910,000 times power, drive high pressure turbine and output atmospheric pressure at same speed Various energy storage cycle coalescence engine with heat, electricity, and cold supply facilities that make steam-driven 1,700 times the weight of m / sec.   Turbine blade cross section (4D) full rotor blade combustion part (32X) high temperature water (52b) driven by high pressure turbine with bearing (80) thrust bearing (80a) aiming for 910,000 times power Various energy storage cycle coalescence engine with heat, electricity, and cold supply facilities that make 1700 times the weight of steam driven m / sec.   Turbine blade cross section (4D) full rotor blade combustion part (32Y) high temperature water (52b) bearing 910,000 times power target bearing (80) thrust bearing (80a) driven high pressure turbine driven at atmospheric pressure and same speed output Various energy storage cycle coalescence engine with heat, electricity, and cold supply facilities that make 1700 times the weight of steam driven m / sec.   Turbine blade cross section (4D) full rotor blade combustion part (32X) high temperature mercury (1d) 16650 times work rate bearing (80) thrust bearing (80a) provided high pressure turbine drive Various energy storage cycle coalescing engines with heat, electricity, and cold supply equipment that make the speed output 23,000 times the weight of steam driven by steam, m / sec.   Turbine blade cross section (4D) full rotor blade combustion part (32Y) high temperature mercury (1d) bearing with a target of 166,000 times work rate (80) thrust bearing (80a) driven high pressure turbine driven at the same atmospheric pressure Various energy storage cycle coalescing engines with heat, electricity, and cold supply equipment that make the speed output 23,000 times the weight of steam driven by steam, m / sec.   Turbine blade cross section (4D) coalescence engine combustion part (31X) high temperature mercury (1d) bearing with a target of 166,000 times power (80) thrust bearing (80a) is driven by a high pressure turbine driven at the same atmospheric pressure Various energy storage cycle coalescence engine with heat, electricity, and cold supply facilities that output 23,000 times the weight of steam driven by steam, m / sec.   Turbine blade cross section (4D) coalescence engine combustion section (31Y) high temperature mercury (1d) bearing with a target of 166,000 times power (80) thrust bearing (80a) driven by high pressure turbine driven at same atmospheric pressure Various energy storage cycle coalescence engine with heat, electricity, and cold supply facilities that output 23,000 times the weight of steam driven by steam, m / sec.   Turbine blade cross section (4D) coalescence engine combustion part (31X) high temperature mercury (1d) bearing with a target of 166,000 times power (80) thrust bearing (80a) is driven by a high pressure turbine driven at the same atmospheric pressure Various energy storage cycle coalescing engines with an output of 23,000 times the weight of steam driven by steam, m / second, and heat / electricity / cold heat supply facility in the vicinity of 1/72 of heat consumption.   Turbine blade cross section (4D) coalescence engine combustion section (31Y) high temperature mercury (1d) bearing with a target of 166,000 times power (80) thrust bearing (80a) driven by high pressure turbine driven at same atmospheric pressure Various energy storage cycle coalescing engines with an output of 23,000 times the weight of steam driven by steam, m / second, and heat / electricity / cold heat supply facility in the vicinity of 1/72 of heat consumption.   Turbine blade cross section (4D) full rotor blade combustion part (32X) high temperature mercury (1d) 16650 times work rate bearing (80) thrust bearing (80a) provided high pressure turbine drive Various energy storage cycle coalescing engines with a speed output of 23,000 times the weight of steam driven by steam, m / second, and heat / electricity / cold heat supply facility near 1/72 of heat consumption.   Turbine blade cross section (4D) full rotor blade combustion part (32Y) high temperature mercury (1d) bearing with a target of 166,000 times work rate (80) thrust bearing (80a) driven high pressure turbine driven at the same atmospheric pressure Various energy storage cycle coalescing engines with a speed output of 23,000 times the weight of steam driven by steam, m / second, and heat / electricity / cold heat supply facility near 1/72 of heat consumption.   Turbine blade cross section (4D) full rotor blade combustion part (32X) high temperature mercury (1d) 16650 times work rate bearing (80) thrust bearing (80a) provided high pressure turbine drive Various energy conservation cycle coalescing engines with a speed output of 23,000 times the weight of steam driven by m / sec and a heat consumption of 1/72.   Turbine blade cross section (4D) full rotor blade combustion part (32Y) high temperature mercury (1d) bearing with a target of 166,000 times work rate (80) thrust bearing (80a) driven high pressure turbine driven at the same atmospheric pressure Various energy conservation cycle coalescing engines with a speed output of 23,000 times the weight of steam driven by m / sec and a heat consumption of 1/72.   Turbine blade cross section (4D) coalescence engine combustion part (31X) high temperature mercury (1d) bearing with a target of 166,000 times power (80) thrust bearing (80a) is driven by a high pressure turbine driven at the same atmospheric pressure Various energy storage cycle coalescing engines with an output of 23,000 times the weight of steam driven m / s and water consumption of 1/72.   Turbine blade cross section (4D) coalescence engine combustion section (31Y) high temperature mercury (1d) bearing with a target of 166,000 times power (80) thrust bearing (80a) driven by high pressure turbine driven at same atmospheric pressure Various energy storage cycle coalescing engines with an output of 23,000 times the weight of steam driven m / s and water consumption of 1/72.   Turbine blade cross section (4D) coalescence engine combustion part (31X) high temperature mercury (1d) bearing with a target of 166,000 times power (80) thrust bearing (80a) is driven by a high pressure turbine driven at the same atmospheric pressure Various energy conservation cycle coalescing engines with various outputs of 23,000 times the weight of steam driven by steam and 1/72 of heat consumption.   Turbine blade cross section (4D) coalescence engine combustion section (31Y) high temperature mercury (1d) bearing with a target of 166,000 times power (80) thrust bearing (80a) driven by high pressure turbine driven at same atmospheric pressure Various energy conservation cycle coalescing engines with various outputs of 23,000 times the weight of steam driven by steam and 1/72 of heat consumption.   Turbine blade cross section (4D) full rotor blade combustion part (32X) high temperature mercury (1d) 16650 times work rate bearing (80) thrust bearing (80a) provided high pressure turbine drive Various energy storage cycle coalescing engines that make the speed output 23,000 times kg weight m / sec of steam drive and various airplanes equipped with heat consumption 1/72 vicinity.   Turbine blade cross section (4D) full rotor blade combustion part (32Y) high temperature mercury (1d) bearing with a target of 166,000 times work rate (80) thrust bearing (80a) driven high pressure turbine driven at the same atmospheric pressure Various energy storage cycle coalescing engines that make the speed output 23,000 times kg weight m / sec of steam drive and various airplanes equipped with heat consumption 1/72 vicinity.   Turbine blade cross section (4D) full rotor blade combustion part (32X) high temperature water (52b) driven by high pressure turbine with bearing (80) thrust bearing (80a) aiming for 910,000 times power Various energy conservation cycle coalescence engines that make various airplanes equipped with 1700 times kg weight m / second of steam drive and heat consumption 1/539 vicinity.   Turbine blade cross section (4D) full rotor blade combustion part (32Y) high temperature water (52b) bearing 910,000 times power target bearing (80) thrust bearing (80a) driven high pressure turbine driven at atmospheric pressure and same speed output Various energy conservation cycle coalescence engines that make various airplanes equipped with 1700 times kg weight m / second of steam drive and heat consumption 1/539 vicinity.   Combined engine combustion section (31X) high temperature water (52b) with turbine blade cross section (4D) driven by high pressure turbine with bearing (80) thrust bearing (80a) aiming for 910,000 times power, and output at the same pressure at atmospheric pressure Steam-driven 1700 times kg weight m / sec. Heat energy consumption 1/539 vicinity Various airplanes equipped with various energy storage cycle coalescing engines.   Combined combustion section (31Y) of turbine blade cross section (4D) with high temperature water (52b), bearing (80) thrust bearing (80a) aiming for 910,000 times power, drive high pressure turbine and output atmospheric pressure at same speed Steam-driven 1700 times kg weight m / sec. Heat energy consumption 1/539 vicinity Various airplanes equipped with various energy storage cycle coalescing engines.   Combined engine combustion section (31X) high temperature water (52b) with turbine blade cross section (4D) driven by high pressure turbine with bearing (80) thrust bearing (80a) aiming for 910,000 times power, and output at the same pressure at atmospheric pressure Steam-driven 1700 times kg weight m / sec and heat energy consumption 1/539 neighborhood Various energy conservation cycle coalescing engines that make various ships.   Combined combustion section (31Y) of turbine blade cross section (4D) with high temperature water (52b), bearing (80) thrust bearing (80a) aiming for 910,000 times power, drive high pressure turbine and output atmospheric pressure at same speed Steam-driven 1700 times kg weight m / sec and heat energy consumption 1/539 neighborhood Various energy conservation cycle coalescing engines that make various ships.   Turbine blade cross section (4D) full rotor blade combustion part (32X) high temperature water (52b) driven by high pressure turbine with bearing (80) thrust bearing (80a) aiming for 910,000 times power Various energy conservation cycle coalescing engines that make the steam-driven 1700 times kg weight m / second and heat consumption 1/539 vicinity.   Turbine blade cross section (4D) full rotor blade combustion part (32Y) high temperature water (52b) bearing 910,000 times power target bearing (80) thrust bearing (80a) driven high pressure turbine driven at atmospheric pressure and same speed output Various energy conservation cycle coalescing engines that make the steam-driven 1700 times kg weight m / second and heat consumption 1/539 vicinity.   Turbine blade cross section (4D) full rotor blade combustion part (32X) high temperature water (52b) driven by high pressure turbine with bearing (80) thrust bearing (80a) aiming for 910,000 times power Various energy storage cycle coalescence engines that make various heat, electricity and cold supply facilities in the vicinity of steam driven 1700 times kg weight m / sec and heat consumption 1/539.   Turbine blade cross section (4D) full rotor blade combustion part (32Y) high temperature water (52b) bearing 910,000 times power target bearing (80) thrust bearing (80a) driven high pressure turbine driven at atmospheric pressure and same speed output Various energy storage cycle coalescence engines that make various heat, electricity and cold supply facilities in the vicinity of steam driven 1700 times kg weight m / sec and heat consumption 1/539.   Combined engine combustion section (31X) high temperature water (52b) with turbine blade cross section (4D) driven by high pressure turbine with bearing (80) thrust bearing (80a) aiming for 910,000 times power, and output at the same pressure at atmospheric pressure Steam-driven 1700 times kg weight m / sec. Heat consumption 1/539. Various energy conservation cycle coalescing engines for various heat, electricity and cold supply facilities.   Combined combustion section (31Y) of turbine blade cross section (4D) with high temperature water (52b), bearing (80) thrust bearing (80a) aiming for 910,000 times power, drive high pressure turbine and output atmospheric pressure at same speed Steam-driven 1700 times kg weight m / sec. Heat consumption 1/539. Various energy conservation cycle coalescing engines for various heat, electricity and cold supply facilities.   Combined engine combustion section (31X) high-temperature mercury (1d) of turbine blade cross section (4D) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for a 166,000 times work rate below the critical temperature. Various energy storage cycle coalescing engines with a heat consumption of approximately 1/72, 23,000 times the weight of steam driven kg weight m / second, etc. to provide various heat, electricity and cold supply facilities.   Combined engine combustion section (31Y) high-temperature mercury (1d) of turbine blade cross section (4D) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for a 166,000 times work rate below the critical temperature. Various energy storage cycle coalescing engines with a heat consumption of approximately 1/72, 23,000 times the weight of steam driven kg weight m / second, etc. to provide various heat, electricity and cold supply facilities.   The turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 166,000 times the workforce below the critical temperature. Various energy storage cycle coalescing engines with a heat supply of approximately 1/72, 23,000 times the weight of steam driven by kg weight m / sec.   The turbine blade cross section (4D) full blade combustion part (32Y) high-temperature mercury (1d) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for a 166,000 times work efficiency below the critical temperature. Various energy storage cycle coalescing engines with a heat supply of approximately 1/72, 23,000 times the weight of steam driven by kg weight m / sec.   The turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 166,000 times the workforce below the critical temperature. Various energy storage cycle coalescing engines with a heat consumption of approximately 1/72, 23,000 times the weight of steam driven kg weight m / sec.   The turbine blade cross section (4D) full blade combustion part (32Y) high-temperature mercury (1d) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for a 166,000 times work efficiency below the critical temperature. Various energy storage cycle coalescing engines with a heat consumption of approximately 1/72, 23,000 times the weight of steam driven kg weight m / sec.   Combined engine combustion section (31X) high-temperature mercury (1d) of turbine blade cross section (4D) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for a 166,000 times work rate below the critical temperature. Various energy conservation cycle coalescing engines with a heat consumption of approximately 1/72, 23,000 times the weight of steam driven kg weight m / second, etc. to make various ships.   Combined engine combustion section (31Y) high-temperature mercury (1d) of turbine blade cross section (4D) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for a 166,000 times work rate below the critical temperature. Various energy conservation cycle coalescing engines with a heat consumption of approximately 1/72, 23,000 times the weight of steam driven kg weight m / second, etc. to make various ships.   Combined engine combustion section (31X) high-temperature mercury (1d) of turbine blade cross section (4D) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for a 166,000 times work rate below the critical temperature. Various energy storage cycle coalescing engines with a heat consumption of approximately 1/72, 23,000 times the weight of steam driven kg weight m / second, etc. to make various airplanes.   Combined engine combustion section (31Y) high-temperature mercury (1d) of turbine blade cross section (4D) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for a 166,000 times work rate below the critical temperature. Various energy storage cycle coalescing engines with a heat consumption of approximately 1/72, 23,000 times the weight of steam driven kg weight m / second, etc. to make various airplanes.   The turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 166,000 times the workforce below the critical temperature. Various energy storage cycle coalescing engines with a heat consumption of approximately 1/72, 23,000 times the weight of steam driven kg weight m / sec.   The turbine blade cross section (4D) full blade combustion part (32Y) high-temperature mercury (1d) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for a 166,000 times work efficiency below the critical temperature. Various energy storage cycle coalescing engines with a heat consumption of approximately 1/72, 23,000 times the weight of steam driven kg weight m / sec.   High-pressure turbine drive provided with a bearing (80) thrust bearing (80a) aiming at a 166,000 times work efficiency at 1000 degrees Celsius or less for all rotor blade combustion section (32X) high-temperature mercury (1d) of turbine blade cross section (4D) Various energy storage cycle coalescing engines that make various types of airplanes with a heat consumption of approximately 1/72 and steam driven 23,000 times kg weight m / sec.   High-pressure turbine drive provided with a bearing (80) thrust bearing (80a) aiming at a 166,000 times work rate at 1000 degrees Celsius or less for all rotor blade combustion section (32Y) high-temperature mercury (1d) of turbine blade cross section (4D) Various energy storage cycle coalescing engines that make various types of airplanes with a heat consumption of approximately 1/72 and steam driven 23,000 times kg weight m / sec.   Combined engine combustion section (31X) high-temperature mercury (1d) of turbine blade cross section (4D) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 166,000 times power at 1000 degrees Celsius or less. Various energy storage cycle coalescing engines that make various types of airplanes with a heat consumption of approximately 1/72, 23,000 times the weight of steam driven kg weight m / sec.   Combined engine combustion section (31Y) high-temperature mercury (1d) of turbine blade cross section (4D) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 166,000 times power at 1000 degrees Celsius or less. Various energy storage cycle coalescing engines that make various types of airplanes with a heat consumption of approximately 1/72, 23,000 times the weight of steam driven kg weight m / sec.   Combined engine combustion section (31X) high-temperature mercury (1d) of turbine blade cross section (4D) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 166,000 times power at 1000 degrees Celsius or less. Various energy storage cycle coalescing engines that make various kinds of ships with a heat consumption of approximately 1/72, 23,000 times the weight of steam driven kg weight m / sec.   Combined engine combustion section (31Y) high-temperature mercury (1d) of turbine blade cross section (4D) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 166,000 times power at 1000 degrees Celsius or less. Various energy storage cycle coalescing engines that make various kinds of ships with a heat consumption of approximately 1/72, 23,000 times the weight of steam driven kg weight m / sec.   High-pressure turbine drive provided with a bearing (80) thrust bearing (80a) aiming at a 166,000 times work efficiency at 1000 degrees Celsius or less for all rotor blade combustion section (32X) high-temperature mercury (1d) of turbine blade cross section (4D) Various energy storage cycle coalescing engines with various heat consumption of approximately 1/72 and steam driven 23,000 times kg weight m / sec.   High-pressure turbine drive provided with a bearing (80) thrust bearing (80a) aiming at a 166,000 times work rate at 1000 degrees Celsius or less for all rotor blade combustion section (32Y) high-temperature mercury (1d) of turbine blade cross section (4D) Various energy storage cycle coalescing engines with various heat consumption of approximately 1/72 and steam driven 23,000 times kg weight m / sec.   High-pressure turbine drive provided with a bearing (80) thrust bearing (80a) aiming at a 166,000 times work efficiency at 1000 degrees Celsius or less for all rotor blade combustion section (32X) high-temperature mercury (1d) of turbine blade cross section (4D) Various energy storage cycle coalescence engines that use various heat, electricity and cold supply facilities, such as heat consumption of approximately 1/72, steam driven 23,000 times kg weight m / sec.   High-pressure turbine drive provided with a bearing (80) thrust bearing (80a) aiming at a 166,000 times work rate at 1000 degrees Celsius or less for all rotor blade combustion section (32Y) high-temperature mercury (1d) of turbine blade cross section (4D) Various energy storage cycle coalescence engines that use various heat, electricity and cold supply facilities, such as heat consumption of approximately 1/72, steam driven 23,000 times kg weight m / sec.   Combined engine combustion section (31X) high-temperature mercury (1d) of turbine blade cross section (4D) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 166,000 times power at 1000 degrees Celsius or less. Various energy storage cycle coalescence engines that use various heat, electricity, and cold supply facilities such as approximately 1/72 of heat consumption and 23,000 times the weight of steam driven m / s.   Combined engine combustion section (31Y) high-temperature mercury (1d) of turbine blade cross section (4D) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 166,000 times power at 1000 degrees Celsius or less. Various energy storage cycle coalescence engines that use various heat, electricity, and cold supply facilities such as approximately 1/72 of heat consumption and 23,000 times the weight of steam driven m / s.   Combined engine combustion section (31X) high-temperature mercury (1d) of turbine blade cross section (4D) is driven by a high pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 166,000 times power at 800 degrees Celsius or less. Various energy storage cycle coalescence engines that use various heat, electricity, and cold supply facilities such as approximately 1/72 of heat consumption and 23,000 times the weight of steam driven m / s.   Combined engine combustion section (31Y) high-temperature mercury (1d) of turbine blade cross section (4D) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 166,000 times power at 800 degrees Celsius or less. Various energy storage cycle coalescence engines that use various heat, electricity, and cold supply facilities such as approximately 1/72 of heat consumption and 23,000 times the weight of steam driven m / s.   High-pressure turbine drive provided with a bearing (80) thrust bearing (80a) aiming for a 166,000 times work at 800 degrees Celsius or less for all rotor blade combustion section (32X) high temperature mercury (1d) of turbine blade cross section (4D) Various energy storage cycle coalescence engines that use various heat, electricity and cold supply facilities, such as heat consumption of approximately 1/72, steam driven 23,000 times kg weight m / sec.   High-pressure turbine drive provided with a bearing (80) thrust bearing (80a) aiming at a 166,000 times work rate at 800 degrees Celsius or less for all rotor blade combustion section (32Y) high temperature mercury (1d) of turbine blade cross section (4D) Various energy storage cycle coalescence engines that use various heat, electricity and cold supply facilities, such as heat consumption of approximately 1/72, steam driven 23,000 times kg weight m / sec.   High-pressure turbine drive provided with a bearing (80) thrust bearing (80a) aiming for a 166,000 times work at 800 degrees Celsius or less for all rotor blade combustion section (32X) high temperature mercury (1d) of turbine blade cross section (4D) Various energy storage cycle coalescing engines with various heat consumption of approximately 1/72 and steam driven 23,000 times kg weight m / sec.   High-pressure turbine drive provided with a bearing (80) thrust bearing (80a) aiming at a 166,000 times work rate at 800 degrees Celsius or less for all rotor blade combustion section (32Y) high temperature mercury (1d) of turbine blade cross section (4D) Various energy storage cycle coalescing engines with various heat consumption of approximately 1/72 and steam driven 23,000 times kg weight m / sec.   Combined engine combustion section (31X) high-temperature mercury (1d) of turbine blade cross section (4D) is driven by a high pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 166,000 times power at 800 degrees Celsius or less. Various energy storage cycle coalescing engines that make various kinds of ships with a heat consumption of approximately 1/72, 23,000 times the weight of steam driven kg weight m / sec.   Combined engine combustion section (31Y) high-temperature mercury (1d) of turbine blade cross section (4D) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 166,000 times power at 800 degrees Celsius or less. Various energy storage cycle coalescing engines that make various kinds of ships with a heat consumption of approximately 1/72, 23,000 times the weight of steam driven kg weight m / sec.   Combined engine combustion section (31X) high-temperature mercury (1d) of turbine blade cross section (4D) is driven by a high pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 166,000 times power at 800 degrees Celsius or less. Various energy storage cycle coalescing engines that make various types of airplanes with a heat consumption of approximately 1/72, 23,000 times the weight of steam driven kg weight m / sec.   Combined engine combustion section (31Y) high-temperature mercury (1d) of turbine blade cross section (4D) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 166,000 times power at 800 degrees Celsius or less. Various energy storage cycle coalescing engines that make various types of airplanes with a heat consumption of approximately 1/72, 23,000 times the weight of steam driven kg weight m / sec.   High-pressure turbine drive provided with a bearing (80) thrust bearing (80a) aiming for a 166,000 times work at 800 degrees Celsius or less for all rotor blade combustion section (32X) high temperature mercury (1d) of turbine blade cross section (4D) Various energy storage cycle coalescing engines that make various types of airplanes with a heat consumption of approximately 1/72 and steam driven 23,000 times kg weight m / sec.   High-pressure turbine drive provided with a bearing (80) thrust bearing (80a) aiming at a 166,000 times work rate at 800 degrees Celsius or less for all rotor blade combustion section (32Y) high temperature mercury (1d) of turbine blade cross section (4D) Various energy storage cycle coalescing engines that make various types of airplanes with a heat consumption of approximately 1/72 and steam driven 23,000 times kg weight m / sec.   High-pressure turbine drive provided with a bearing (80) thrust bearing (80a) aiming at a 166,000 times work rate at 600 degrees Celsius or less for all blade combustion section (32X) high-temperature mercury (1d) of turbine blade cross section (4D) Various energy storage cycle coalescing engines that make various types of airplanes with a heat consumption of approximately 1/72 and steam driven 23,000 times kg weight m / sec.   High-pressure turbine drive provided with a bearing (80) thrust bearing (80a) aiming at a work of 166,000 times at 600 degrees Celsius or less for all blade combustion section (32Y) high-temperature mercury (1d) of turbine blade cross section (4D) Various energy storage cycle coalescing engines that make various types of airplanes with a heat consumption of approximately 1/72 and steam driven 23,000 times kg weight m / sec.   Combined engine combustion section (31X) high-temperature mercury (1d) of turbine blade cross section (4D) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 166,000 times power at 600 degrees Celsius or less. Various energy storage cycle coalescing engines that make various types of airplanes with a heat consumption of approximately 1/72, 23,000 times the weight of steam driven kg weight m / sec.   Combined engine combustion section (31Y) high-temperature mercury (1d) of turbine blade cross section (4D) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 166,000 times power at 600 degrees Celsius or less. Various energy storage cycle coalescing engines that make various types of airplanes with a heat consumption of approximately 1/72, 23,000 times the weight of steam driven kg weight m / sec.   Combined engine combustion section (31X) high-temperature mercury (1d) of turbine blade cross section (4D) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 166,000 times power at 600 degrees Celsius or less. Various energy storage cycle coalescing engines that make various kinds of ships with a heat consumption of approximately 1/72, 23,000 times the weight of steam driven kg weight m / sec.   Combined engine combustion section (31Y) high-temperature mercury (1d) of turbine blade cross section (4D) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 166,000 times power at 600 degrees Celsius or less. Various energy storage cycle coalescing engines that make various kinds of ships with a heat consumption of approximately 1/72, 23,000 times the weight of steam driven kg weight m / sec.   High-pressure turbine drive provided with a bearing (80) thrust bearing (80a) aiming at a 166,000 times work rate at 600 degrees Celsius or less for all blade combustion section (32X) high-temperature mercury (1d) of turbine blade cross section (4D) Various energy storage cycle coalescing engines with various heat consumption of approximately 1/72 and steam driven 23,000 times kg weight m / sec.   High-pressure turbine drive provided with a bearing (80) thrust bearing (80a) aiming at a work of 166,000 times at 600 degrees Celsius or less for all blade combustion section (32Y) high-temperature mercury (1d) of turbine blade cross section (4D) Various energy storage cycle coalescing engines with various heat consumption of approximately 1/72 and steam driven 23,000 times kg weight m / sec.   High-pressure turbine drive provided with a bearing (80) thrust bearing (80a) aiming at a 166,000 times work rate at 600 degrees Celsius or less for all blade combustion section (32X) high-temperature mercury (1d) of turbine blade cross section (4D) Various energy storage cycle coalescence engines that use various heat, electricity and cold supply facilities, such as heat consumption of approximately 1/72, steam driven 23,000 times kg weight m / sec.   High-pressure turbine drive provided with a bearing (80) thrust bearing (80a) aiming at a work of 166,000 times at 600 degrees Celsius or less for all blade combustion section (32Y) high-temperature mercury (1d) of turbine blade cross section (4D) Various energy storage cycle coalescence engines that use various heat, electricity and cold supply facilities, such as heat consumption of approximately 1/72, steam driven 23,000 times kg weight m / sec.   Combined engine combustion section (31X) high-temperature mercury (1d) of turbine blade cross section (4D) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 166,000 times power at 600 degrees Celsius or less. Various energy storage cycle coalescence engines that use various heat, electricity, and cold supply facilities such as approximately 1/72 of heat consumption and 23,000 times the weight of steam driven m / s.   Combined engine combustion section (31Y) high-temperature mercury (1d) of turbine blade cross section (4D) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 166,000 times power at 600 degrees Celsius or less. Various energy storage cycle coalescence engines that use various heat, electricity, and cold supply facilities such as approximately 1/72 of heat consumption and 23,000 times the weight of steam driven m / s.   Combined engine combustion section (31X) high-temperature water (52b) of turbine blade cross section (4D) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 910,000 times lower than critical temperature. Various energy storage cycle coalescing engines that make various heat, electricity and cold supply facilities such as 1/539 times steam-driven 1700 times kg weight m / sec.   Combined engine combustion section (31Y) high-temperature water (52b) of turbine blade cross section (4D) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 910,000 times lower than the critical temperature and consumes heat. Various energy storage cycle coalescing engines that make various heat, electricity and cold supply facilities such as 1/539 times steam-driven 1700 times kg weight m / sec.   The turbine blade cross section (4D) full blade combustion part (32X) high-temperature water (52b) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 910,000 times lower than the critical temperature. Various energy storage cycle coalescing engines that use various heat, electricity, and cold supply facilities such as 1/539 times the weight of steam and 1700 times the weight of steam, m / sec.   The turbine blade cross section (4D) full blade combustion part (32Y) high-temperature water (52b) is consumed by driving a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 910,000 times lower than the critical temperature. Various energy storage cycle coalescing engines that use various heat, electricity, and cold supply facilities such as 1/539 times the weight of steam and 1700 times the weight of steam, m / sec.   The turbine blade cross section (4D) full blade combustion part (32X) high-temperature water (52b) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 910,000 times lower than the critical temperature. Various energy conservation cycle coalescing engines that make various kinds of ships with a heat quantity of approximately 1/539, 1700 times the weight of steam driven kg weight m / sec.   The turbine blade cross section (4D) full blade combustion part (32Y) high-temperature water (52b) is consumed by driving a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 910,000 times lower than the critical temperature. Various energy conservation cycle coalescing engines that make various kinds of ships with a heat quantity of approximately 1/539, 1700 times the weight of steam driven kg weight m / sec.   Combined engine combustion section (31X) high-temperature water (52b) of turbine blade cross section (4D) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 910,000 times lower than critical temperature. Various energy storage cycle coalescing engines that make various boats such as 1/539 times steam-driven 1700 times kg weight m / sec.   Combined engine combustion section (31Y) high-temperature water (52b) of turbine blade cross section (4D) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 910,000 times lower than the critical temperature and consumes heat. Various energy storage cycle coalescing engines that make various boats such as 1/539 times steam-driven 1700 times kg weight m / sec.   Combined engine combustion section (31X) high-temperature water (52b) of turbine blade cross section (4D) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 910,000 times lower than critical temperature. Various energy storage cycle coalescing engines that make various aircraft such as 1/539 times steam-driven 1700 times kg weight m / sec.   Combined engine combustion section (31Y) high-temperature water (52b) of turbine blade cross section (4D) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 910,000 times lower than the critical temperature and consumes heat. Various energy storage cycle coalescing engines that make various aircraft such as 1/539 times steam-driven 1700 times kg weight m / sec.   The turbine blade cross section (4D) full blade combustion part (32X) high-temperature water (52b) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 910,000 times lower than the critical temperature. Various energy storage cycle coalescing engines that make various kinds of airplanes with a heat quantity of approximately 1/539, 1700 times the weight of steam driven kg weight m / sec.   The turbine blade cross section (4D) full blade combustion part (32Y) high-temperature water (52b) is consumed by driving a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aimed at 910,000 times lower than the critical temperature. Various energy storage cycle coalescing engines that make various kinds of airplanes with a heat quantity of approximately 1/539, 1700 times the weight of steam driven kg weight m / sec.   The turbine blade cross section (4D) full blade combustion part (32X) high-temperature water (52b) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for a 910,000-fold work rate, and the amount of heat consumed is approximately 1 / 539 ・ Various energy storage cycle coalescing engines to make various airplanes such as 1700 times kg weight m / sec of steam drive.   The turbine blade cross section (4D) full blade combustion section (32Y) high temperature water (52b) is driven by a high pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for 910,000 times the power, and the heat consumption is reduced to about 1 / 539 ・ Various energy storage cycle coalescing engines to make various airplanes such as 1700 times kg weight m / sec of steam drive.   Combined engine combustion section (31X) high temperature water (52b) of turbine blade cross section (4D) is driven by a high pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for 910,000 times power, and heat consumption is reduced to about 1 / 539 ・ Various energy storage cycle coalescence engine to make various airplanes such as 1700 times kg weight m / second of steam drive.   Combined engine combustion section (31Y) high temperature water (52b) of turbine blade cross section (4D) is driven by a high pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for 910,000 times power, and heat consumption is reduced to about 1 / 539 ・ Various energy storage cycle coalescence engine to make various airplanes such as 1700 times kg weight m / second of steam drive.   Combined engine combustion section (31X) high temperature water (52b) of turbine blade cross section (4D) is driven by a high pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for 910,000 times power, and heat consumption is reduced to about 1 / 539 ・ Various energy storage cycle coalescence engine to make various ships such as steam driven 1700 times kg weight m / sec.   Combined engine combustion section (31Y) high temperature water (52b) of turbine blade cross section (4D) is driven by a high pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for 910,000 times power, and heat consumption is reduced to about 1 / 539 ・ Various energy storage cycle coalescence engine to make various ships such as steam driven 1700 times kg weight m / sec.   The turbine blade cross section (4D) full blade combustion part (32X) high-temperature water (52b) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for a 910,000-fold work rate, and the amount of heat consumed is approximately 1 / 539 ・ Various energy conservation cycle coalescence engine for various ships such as steam driven 1700 times kg weight m / sec.   The turbine blade cross section (4D) full blade combustion section (32Y) high temperature water (52b) is driven by a high pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for 910,000 times the power, and the heat consumption is reduced to about 1 / 539 ・ Various energy conservation cycle coalescence engine for various ships such as steam driven 1700 times kg weight m / sec.   The turbine blade cross section (4D) full blade combustion part (32X) high-temperature water (52b) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for a 910,000-fold work rate, and the amount of heat consumed is approximately 1 / 539 ・ Various energy storage cycle coalescence engine that uses various heat, electricity and cold supply facilities such as 1700 times kg weight m / second of steam drive.   The turbine blade cross section (4D) full blade combustion section (32Y) high temperature water (52b) is driven by a high pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for 910,000 times the power, and the heat consumption is reduced to about 1 / 539 ・ Various energy storage cycle coalescence engine that uses various heat, electricity and cold supply facilities such as 1700 times kg weight m / second of steam drive.   Combined engine combustion section (31X) high temperature water (52b) of turbine blade cross section (4D) is driven by a high pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for 910,000 times power, and heat consumption is reduced to about 1 / 539 ・ Various energy storage cycle coalescence engine for various heat, electricity and cold supply facilities such as 1700 times kg weight m / sec of steam drive.   Combined engine combustion section (31Y) high temperature water (52b) of turbine blade cross section (4D) is driven by a high pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for 910,000 times power, and heat consumption is reduced to about 1 / 539 ・ Various energy storage cycle coalescence engine for various heat, electricity and cold supply facilities such as 1700 times kg weight m / sec of steam drive.   Combined engine combustion section (31X) high temperature water (52b) of turbine blade cross section (4D) is driven by a high pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for 910,000 times power, and heat consumption is reduced to about 1 / 539 ・ Various energy storage cycle coalescence engine that makes the same speed output of atmospheric pressure 1700 times kg weight m / second of steam drive and supplies various heat, electricity and cold supply facilities with gravity acceleration in vacuum.   Combined engine combustion section (31Y) high temperature water (52b) of turbine blade cross section (4D) is driven by a high pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for 910,000 times power, and heat consumption is reduced to about 1 / 539 ・ Various energy storage cycle coalescence engine that makes the same speed output of atmospheric pressure 1700 times kg weight m / second of steam drive and supplies various heat, electricity and cold supply facilities with gravity acceleration in vacuum.   The turbine blade cross section (4D) full blade combustion part (32X) high-temperature water (52b) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for a 910,000-fold work rate, and the amount of heat consumed is approximately 1 / 539 ・ Various energy storage cycle coalescence engine that makes the same speed output of atmospheric pressure 1700 times kg weight m / sec of steam drive and supplies various heat, electricity and cold supply facilities with gravity acceleration in vacuum.   The turbine blade cross section (4D) full blade combustion section (32Y) high temperature water (52b) is driven by a high pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for 910,000 times the power, and the heat consumption is reduced to about 1 / 539 ・ Various energy storage cycle coalescence engine that makes the same speed output of atmospheric pressure 1700 times kg weight m / sec of steam drive and supplies various heat, electricity and cold supply facilities with gravity acceleration in vacuum.   The turbine blade cross section (4D) full blade combustion part (32X) high-temperature water (52b) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for a 910,000-fold work rate, and the amount of heat consumed is approximately 1 / 539 ・ Various energy conservation cycle coalescence engine that makes the same speed output at atmospheric pressure 1700 times kg weight m / sec.   The turbine blade cross section (4D) full blade combustion section (32Y) high temperature water (52b) is driven by a high pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for 910,000 times the power, and the heat consumption is reduced to about 1 / 539 ・ Various energy conservation cycle coalescence engine that makes the same speed output at atmospheric pressure 1700 times kg weight m / sec.   Combined engine combustion section (31X) high temperature water (52b) of turbine blade cross section (4D) is driven by a high pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for 910,000 times power, and heat consumption is reduced to about 1 / 539 ・ Various energy storage cycle coalescing engine that makes the same pressure output at atmospheric pressure 1700 times kg weight m / sec.   Combined engine combustion section (31Y) high temperature water (52b) of turbine blade cross section (4D) is driven by a high pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for 910,000 times power, and heat consumption is reduced to about 1 / 539 ・ Various energy storage cycle coalescing engine that makes the same pressure output at atmospheric pressure 1700 times kg weight m / sec.   Combined engine combustion section (31X) high temperature water (52b) of turbine blade cross section (4D) is driven by a high pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for 910,000 times power, and heat consumption is reduced to about 1 / 539 ・ Various energy storage cycle coalescing engine that makes the same speed output of atmospheric pressure 1700 times kg weight m / sec of steam drive and makes various airplanes with gravity acceleration added in vacuum.   Combined engine combustion section (31Y) high temperature water (52b) of turbine blade cross section (4D) is driven by a high pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for 910,000 times power, and heat consumption is reduced to about 1 / 539 ・ Various energy storage cycle coalescing engine that makes the same speed output of atmospheric pressure 1700 times kg weight m / sec of steam drive and makes various airplanes with gravity acceleration added in vacuum.   The turbine blade cross section (4D) full blade combustion part (32X) high-temperature water (52b) is driven by a high-pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for a 910,000-fold work rate, and the amount of heat consumed is approximately 1 / 539 ・ Various energy conservation cycle coalescence engine that makes the same speed output of atmospheric pressure 1700 times kg weight m / second of steam drive, and makes various airplanes with gravity acceleration added in vacuum.   The turbine blade cross section (4D) full blade combustion section (32Y) high temperature water (52b) is driven by a high pressure turbine provided with a bearing (80) thrust bearing (80a) aiming for 910,000 times the power, and the heat consumption is reduced to about 1 / 539 ・ Various energy conservation cycle coalescence engine that makes the same speed output of atmospheric pressure 1700 times kg weight m / second of steam drive, and makes various airplanes with gravity acceleration added in vacuum.   A turbine blade cross section (4D) full rotor blade combustion part (32X) high temperature mercury (1d) with a bearing aimed at 166,000 times work (80) thrust bearing (80a) is driven by a high pressure turbine to drive heat consumption. Various energy conservation cycle coalescing engines that make approximately 1/72 at atmospheric pressure and the same speed output to 23,000 times the weight of steam driven kg weight m / sec.   A turbine blade cross section (4D) full rotor blade combustion section (32Y) high temperature mercury (1d) with a bearing aiming at 166,000 times work rate (80) thrust bearing (80a) is driven by a high pressure turbine to reduce the amount of heat consumed. Various energy conservation cycle coalescing engines that make approximately 1/72 at atmospheric pressure and the same speed output to 23,000 times the weight of steam driven kg weight m / sec.   Combined engine combustion section (31X) high-temperature mercury (1d) of turbine blade cross section (4D), bearing (80) thrust bearing (80a) aimed at 166,000 times work rate, driven by high pressure turbine to reduce heat consumption 1/72 ・ Atmospheric pressure same speed output 23,000 times the weight of steam driven kg weight m / second, etc. Various energy conservation cycle coalescing engine to make various airplanes with gravity acceleration added in vacuum.   Combined combustion section (31Y) of turbine blade cross section (4D) with high-temperature mercury (1d), bearing (80) thrust bearing (80a) aimed at 166,000 times work rate, driven by high pressure turbine to reduce heat consumption 1/72 ・ Atmospheric pressure same speed output 23,000 times the weight of steam driven kg weight m / second, etc. Various energy conservation cycle coalescing engine to make various airplanes with gravity acceleration added in vacuum.   Combined engine combustion section (31X) high-temperature mercury (1d) of turbine blade cross section (4D), bearing (80) thrust bearing (80a) aimed at 166,000 times work rate, driven by high pressure turbine to reduce heat consumption Various energy conservation cycle coalescing engines that make 1/72 · atmospheric pressure same speed output to 23,000 times the weight of steam driven kg weight m / second, etc. in a ship with additional gravity acceleration in vacuum.   Combined combustion section (31Y) of turbine blade cross section (4D) with high-temperature mercury (1d), bearing (80) thrust bearing (80a) aimed at 166,000 times work rate, driven by high pressure turbine to reduce heat consumption Various energy conservation cycle coalescing engines that make 1/72 · atmospheric pressure same speed output to 23,000 times the weight of steam driven kg weight m / second, etc. in a ship with additional gravity acceleration in vacuum.   A turbine blade cross section (4D) full rotor blade combustion part (32X) high temperature mercury (1d) with a bearing aimed at 166,000 times work (80) thrust bearing (80a) is driven by a high pressure turbine to drive heat consumption. Various energy conservation cycle coalescing engines that make approximately 1/72 at atmospheric pressure and the same speed output 23,000 times the weight of steam driven kg weight m / sec.   A turbine blade cross section (4D) full rotor blade combustion section (32Y) high temperature mercury (1d) with a bearing aiming at 166,000 times work rate (80) thrust bearing (80a) is driven by a high pressure turbine to reduce the amount of heat consumed. Various energy conservation cycle coalescing engines that make approximately 1/72 at atmospheric pressure and the same speed output 23,000 times the weight of steam driven kg weight m / sec.   A turbine blade cross section (4D) full rotor blade combustion part (32X) high temperature mercury (1d) with a bearing aimed at 166,000 times work (80) thrust bearing (80a) is driven by a high pressure turbine to drive heat consumption. Combined with various energy conservation cycles to provide various heat, electricity and cold supply equipment with additional gravity acceleration in a vacuum of approximately 1/72 · atmospheric pressure at the same speed output to 23,000 times kg weight m / second of steam drive organ.   A turbine blade cross section (4D) full rotor blade combustion section (32Y) high temperature mercury (1d) with a bearing aiming at 166,000 times work rate (80) thrust bearing (80a) is driven by a high pressure turbine to reduce the amount of heat consumed. Combined with various energy conservation cycles to provide various heat, electricity and cold supply equipment with additional gravity acceleration in a vacuum of approximately 1/72 · atmospheric pressure at the same speed output to 23,000 times kg weight m / second of steam drive organ.   Combined engine combustion section (31X) high-temperature mercury (1d) of turbine blade cross section (4D), bearing (80) thrust bearing (80a) aimed at 166,000 times work rate, driven by high pressure turbine to reduce heat consumption 1/72 ・ Atmospheric pressure same speed output 23,000 times the weight of steam driven kg weight m / second, etc. Various energy conservation cycle coalescence engine that makes gravity acceleration additional various heat, electricity and cold supply equipment in vacuum .   Combined combustion section (31Y) of turbine blade cross section (4D) with high-temperature mercury (1d), bearing (80) thrust bearing (80a) aimed at 166,000 times work rate, driven by high pressure turbine to reduce heat consumption 1/72 ・ Atmospheric pressure same speed output 23,000 times the weight of steam driven kg weight m / second, etc. Various energy conservation cycle coalescence engine that makes gravity acceleration additional various heat, electricity and cold supply equipment in vacuum .   Turbine blade cross section (4D) united engine combustion part (31X) high temperature mercury (1d) injected vertically downward in a vacuum and added acceleration of gravitational acceleration, bearing aiming at 166,000 times work rate (80) thrust bearing ( Various energy storage cycle coalescing engines that reduce the heat consumption of the high-pressure turbine drive provided with 80a) to approximately 1/72.   Turbine blade cross section (4D) coalescence engine combustion part (31Y) high temperature mercury (1d) vertically downward jetting acceleration by adding gravitational acceleration in vacuum, bearing aiming at 166,000 times work rate (80) thrust bearing ( Various energy storage cycle coalescing engines that reduce the heat consumption of the high-pressure turbine drive provided with 80a) to approximately 1/72.   Turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) injected vertically downward in a vacuum and acceleration by adding gravitational acceleration to a bearing aiming at 166,000 times work rate (80) thrust bearing (80a) A high-pressure turbine drive heat consumption amount that is provided with various energy storage cycle coalescing engines that are approximately 1/72.   Turbine blade cross section (4D) full blade combustor (32Y) high temperature mercury (1d) injected vertically downward in a vacuum to accelerate acceleration by adding gravitational acceleration (80) thrust bearing (80) thrust bearing (80a) A high-pressure turbine drive heat consumption amount that is provided with various energy storage cycle coalescing engines that are approximately 1/72.   Turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) injected vertically downward in a vacuum and acceleration by adding gravitational acceleration to a bearing aiming at 166,000 times work rate (80) thrust bearing (80a) A high-speed turbine drive heat consumption is provided. Various energy storage cycle coalescing engines that use approximately 1/72 of various heat, electricity, and cold supply facilities.   Turbine blade cross section (4D) full blade combustor (32Y) high temperature mercury (1d) injected vertically downward in a vacuum to accelerate acceleration by adding gravitational acceleration (80) thrust bearing (80) thrust bearing (80a) A high-speed turbine drive heat consumption is provided. Various energy storage cycle coalescing engines that use approximately 1/72 of various heat, electricity, and cold supply facilities.   Turbine blade cross section (4D) united engine combustion part (31X) high temperature mercury (1d) injected vertically downward in a vacuum and added acceleration of gravitational acceleration, bearing aiming at 166,000 times work rate (80) thrust bearing ( Various energy storage cycle coalescing engines which use 80a) to supply high heat turbine drive heat consumption of approximately 1/72 of various heat, electricity and cold supply facilities.   Turbine blade cross section (4D) coalescence engine combustion part (31Y) high temperature mercury (1d) vertically downward jetting acceleration by adding gravitational acceleration in vacuum, bearing aiming at 166,000 times work rate (80) thrust bearing ( Various energy storage cycle coalescing engines which use 80a) to supply high heat turbine drive heat consumption of approximately 1/72 of various heat, electricity and cold supply facilities.   Turbine blade cross section (4D) united engine combustion part (31X) high temperature mercury (1d) injected vertically downward in a vacuum and added acceleration of gravitational acceleration, bearing aiming at 166,000 times work rate (80) thrust bearing ( Various energy storage cycle coalescing engines that make the high-pressure turbine drive heat consumption provided with 80a) approximately 1/72 of various ships.   Turbine blade cross section (4D) coalescence engine combustion part (31Y) high temperature mercury (1d) vertically downward jetting acceleration by adding gravitational acceleration in vacuum, bearing aiming at 166,000 times work rate (80) thrust bearing ( Various energy storage cycle coalescing engines that make the high-pressure turbine drive heat consumption provided with 80a) approximately 1/72 of various ships.   Turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) injected vertically downward in a vacuum and acceleration by adding gravitational acceleration to a bearing aiming at 166,000 times work rate (80) thrust bearing (80a) A high-speed turbine drive heat consumption amount provided with various energy storage cycle coalescing engines that make various ship types approximately 1/72.   Turbine blade cross section (4D) full blade combustor (32Y) high temperature mercury (1d) injected vertically downward in a vacuum to accelerate acceleration by adding gravitational acceleration (80) thrust bearing (80) thrust bearing (80a) A high-speed turbine drive heat consumption amount provided with various energy storage cycle coalescing engines that make various ship types approximately 1/72.   Turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) injected vertically downward in a vacuum and acceleration by adding gravitational acceleration to a bearing aiming at 166,000 times work rate (80) thrust bearing (80a) A high-speed turbine drive heat consumption is provided.   Turbine blade cross section (4D) full blade combustor (32Y) high temperature mercury (1d) injected vertically downward in a vacuum to accelerate acceleration by adding gravitational acceleration (80) thrust bearing (80) thrust bearing (80a) A high-speed turbine drive heat consumption is provided.   Turbine blade cross section (4D) united engine combustion part (31X) high temperature mercury (1d) injected vertically downward in a vacuum and added acceleration of gravitational acceleration, bearing aiming at 166,000 times work rate (80) thrust bearing ( Various energy storage cycle coalescing engines that use 80a) to make various airplanes whose heat consumption for driving a high-pressure turbine is approximately 1/72.   Turbine blade cross section (4D) coalescence engine combustion part (31Y) high temperature mercury (1d) vertically downward jetting acceleration by adding gravitational acceleration in vacuum, bearing aiming at 166,000 times work rate (80) thrust bearing ( Various energy storage cycle coalescing engines that use 80a) to make various airplanes whose heat consumption for driving a high-pressure turbine is approximately 1/72.   Combined engine combustion section (31X) high-temperature water (52b) with turbine blade cross section (4D) sprayed vertically downward in a vacuum to add a gravitational acceleration to a bearing aiming at 910,000 times power (80) thrust bearing (80a) Various energy conservation cycle coalescing engines that make various types of airplanes with approximately 1/539 of heat consumption for driving high-pressure turbines.   Turbine blade cross section (4D) united engine combustion section (31Y) high temperature water (52b) jetted vertically downward in a vacuum to add a gravitational acceleration bearing (80) thrust bearing (80a) thrust bearing (80a) Various energy conservation cycle coalescing engines that make various types of airplanes with approximately 1/539 of heat consumption for driving high-pressure turbines.   Turbine blade cross section (4D) full blade combustion part (32X) high temperature water (52b) jetted vertically downward in a vacuum to add acceleration of gravitational acceleration bearing (80) thrust bearing (80a) thrust bearing (80a Various energy storage cycle coalescing engines that make various types of airplanes having a heat consumption of about 1/539.   Turbine blade cross section (4D) full rotor blade combustion section (32Y) high temperature water (52b) injected vertically downward in a vacuum and added with gravitational acceleration, bearing (80) thrust bearing (80a) Various energy storage cycle coalescing engines that make various types of airplanes having a heat consumption of about 1/539.   Turbine blade cross section (4D) full blade combustion part (32X) high temperature water (52b) jetted vertically downward in a vacuum to add acceleration of gravitational acceleration bearing (80) thrust bearing (80a) thrust bearing (80a Various energy storage cycle coalescing engines that make the high-pressure turbine drive heat consumption provided with a) about 1/539 of various ships.   Turbine blade cross section (4D) full rotor blade combustion section (32Y) high temperature water (52b) injected vertically downward in a vacuum and added with gravitational acceleration, bearing (80) thrust bearing (80a) Various energy storage cycle coalescing engines that make the high-pressure turbine drive heat consumption provided with a) about 1/539 of various ships.   Combined engine combustion section (31X) high-temperature water (52b) with turbine blade cross section (4D) sprayed vertically downward in a vacuum to add a gravitational acceleration to a bearing aiming at 910,000 times power (80) thrust bearing (80a) Various energy storage cycle coalescing engines which make the high-pressure turbine drive heat consumption with approximately 1/539 various ships.   Turbine blade cross section (4D) united engine combustion section (31Y) high temperature water (52b) jetted vertically downward in a vacuum to add a gravitational acceleration bearing (80) thrust bearing (80a) thrust bearing (80a) Various energy storage cycle coalescing engines which make the high-pressure turbine drive heat consumption with approximately 1/539 various ships.   Combined engine combustion section (31X) high-temperature water (52b) with turbine blade cross section (4D) sprayed vertically downward in a vacuum to add a gravitational acceleration to a bearing aiming at 910,000 times power (80) thrust bearing (80a) Various energy storage cycle coalescing engines that use a high-pressure turbine drive with a heat consumption of approximately 1/539 of various heat, electricity, and cold supply facilities.   Turbine blade cross section (4D) united engine combustion section (31Y) high temperature water (52b) jetted vertically downward in a vacuum to add a gravitational acceleration bearing (80) thrust bearing (80a) thrust bearing (80a) Various energy storage cycle coalescing engines that use a high-pressure turbine drive with a heat consumption of approximately 1/539 of various heat, electricity, and cold supply facilities.   Turbine blade cross section (4D) full blade combustion part (32X) high temperature water (52b) jetted vertically downward in a vacuum to add acceleration of gravitational acceleration bearing (80) thrust bearing (80a) thrust bearing (80a Various energy storage cycle coalescing engines that use high-pressure turbine drive heat consumption provided with a) to make various heat, electricity and cold supply facilities of approximately 1/539.   Turbine blade cross section (4D) full rotor blade combustion section (32Y) high temperature water (52b) injected vertically downward in a vacuum and added with gravitational acceleration, bearing (80) thrust bearing (80a) Various energy storage cycle coalescing engines that use high-pressure turbine drive heat consumption provided with a) to make various heat, electricity and cold supply facilities of approximately 1/539.   Turbine blade cross section (4D) full blade combustion part (32X) high temperature water (52b) jetted vertically downward in a vacuum to add acceleration of gravitational acceleration bearing (80) thrust bearing (80a) thrust bearing (80a ) Various energy storage cycle coalescing engines that reduce the heat consumption of high-pressure turbine drive to approximately 1/539.   Turbine blade cross section (4D) full rotor blade combustion section (32Y) high temperature water (52b) injected vertically downward in a vacuum and added with gravitational acceleration, bearing (80) thrust bearing (80a) ) Various energy storage cycle coalescing engines that reduce the heat consumption of high-pressure turbine drive to approximately 1/539.   Combined engine combustion section (31X) high-temperature water (52b) with turbine blade cross section (4D) sprayed vertically downward in a vacuum to add a gravitational acceleration to a bearing aiming at 910,000 times power (80) thrust bearing (80a) Various energy storage cycle coalescing engines that reduce the heat consumption of high-pressure turbine drive to approximately 1/539.   Turbine blade cross section (4D) united engine combustion section (31Y) high temperature water (52b) jetted vertically downward in a vacuum to add a gravitational acceleration bearing (80) thrust bearing (80a) thrust bearing (80a) Various energy storage cycle coalescing engines that reduce the heat consumption of high-pressure turbine drive to approximately 1/539.   Turbine blade cross section (4D) bearing with a target of 166,000 times the work rate (80) Combined engine combustion section (31X) with thrust bearing (80a) High temperature mercury (1d) Heated intake air is compressed by the amount of exhaust heat Heat recovery theory The best heat pump (1G), combined with various energy storage cycle engines that consumes almost 1/72 of heat.   Turbine blade cross section (4D) bearing with a target of 166,000 times the work rate (80) Combined engine combustion section (31Y) provided with thrust bearing (80a) High-temperature mercury (1d) Heated intake air is compressed by the amount of exhaust heat Heat recovery theory The best heat pump (1G), combined with various energy storage cycle engines that consumes almost 1/72 of heat.   Turbine blade cross section (4D) bearing with a target of 166,000 times the work rate (80) Thrust blade combustion part (32X) provided with thrust bearing (80a) High temperature mercury (1d) Compression heat recovery theory The best heat pump (1G), combined with various energy storage cycle engines that consumes approximately 1/72 of heat.   Turbine blade cross section (4D) bearing with a target of 166,000 times the work efficiency (80) Thrust bearing combustion unit (32Y) provided with thrust bearing (80a) High-temperature mercury (1d) Compression heat recovery theory The best heat pump (1G), combined with various energy storage cycle engines that consumes approximately 1/72 of heat.   Turbine blade cross section (4D) bearing with a target of 166,000 times the work rate (80) Thrust bearing combustion portion (32X) with high thrust mercury (1d) near 230 degrees Various energy storage cycle coalescing engine that heats and consumes approximately 1/72 as the best heat pump (1G) for compression heat recovery theory.   Turbine blade cross section (4D) bearing with a target of 166,000 times the work efficiency (80) Thrust bearing combustion portion (32Y) high temperature mercury (1d) provided with thrust bearing (80a) Various energy storage cycle coalescing engine that heats and consumes approximately 1/72 as the best heat pump (1G) for compression heat recovery theory.   Turbine blade cross-section (4D) bearing with a target of 166,000 times the work rate (80) Combined engine combustion part (31X) provided with thrust bearing (80a) High-temperature mercury (1d) Heating the intake air by 230 degree exhaust heat As a compression heat recovery theory best heat pump (1G), various energy storage cycle coalescing engines that reduce the amount of heat consumed to approximately 1/72.   Turbine blade cross section (4D) bearing with a target of 166,000 times work (80) Combined engine combustion part (31Y) with thrust bearing (80a) High temperature mercury (1d) Heating intake air by 230 degree exhaust heat quantity As a compression heat recovery theory best heat pump (1G), various energy storage cycle coalescing engines that reduce the amount of heat consumed to approximately 1/72.   Turbine blade cross-section (4D) bearing with a target of 166,000 times the work rate (80) Combined engine combustion part (31X) provided with thrust bearing (80a) High-temperature mercury (1d) Heating the intake air by 230 degree exhaust heat As a compression heat recovery theory best heat pump (1G), various energy storage cycle coalescing engines that use various heat, electricity and cold supply facilities with a heat consumption of approximately 1/72.   Turbine blade cross section (4D) bearing with a target of 166,000 times work (80) Combined engine combustion part (31Y) with thrust bearing (80a) High temperature mercury (1d) Heating intake air by 230 degree exhaust heat quantity As a compression heat recovery theory best heat pump (1G), various energy storage cycle coalescing engines that use various heat, electricity and cold supply facilities with a heat consumption of approximately 1/72.   Turbine blade cross section (4D) bearing with a target of 166,000 times the work rate (80) Thrust bearing combustion portion (32X) with high thrust mercury (1d) near 230 degrees Various energy storage cycle coalescing engines that use heat and heat as the best heat pump (1G) to make the heat, electricity, and cold supply facilities of approximately 1/72.   Turbine blade cross section (4D) bearing with a target of 166,000 times the work efficiency (80) Thrust bearing combustion portion (32Y) high temperature mercury (1d) provided with thrust bearing (80a) Various energy storage cycle coalescing engines that use heat and heat as the best heat pump (1G) to make the heat, electricity, and cold supply facilities of approximately 1/72.   Turbine blade cross section (4D) bearing with a target of 166,000 times the work rate (80) Thrust bearing combustion portion (32X) with high thrust mercury (1d) near 230 degrees Various energy storage cycle coalescing engines that heat and use as the best heat pump (1G) for compression heat recovery to make various kinds of ships whose heat consumption is approximately 1/72.   Turbine blade cross section (4D) bearing with a target of 166,000 times the work efficiency (80) Thrust bearing combustion portion (32Y) high temperature mercury (1d) provided with thrust bearing (80a) Various energy storage cycle coalescing engines that heat and use as the best heat pump (1G) for compression heat recovery to make various kinds of ships whose heat consumption is approximately 1/72.   Turbine blade cross-section (4D) bearing with a target of 166,000 times the work rate (80) Combined engine combustion part (31X) provided with thrust bearing (80a) High-temperature mercury (1d) Heating the intake air by 230 degree exhaust heat As a best heat pump (1G) for compression heat recovery, various energy storage cycle coalescing engines that make various kinds of ships whose heat consumption is approximately 1/72.   Turbine blade cross section (4D) bearing with a target of 166,000 times work (80) Combined engine combustion part (31Y) with thrust bearing (80a) High temperature mercury (1d) Heating intake air by 230 degree exhaust heat quantity As a best heat pump (1G) for compression heat recovery, various energy storage cycle coalescing engines that make various kinds of ships whose heat consumption is approximately 1/72.   Turbine blade cross-section (4D) bearing with a target of 166,000 times the work rate (80) Combined engine combustion part (31X) provided with thrust bearing (80a) High-temperature mercury (1d) Heating the intake air by 230 degree exhaust heat As a best heat pump (1G) for compression heat recovery, various energy storage cycle coalescing engines with various heat consumption of approximately 1/72.   Turbine blade cross section (4D) bearing with a target of 166,000 times work (80) Combined engine combustion section (31Y) with high thrust mercury (1d) with thrust bearing (80a) Heating intake air by 230 degree exhaust heat As a best heat pump (1G) for compression heat recovery, various energy storage cycle coalescing engines with various heat consumption of approximately 1/72.   Turbine blade cross section (4D) bearing with a target of 166,000 times the work rate (80) Thrust bearing combustion portion (32X) with high thrust mercury (1d) near 230 degrees Various energy storage cycle coalescing engines that are heated to produce various airplanes with a heat consumption of approximately 1/72 as the best heat pump (1G) for compression heat recovery theory.   Turbine blade cross section (4D) bearing with a target of 166,000 times the work efficiency (80) Thrust bearing combustion portion (32Y) high temperature mercury (1d) provided with thrust bearing (80a) Various energy storage cycle coalescing engines that are heated to produce various airplanes with a heat consumption of approximately 1/72 as the best heat pump (1G) for compression heat recovery theory.   Turbine blade cross section (4D) bearing with a target of 166,000 times the work efficiency (80) Combined engine combustion part (31X) with thrust bearing (80a) High temperature mercury (1d) Heated intake air is compressed by the amount of exhaust heat Heat recovery theory The best heat pump (1G), combined with various energy storage cycle engines that use approximately 1/72 of various heat, electricity and cold supply facilities.   Turbine blade cross section (4D) bearing with a target of 166,000 times the work rate (80) Combined engine combustion section (31Y) provided with thrust bearing (80a) High-temperature mercury (1d) Heated intake air is compressed by the amount of exhaust heat Heat recovery theory The best heat pump (1G), combined with various energy storage cycle engines that use approximately 1/72 of various heat, electricity and cold supply facilities.   Turbine blade cross section (4D) bearing with a target of 166,000 times the work rate (80) Thrust blade combustion part (32X) provided with thrust bearing (80a) High temperature mercury (1d) Compressed heat recovery theory The best energy pump (1G), combined with various energy storage cycle engines that use various heat, electricity, and cold supply facilities that consume approximately 1/72 of heat.   Turbine blade cross section (4D) bearing with a target of 166,000 times the work efficiency (80) Thrust bearing combustion unit (32Y) provided with thrust bearing (80a) High-temperature mercury (1d) Compressed heat recovery theory The best energy pump (1G), combined with various energy storage cycle engines that use various heat, electricity, and cold supply facilities that consume approximately 1/72 of heat.   Turbine blade cross section (4D) bearing with a target of 166,000 times the work rate (80) Thrust blade combustion part (32X) provided with thrust bearing (80a) High temperature mercury (1d) Compressed heat recovery theory The best heat pump (1G), combined with various energy storage cycle engines that make various kinds of ships whose heat consumption is approximately 1/72.   Turbine blade cross section (4D) bearing with a target of 166,000 times the work efficiency (80) Thrust bearing combustion unit (32Y) provided with thrust bearing (80a) High-temperature mercury (1d) Compressed heat recovery theory The best heat pump (1G), combined with various energy storage cycle engines that make various kinds of ships whose heat consumption is approximately 1/72.   Turbine blade cross section (4D) bearing with a target of 166,000 times the work rate (80) Combined engine combustion section (31X) with thrust bearing (80a) High temperature mercury (1d) Heated intake air is compressed by the amount of exhaust heat Heat recovery theory The best energy pump (1G), combined with various energy conservation cycle engines that make various kinds of ships with a heat consumption of approximately 1/72.   Turbine blade cross section (4D) bearing with a target of 166,000 times the work rate (80) Combined engine combustion section (31Y) provided with thrust bearing (80a) High-temperature mercury (1d) Heated intake air is compressed by the amount of exhaust heat Heat recovery theory The best energy pump (1G), combined with various energy conservation cycle engines that make various kinds of ships with a heat consumption of approximately 1/72.   Turbine blade cross section (4D) bearing with a target of 166,000 times the work rate (80) Combined engine combustion section (31X) with thrust bearing (80a) High temperature mercury (1d) Heated intake air is compressed by the amount of exhaust heat Heat recovery theory The best engine for heat recovery (1G). Various energy storage cycle coalescing engines that use various airplanes with approximately 1/72 of heat consumption.   Turbine blade cross section (4D) bearing with a target of 166,000 times the work rate (80) Combined engine combustion section (31Y) provided with thrust bearing (80a) High-temperature mercury (1d) Heated intake air is compressed by the amount of exhaust heat Heat recovery theory The best engine for heat recovery (1G). Various energy storage cycle coalescing engines that use various airplanes with approximately 1/72 of heat consumption.   Turbine blade cross section (4D) bearing with a target of 166,000 times the work rate (80) Thrust blade combustion part (32X) provided with thrust bearing (80a) High temperature mercury (1d) Compressed heat recovery theory As a best heat pump (1G), it combines various energy storage cycle engines that make various airplanes with a heat consumption of approximately 1/72.   Turbine blade cross section (4D) bearing with a target of 166,000 times the work efficiency (80) Thrust bearing combustion unit (32Y) provided with thrust bearing (80a) High-temperature mercury (1d) Compressed heat recovery theory As a best heat pump (1G), it combines various energy storage cycle engines that make various airplanes with a heat consumption of approximately 1/72.   Various types of recovering cold heat by providing a cold heat recovery means (3C) on the turbine blade (8c) of a full blade gas turbine provided with a bearing (80) thrust bearing (80a) corresponding to all blades of the turbine blade cross section (4D). Various energy storage cycle coalescing engines for heat, electricity and cold supply facilities.   A turbine blade cross section (4D) bearing for all moving blades (80) Various heat for heating by providing a cold heat recovery means (3C) to the turbine blade (8c) of a full moving blade gas turbine provided with a thrust bearing (80a) Various energy storage cycle coalescing engines for supplying electricity and cold energy.   A turbine blade (8c) of a full rotor blade gas turbine provided with a bearing (80) thrust bearing (80a) corresponding to all rotor blades of a turbine blade cross section (4D) is provided with a cold heat recovery means (3C) to provide alcohol (1C), etc. Various energy storage cycle coalescing engines that use various heat and electricity and cold supply facilities to recover cold heat.   A turbine blade (8c) of a full rotor blade gas turbine provided with a bearing (80) thrust bearing (80a) corresponding to all rotor blades of a turbine blade cross section (4D) is provided with a cold heat recovery means (3C) to provide alcohol (1C), etc. Various energy storage cycle coalescing engine to supply various heat and electricity and cold supply equipment.   A turbine blade (8c) of a full rotor blade gas turbine provided with a bearing (80) thrust bearing (80a) corresponding to all rotor blades of a turbine blade cross section (4D) is provided with a cold heat recovery means (3C) to provide alcohol (1C), etc. Various energy storage cycle coalescing engines that use various heat, electricity, and cold supply facilities to increase the recovery output of cold heat.   A turbine blade (8c) of a full rotor blade gas turbine provided with a bearing (80) thrust bearing (80a) corresponding to all rotor blades of a turbine blade cross section (4D) is provided with a cold heat recovery means (3C) to provide alcohol (1C), etc. Various energy storage cycle coalescing engines that use various heat, electricity and cold supply facilities to increase heating output.   A turbine blade (8c) of a full rotor blade gas turbine provided with a bearing (80) thrust bearing (80a) corresponding to all rotor blades of a turbine blade cross section (4D) is provided with a cold heat recovery means (3C) to provide alcohol (1C), etc. Recovers cold energy at various energy storage cycle coalescing engines that make various types of heat, electricity, and cold energy supply equipment that prevents dry ice and moisture from sticking.   A turbine blade (8c) of a full rotor blade gas turbine provided with a bearing (80) thrust bearing (80a) corresponding to all rotor blades of a turbine blade cross section (4D) is provided with a cold heat recovery means (3C) to provide alcohol (1C), etc. Various energy storage cycle coalescing engines that use various heat, electricity, and cold supply facilities to prevent adhesion of heated dry ice and moisture.   A turbine blade (8c) provided with a bearing (80) thrust bearing (80a) aiming at a 910,000-fold work rate of the turbine blade cross section (4D) is provided with a heating high temperature means (3B) and heated. Various energy storage cycle coalescing engines for heat, electricity and cold supply facilities.   The turbine blade (8c) of the all-rotor blade water turbine provided with the bearing (80) thrust bearing (80a) aiming for 910,000 times the work of the turbine blade cross section (4D) is provided with water repellent action (3A) to repel water. Various energy storage cycle coalescing engines to provide various heat, electricity and cold supply facilities.   The turbine blade (8c) of the all-blade water turbine provided with the bearing (80) thrust bearing (80a) aiming at 910,000 times the power of the turbine blade cross section (4D) is provided with a heating high temperature means (3B) and heated vaporized film Various energy storage cycle coalescence engines that use various heat, electricity, and cold supply facilities for rolling contact rotation output.   Turbine blade cross section (4D) 910,000 times work-targeted bearing (80) Thrust bearing (80a) provided with water-repellent action (3A) on turbine blade (8c) of all-bladed water turbine Various energy storage cycle coalescence engines that use various heat, electricity, and cold supply facilities for rolling contact rotation output.   Various heat and electricity in which the exhaust saturation temperature of the whole rotor blade water turbine provided with the bearing (80) thrust bearing (80a) aiming at 910,000 times the turbine blade cross section (4D) is cooled (52e) cooling Combined with various energy storage cycle engines to make cold and cold supply equipment.   Turbine blade cross section (4D) 910,000 times work-targeted bearing (80) Thrust bearing (80a) provided with a thrust blade (80a) of all rotor blade water turbine near 30 degrees exhaust saturation temperature cooling (52e) cooling to prevent seawater temperature rise Various energy storage cycle coalescing engines that make various heat, electricity and cold supply facilities.   Various heat, electricity, and cold used by recovering and storing alcohol cold heat (52e) in a full rotor blade gas turbine provided with a bearing (80) thrust bearing (80a) aiming for a 910,000-fold work rate of the turbine blade cross section (4D) Various energy conservation cycle coalescing engines to be used as a supply facility.   A turbine blade cross-section (4D) bearing for all rotor blades (80) Compressed air cold heat (52e) is recovered and stored in an all rotor blade gas turbine provided with a thrust bearing (80a). Various energy storage cycle coalescing engines for supply facilities.   Supply of various types of heat, electricity, and cold used by recovering and storing ice-cooled heat (52e) in a full-rotary-blade gas turbine provided with a bearing (80) thrust bearing (80a) with a turbine blade cross section (4D) Various energy storage cycle coalescing engines for equipment.   A turbine blade cross-section (4D) bearing for all rotor blades (80) A variety of heat to be used for various refrigeration equipment by collecting and storing cold heat (52e) in a full rotor blade gas turbine provided with a thrust bearing (80a) Various energy storage cycle coalescing engines for supplying electricity and cold energy.   A turbine blade cross-section (4D) bearing for all moving blades (80) Various heats for collecting and storing cold heat (52e) in a full rotor blade gas turbine provided with a thrust bearing (80a) Various energy storage cycle coalescing engines for supplying electricity and cold energy.   A turbine blade cross-section (4D) bearing for all rotor blades (80) A variety of heat to be used as various cooling equipment by collecting and storing cold heat (52e) in a full rotor blade gas turbine provided with a thrust bearing (80a) Various energy storage cycle coalescing engines for supplying electricity and cold energy.   A turbine blade cross-section (4D) bearing for all rotor blades (80) A variety of heat used to recover and store cold heat (52e) in a turbine blade gas turbine provided with a thrust bearing (80a) Various energy storage cycle coalescing engines for supplying electricity and cold energy.   A turbine blade cross-section (4D) bearing for all rotor blades (80) Various heat used for various ice making equipment by collecting and storing cold heat (52e) in a full rotor blade gas turbine provided with a thrust bearing (80a) Various energy storage cycle coalescing engines for supplying electricity and cold energy.   A turbine blade cross-section (4D) bearing for all rotor blades (80) Various moving turbine gas turbines provided with thrust bearings (80a) collect and store cold heat (52e) and use them as various compressed air cold piping buildings Various energy storage cycle coalescing engines for heat, electricity and cold supply facilities.   Various heat and electricity for supplying all rotor blade gas turbine exhaust with a turbine blade cross section (4D) corresponding to all rotor blades (80) thrust bearing (80a) to the seabed as CO2 and other combustion gas dissolved water (52 g) Combined with various energy storage cycle engines to make cold and cold supply equipment.   Turbine blade cross section (4D) bearings for all rotor blades (80) Thrust blade gas turbine exhaust provided with thrust bearing (80a) is supplied to the sea floor as CO2 and other combustion gas dissolved water (52 g) to supply seaweed Various energy storage cycle coalescing engines for various heat, electricity and cold supply facilities.   A turbine blade cross section (4D) bearing for all rotor blades (80) Thrust blade gas turbine exhaust provided with thrust bearing (80a) is supplied as combustion gas dissolved water (52 g) such as CO2 to the seafloor to grow algae Various energy storage cycle coalescing engines that make various heat, electricity and cold supply facilities.   A turbine blade cross section (4D) bearing for all rotor blades (80) Thrust blade gas turbine exhaust provided with thrust bearings (80a) is supplied to the sea floor as CO2 and other combustion gas dissolved water (52 g) to provide phytoplanktons Various energy storage cycle coalescing engines to make various heat and electricity and cold supply equipment to grow.   A specially designed rotary output equipped with a bearing (80) thrust bearing (80a) for turbine blade cross section (4D) applications. Various heat and electricity used by recovering and storing surplus heat at various temperatures (52d) of 300 degrees or less Combined with various energy storage cycle engines to make cold and cold supply equipment.   A specially designed rotary output with bearing (80) thrust bearing (80a) for turbine blade cross-section (4D) use is used to collect and store excess heat at various temperatures (52d) of 300 degrees or less as various types of heating equipment. Various energy storage cycle coalescing engines that use various heat, electricity, and cold supply facilities.   A specially designed rotary output equipped with a bearing (80) thrust bearing (80a) corresponding to the turbine blade cross section (4D) application is used to collect and store excess heat at various temperatures (52d) of 300 degrees or less as various cooking equipment. Various energy storage cycle coalescing engines that use various heat, electricity, and cold supply facilities.   A specially designed rotary output with bearing (80) thrust bearing (80a) for turbine blade cross-section (4D) use is used to collect and store surplus heat at various temperatures (52d) of 300 degrees or less as various types of hot water equipment. Various energy storage cycle coalescing engines that use various heat, electricity, and cold supply facilities.   A specially designed bearing for the turbine blade cross section (4D) (80) Thrust bearing (80a) is provided exclusively for rotational output. The excess heat is recovered and stored at various temperatures (52d) below 300 degrees and used as various dishwashers. Various energy storage cycle coalescing engines that make various heat, electricity and cold supply facilities.   A dedicated bearing for the turbine blade cross section (4D) (80) Thrust bearing (80a) is provided exclusively for rotational output. The excess heat is recovered and stored at various temperatures (52d) of 300 degrees or less as various washing dryers. Various energy storage cycle coalescing engines that use various heat, electricity, and cold supply facilities.   Bearings (80) suitable for turbine blade cross-section (4D) applications (80) Thrust bearings (80a) are provided exclusively for rotational output, and excess water is collected and stored at various temperatures (52d) of 300 degrees or less, and various hydrothermal pipe buildings Various energy storage cycle coalescing engine to be used as various heat, electricity and cold supply facilities.   For rotation output dedicated bearings (80) and thrust bearings (80a) that support turbine blade cross section (4D) applications, excess heat is recovered and stored at various temperatures (52d) of 300 degrees or less to distill various water such as seawater. Various energy storage cycle coalescing engines that use various heat, electricity, and cold supply facilities for water.   For rotation output dedicated bearings (80) and thrust bearings (80a) that support turbine blade cross section (4D) applications, excess heat is recovered and stored at various temperatures (52d) of 300 degrees or less to distill various water such as seawater. Various energy storage cycle coalescing engines for supplying various types of heat, electricity and cold energy used as water and salt.   Bearings (80) and thrust bearings (80a) corresponding to the turbine blade cross section (4D) application are provided, and the amount of compressed air heat (28b) is recovered by the intake air (28a) and the compression heat is recovered by the heat pump (1G). Various energy storage cycle coalescing engines for heat, electricity and cold supply facilities.   A bearing (80) thrust bearing (80a) corresponding to the application of the turbine blade cross section (4D) is provided, and the heat pump (1G) collects the mercury exhaust heat quantity (5A) + compressed air heat quantity (28b) by the intake air (28a). ) Various energy storage cycle coalescing engines that use various heat, electricity and cold supply facilities to recover compression heat.   A bearing (80) thrust bearing (80a) corresponding to the use of the turbine blade cross section (4D) is provided, and the amount of compressed air heat (28b) is recovered by the intake air (28a) and compressed by the heat pump (1G) at 500 to 1000 degrees. Various energy storage cycle coalescing engines to provide various heat, electricity and cold supply facilities for heat recovery.   A bearing (80) thrust bearing (80a) corresponding to the application of the turbine blade cross section (4D) is provided, and the heat pump (1G) collects the mercury exhaust heat quantity (5A) + compressed air heat quantity (28b) by the intake air (28a). ) Various energy storage cycle coalescing engines that use various heat, electricity, and cold supply facilities to recover heat at a compression of 500 to 1000 degrees.   A bearing (80) thrust bearing (80a) corresponding to the use of the turbine blade cross section (4D) is provided, and the amount of compressed air heat (28b) is recovered by the intake air (28a) and compressed by the heat pump (1G) at 500 to 1000 degrees. Various energy storage cycle coalescing engines that use various heat, electricity, and cold supply facilities to recover the heat and drive all rotor blade water turbines.   A bearing (80) thrust bearing (80a) corresponding to the use of the turbine blade cross section (4D) is provided, and the amount of compressed air heat (28b) is recovered by the intake air (28a) and compressed by the heat pump (1G) at 500 to 1000 degrees. Various energy storage cycle coalescing engines that supply various heat, electricity, and cold energy to recover the heat and drive all turbine blade turbines.   A bearing (80) thrust bearing (80a) corresponding to the use of the turbine blade cross section (4D) is provided, and the amount of compressed air heat (28b) is recovered by the intake air (28a) and compressed by the heat pump (1G) at 500 to 1000 degrees. Various energy storage cycle coalescing engines that use various heat, electricity, and cold supply equipment to recover heat and drive all rotor blade gas turbines.   Piping water (52a) pipes made of carbon fiber, etc. that have been reduced in weight to high pressure, such as flying wings (38b) and flying wings (38c) on the turbine blade cross-section (4D), which are heated at the time of flight. Various energy storage cycle coalescing engines that recover heat from the high-pressure and light-weight container and provide various heat, electricity, and cold supply facilities provided with a bearing (80) and a thrust bearing (80a) corresponding to the application during stoppage.   A superheated steam (50) pipe made of carbon fiber, etc., that has been reduced in weight to high pressure on all parts of the turbine blade cross section (4D), such as the flying wing (38b) and the flying tail (38c), which have a high flight speed when returning to the earth. Various energy storage cycle coalescing engines with various heat, electricity, and cold supply facilities provided with piping (80) and thrust bearings (80a) that correspond to the application during piping, recovering heat from high-pressure lightweight containers .   A high-temperature mercury (1d) tube that has been reduced in weight to high pressure with carbon fiber or the like is applied to all parts that become hot when returning to the earth at the flight speed, such as the flight wing (38b) and the flight tail (38c) of the turbine blade cross section (4D). Various energy storage cycle coalescing engines with various heat, electricity, and cold supply facilities provided with piping (80) and thrust bearings (80a) that correspond to the application during piping, recovering heat from high-pressure lightweight containers .   A combustion gas pipe reduced in weight and increased in pressure by carbon fiber or the like is piped on all the portions of the turbine blade cross section (4D), such as the flying wing (38b) and the flying tail wing (38c) that are heated at the flight speed, such as the flying tail (38c). Various energy storage cycle coalescing engine that recovers heat from the high-pressure light weight container and uses various bearings (80) and thrust bearings (80a) corresponding to the application to provide various heat, electricity and cold supply facilities.   Piping water (52a) pipes that have been reduced in weight to high pressure with carbon nanotubes, etc., on all parts of the turbine blade cross section (4D), such as flying wings (38b) and flying tail wings (38c) that are at high speed when returning to the earth. Various energy storage cycle coalescing engines that recover heat from the high-pressure and light-weight container and provide various heat, electricity, and cold supply facilities provided with a bearing (80) and a thrust bearing (80a) corresponding to the application during stoppage.   The superheated steam (50) tube, which has been reduced in weight to high pressure with carbon nanotubes, etc., is applied to all the parts that become hot at the time of return to the earth, such as the flight wing (38b) and the flight tail (38c) of the turbine blade cross section (4D). Various energy storage cycle coalescing engines with various heat, electricity, and cold supply facilities provided with piping (80) and thrust bearings (80a) that correspond to the application during piping, recovering heat from high-pressure lightweight containers .   A high-temperature mercury (1d) tube that has been reduced in weight to high pressure with carbon nanotubes, etc., is applied to all parts that become hot at the time of return to the earth, such as the flying wing (38b) and the flying tail (38c) of the turbine blade cross section (4D). Various energy storage cycle coalescing engines with various heat, electricity, and cold supply facilities provided with piping (80) and thrust bearings (80a) that correspond to the application during piping, recovering heat from high-pressure lightweight containers .   A combustion gas pipe that has been reduced in weight to high pressure with carbon nanotubes, etc., is piped to all 0 parts of the turbine blade cross section (4D), such as the flying wing (38b) and flying tail wing (38c), which are at high speed when returning to the earth. Various energy storage cycle coalescence engines that recover heat from a high-pressure lightweight container and provide various heat, electricity, and cold supply facilities provided with a bearing (80) and thrust bearing (80a) corresponding to the application during stoppage.   The combustion air (49) is recovered by the intake air (28a) at the turbine blade cross section (4E), and is recovered by the heat pump (1G) as compressed to 500 to 1000 degrees to drive the entire blade water turbine and stop. Inside, various energy storage cycle coalescence engine with various heat, electricity and cold supply facilities provided with bearing (80) and thrust bearing (80a) corresponding to the application.   The combustion air (49) recovers the amount of heat from the intake air (28a) on the turbine blade cross section (4E), and the heat pump (1G) recovers the heat to 500-1000 degrees C, etc. Inside, various energy storage cycle coalescence engine with various heat, electricity and cold supply facilities provided with bearing (80) and thrust bearing (80a) corresponding to the application.   The combustion air (49) recovers the amount of heat from the intake air (28a) in the turbine blade cross section (4E), and the heat pump (1G) recovers the heat to 500-1000 degrees C, etc. Inside, various energy storage cycle coalescence engine with various heat, electricity and cold supply facilities provided with bearing (80) and thrust bearing (80a) corresponding to the application.   The combustion air (49) recovers the amount of heat by the intake air (28a) in the turbine blade cross section (4E) and is recovered by the heat pump (1G) as a compression of 500 to 1000 degrees to drive the combined engine injection section (79K). , Various energy storage cycle coalescence engine with various heat, electricity and cold supply facilities provided with bearing (80) thrust bearing (80a) corresponding to the application during stoppage.   Water jet (79M) all-blade mercury turbine recovers heat quantity of combustion gas (49) by intake air (28a) of turbine blade cross section (4E), and recovers heat as compression 500-1000 degrees by heat pump (1G) Various energy storage cycle coalescence engines that are equipped with various heat, electricity, and cold supply facilities provided with a bearing (80) and a thrust bearing (80a) corresponding to the application.   The compressed air calorie (28b) is recovered by the intake air (28a) in the turbine blade cross section (4E), and is recovered by the heat pump (1G) to a compression of 500 to 1000 degrees or the like to drive the combined engine injection unit (79K). , Various energy storage cycle coalescence engine with various heat, electricity and cold supply facilities provided with bearing (80) thrust bearing (80a) corresponding to the application during stoppage.   Compressed air calorie (28b) is recovered by intake air (28a) at the turbine blade cross section (4E), and heat is recovered to 500-1000 ° C. by a heat pump (1G), and the water jet (79M) is driven and stopped. Inside, various energy storage cycle coalescence engine with various heat, electricity and cold supply facilities provided with bearing (80) and thrust bearing (80a) corresponding to the application.   The turbine blade cross section (4D) full blade combustion part (32X) vertical all blade gas turbine (8A) and other application-compatible bearings (80) thrust bearings (80a) are provided to drive various automobiles. Various energy conservation cycle coalescence engine.   The turbine blade cross section (4D) full rotor blade combustion section (32Y) vertical all rotor blade gas turbine (8A) and other various types of automobiles that are driven by providing a bearing (80) thrust bearing (80a) corresponding to the application. Various energy conservation cycle coalescence engine.   Combined engine combustion part (31Y) turbine blade cross section (4D) turbine blade cross section (4D) gas turbine (8a) and other various types of energy for various automobiles to be driven by providing bearings (80) thrust bearings (80a) for applications Conservation cycle coalescence organization.   Combined engine combustion section (31X) full blade impeller gas turbine (8a) with turbine blade cross section (4D), and various other energy sources for various automobiles to be driven by providing a bearing (80) thrust bearing (80a) for the application Conservation cycle coalescence organization.   The turbine blade cross section (4D) full blade combustion section (32X) vertical all blade gas turbine (8A) and other application-compatible bearing (80) thrust bearing (80a) cold energy recovery means (3C) Various energy conservation cycle coalescing engines for various automobiles.   The turbine blade cross section (4D) full blade combustion section (32Y) vertical all blade gas turbine (8A) and other bearings (80) thrust bearings (80a) and cold recovery means (3C) are also provided. Various energy conservation cycle coalescing engines for various automobiles.   Combined engine combustion section (31Y) full rotor blade propeller gas turbine (8a) with turbine blade cross section (4D) and other various types of bearings (80), thrust bearings (80a), and cold recovery means (3C) to be driven Various energy conservation cycle coalescence engine for automobiles.   Combined engine combustion section (31X) full blade impeller gas turbine (8a) with turbine blade cross section (4D) and other various types of bearings (80), thrust bearings (80a), and cold recovery means (3C) that are used for driving Various energy conservation cycle coalescence engine for automobiles.   The turbine blade cross section (4D) full blade combustion section (32X) vertical all blade gas turbine (8A) and other application-compatible bearings (80) thrust bearing (80a) cold heat recovery device (103) Various energy conservation cycle coalescing engines for various automobiles.   Turbine blade cross section (4D) all-blade combustion section (32Y) vertical all-blade gas turbine (8A) and other application-compatible bearing (80) thrust bearing (80a) cold heat recovery device (103) Various energy conservation cycle coalescing engines for various automobiles.   Combined engine combustion section (31X) full blade impeller gas turbine (8a) with turbine blade cross section (4D) and various bearings (80) thrust bearings (80a) cold heat recovery device (103) for use Various energy conservation cycle coalescence engine for automobiles.   Combined engine combustion section (31Y) full blade impeller gas turbine (8a) with turbine blade cross section (4D) and other various types of bearings (80) thrust bearings (80a) and cold recovery devices (103) that are driven Various energy conservation cycle coalescence engine for various automobiles.   Turbine blade cross section (4D) full blade combustion part (32X) vertical all blade gas turbine (8A) and other application-compatible bearing (80) thrust bearing (80a) cold heat recovery device (103) (103) Various energy conservation cycle coalescing engines that are installed and driven by various automobiles.   Turbine blade cross section (4D) all blade combusting part (32Y) vertical all blade gas turbine (8A) and other application-compatible bearing (80) thrust bearing (80a) cold heat recovery device (103) (103) Various energy conservation cycle coalescing engines that are installed and driven by various automobiles.   Combined engine combustion section (31X) full blade impeller gas turbine (8a) with turbine blade cross section (4D) and other application-compatible bearing (80) thrust bearing (80a) cold recovery device (103) (103) Various energy conservation cycle coalescing engines for various types of automobiles to be driven.   Combined engine combustion part (31Y) turbine blade cross section gas turbine (8a) with turbine blade cross section (4D) and other application-compatible bearing (80) thrust bearing (80a) cold recovery device (103) (103) Various energy conservation cycle coalescing engines for various types of automobiles to be driven.   Combined engine combustion section (31X) full blade impeller gas turbine (8a) with turbine blade cross section (4D) and other application-compatible bearing (80) thrust bearing (80a) cold recovery device (103) (103) Various energy storage cycle coalescing engines as various automobiles driven by 24-300 MPa combustion gas (49) around 150 degrees Celsius.   Combined engine combustion part (31Y) turbine blade cross section gas turbine (8a) with turbine blade cross section (4D) and other application-compatible bearing (80) thrust bearing (80a) cold recovery device (103) (103) Various energy storage cycle coalescing engines as various automobiles driven by 24-300 MPa combustion gas (49) around 150 degrees Celsius.   Turbine blade cross section (4D) full blade combustion part (32X) vertical all blade gas turbine (8A) and other application-compatible bearing (80) thrust bearing (80a) cold heat recovery device (103) (103) Various energy storage cycle coalescing engines that are installed and driven by various types of automobiles that are driven by 24-300 MPa combustion gas (49) around 150 degrees Celsius.   Turbine blade cross section (4D) all blade combusting part (32Y) vertical all blade gas turbine (8A) and other application-compatible bearing (80) thrust bearing (80a) cold heat recovery device (103) (103) Various energy storage cycle coalescing engines that are installed and driven by various types of automobiles that are driven by 24-300 MPa combustion gas (49) around 150 degrees Celsius.   Combined engine combustion section (31X) full blade impeller gas turbine (8a) with turbine blade cross section (4D) and other application-compatible bearing (80) thrust bearing (80a) cold recovery device (103) (103) Various energy storage cycle coalescing engines as various automobiles driven by 24-300 MPa combustion gas (49) around 200 degrees Celsius.   Combined engine combustion part (31Y) turbine blade cross section gas turbine (8a) with turbine blade cross section (4D) and other application-compatible bearing (80) thrust bearing (80a) cold recovery device (103) (103) Various energy storage cycle coalescing engines as various automobiles driven by 24-300 MPa combustion gas (49) around 200 degrees Celsius.   Turbine blade cross section (4D) full blade combustion part (32X) vertical all blade gas turbine (8A) and other application-compatible bearing (80) thrust bearing (80a) cold heat recovery device (103) (103) Various energy storage cycle coalescing engines that are installed and driven by various types of automobiles driven by 24-300 MPa combustion gas (49) around 200 degrees Celsius.   Turbine blade cross section (4D) all blade combusting part (32Y) vertical all blade gas turbine (8A) and other application-compatible bearing (80) thrust bearing (80a) cold heat recovery device (103) (103) Various energy storage cycle coalescing engines that are installed and driven by various types of automobiles driven by 24-300 MPa combustion gas (49) around 200 degrees Celsius.   Turbine blade cross section (4D) full blade combustion part (32X) vertical all blade gas turbine (8A) and other application-compatible bearing (80) thrust bearing (80a) cold heat recovery device (103) (103) Various energy storage cycle coalescing engines that are installed and driven by various types of automobiles driven by 24-300 MPa combustion gas (49) around 300 degrees Celsius.   Turbine blade cross section (4D) all blade combusting part (32Y) vertical all blade gas turbine (8A) and other application-compatible bearing (80) thrust bearing (80a) cold heat recovery device (103) (103) Various energy storage cycle coalescing engines that are installed and driven by various types of automobiles driven by 24-300 MPa combustion gas (49) around 300 degrees Celsius.   Combined engine combustion section (31X) full blade impeller gas turbine (8a) with turbine blade cross section (4D) and other application-compatible bearing (80) thrust bearing (80a) cold recovery device (103) (103) Various energy storage cycle coalescing engines as various automobiles driven by 24-300 MPa combustion gas (49) around 300 degrees Celsius.   Combined engine combustion part (31Y) turbine blade cross section gas turbine (8a) with turbine blade cross section (4D) and other application-compatible bearing (80) thrust bearing (80a) cold recovery device (103) (103) Various energy storage cycle coalescing engines as various automobiles driven by 24-300 MPa combustion gas (49) around 300 degrees Celsius.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31X) of the turbine blade cross section (4D), and the high-temperature mercury (1d) is driven by a high-pressure turbine at a critical temperature or less to reduce the amount of heat consumed by about 1. / Energy conservation cycle coalescence engine for various automobiles such as 72.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and the high-temperature mercury (1d) is driven by a high-pressure turbine below the critical temperature to reduce the amount of heat consumed by about 1 / Energy conservation cycle coalescence engine for various automobiles such as 72.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32X) of the turbine blade cross section (4D), and the high-temperature mercury (1d) is driven by a high-pressure turbine below the critical temperature to reduce the amount of heat consumed. Various energy storage cycle coalescing engines that are 1/72 etc. various automobiles.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32Y) of the turbine blade cross section (4D), and the high-temperature mercury (1d) is driven by a high-pressure turbine below the critical temperature to reduce the amount of heat consumed. Various energy storage cycle coalescing engines that are 1/72 etc. various automobiles.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32X) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at 1000 degrees Celsius or less to reduce the amount of heat consumed. Various energy conservation cycle coalescing engines, which are various automobiles that are reduced to approximately 1/72.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32Y) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at 1000 degrees Celsius or less to reduce the amount of heat consumed. Various energy conservation cycle coalescing engines, which are various automobiles that are reduced to approximately 1/72.   A combined bearing (80) thrust bearing (80a) for the combined engine combustion section (31X) of the turbine blade cross section (4D) is provided, and high-temperature mercury (1d) is driven by a high-pressure turbine at 1000 degrees Celsius or less to reduce heat consumption. Various energy storage cycle coalescing engines that are 1/72 etc. various automobiles.   A combined bearing (80) thrust bearing (80a) for the combined engine combustion section (31Y) of the turbine blade cross section (4D) is provided, and high-temperature mercury (1d) is driven by a high-pressure turbine at 1000 degrees Celsius or less to reduce the amount of heat consumed. Various energy storage cycle coalescing engines that are 1/72 etc. various automobiles.   A combined bearing (80) thrust bearing (80a) is installed in the combined engine combustion section (31X) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at a temperature of 800 degrees Celsius or less to reduce heat consumption. Various energy storage cycle coalescing engines that are 1/72 etc. various automobiles.   A combined bearing (80) thrust bearing (80a) is installed in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at 800 degrees Celsius or less to reduce the amount of heat consumed. Various energy storage cycle coalescing engines that are 1/72 etc. various automobiles.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32X) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at 800 degrees Celsius or less to reduce heat consumption. Various energy conservation cycle coalescing engines, which are various automobiles that are reduced to approximately 1/72.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32Y) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at 800 degrees Celsius or less to reduce the amount of heat consumed. Various energy conservation cycle coalescing engines, which are various automobiles that are reduced to approximately 1/72.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32X) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at 600 degrees Celsius or less to reduce the amount of heat consumed. Various energy conservation cycle coalescing engines, which are various automobiles that are reduced to approximately 1/72.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32Y) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at 600 degrees Celsius or less to reduce the amount of heat consumed. Various energy conservation cycle coalescing engines, which are various automobiles that are reduced to approximately 1/72.   A combined bearing (80) thrust bearing (80a) is installed in the combined engine combustion section (31X) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at 600 degrees Celsius or less to reduce heat consumption. Various energy storage cycle coalescing engines that are 1/72 etc. various automobiles.   A combined bearing (80) thrust bearing (80a) is installed in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at 600 degrees Celsius or less to reduce heat consumption. Various energy storage cycle coalescing engines that are 1/72 etc. various automobiles.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31X) of the turbine blade cross section (4D), and the high-temperature water (52b) is driven at a high pressure turbine below the critical temperature to reduce the amount of heat consumed by about 1. / 539 etc. Various energy conservation cycle coalescence engine made into various automobiles.   A combined bearing (80) thrust bearing (80a) corresponding to the application is provided in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and the high-temperature water (52b) is driven by a high-pressure turbine at a critical temperature or less to reduce the amount of heat consumed by about 1. / 539 etc. Various energy conservation cycle coalescence engine made into various automobiles.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32X) of the turbine blade cross section (4D), and the high temperature water (52b) is driven by a high pressure turbine below the critical temperature to reduce the amount of heat consumed. Various energy conservation cycle coalescing engines that are 1/539 etc.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the turbine blade cross section (4Y) of the turbine blade cross section (4D), and the high temperature water (52b) is driven by a high pressure turbine below the critical temperature to reduce the amount of heat consumed. Various energy conservation cycle coalescing engines that are 1/539 etc.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32X) of the turbine blade cross section (4D), and the high-pressure turbine is driven by high-temperature water (52b) to reduce the amount of heat consumed by approximately 1/539, etc. Various energy conservation cycle coalescing engines for various automobiles.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire rotor blade combustion section (32Y) of the turbine blade cross section (4D), and the high-pressure turbine is driven with high-temperature water (52b) to reduce the heat consumption by approximately 1/539, etc. Various energy conservation cycle coalescing engines for various automobiles.   Provide a bearing (80) thrust bearing (80a) corresponding to the application in the combined engine combustion section (31X) of the turbine blade cross section (4D) and drive the high-pressure turbine with high-temperature water (52b) to reduce the heat consumption to approximately 1/539, etc. Various energy conservation cycle coalescing engines for various automobiles.   Provide a bearing (80) thrust bearing (80a) corresponding to the application in the combined engine combustion section (31Y) of the turbine blade cross section (4D) and drive the high-pressure turbine with high-temperature water (52b) to reduce the heat consumption to approximately 1/539, etc. Various energy conservation cycle coalescing engines for various automobiles.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31X) of the turbine blade cross section (4D), and the high-pressure turbine is driven with high-temperature water (52b) to generate the same-pressure output at the atmospheric pressure with steam. Various energy storage cycle coalescing engines for various automobiles with 1700 times kg weight m / sec.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and high-pressure turbine driving is performed with high-temperature water (52b) to generate the same pressure output at atmospheric pressure as steam. Various energy storage cycle coalescing engines for various automobiles with 1700 times kg weight m / sec.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the turbine blade cross section (4D) of the turbine blade cross section (4D), and a high-pressure turbine is driven with high-temperature water (52b) to drive the atmospheric pressure at the same speed output by steam. Various energy conservation cycle coalescing engines that are 1700 times kg weight m / sec.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the turbine blade cross section (4Y) of the turbine blade cross section (4D), and high-pressure turbine driving is performed with high-temperature water (52b) to drive the atmospheric pressure at the same speed output by steam. Various energy conservation cycle coalescing engines that are 1700 times kg weight m / sec.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the turbine blade cross section (4D) of the turbine blade cross section (4D), and a high-pressure turbine is driven by high-temperature mercury (1d) to drive the atmospheric pressure at the same speed by steam. Various energy storage cycle coalescing engines with various automobiles to 23,000 times kg weight m / sec.   Provided bearing (80) thrust bearing (80a) corresponding to application in all rotor blade combustion section (32Y) of turbine blade cross section (4D), high-pressure turbine driven with high-temperature mercury (1d), steam-driven at atmospheric pressure and same speed output Various energy storage cycle coalescing engines with various automobiles to 23,000 times kg weight m / sec.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31X) of the turbine blade cross section (4D), and high-pressure turbine driving is performed with high-temperature mercury (1d), and the atmospheric pressure and the same speed output is steam-driven. Various energy storage cycle coalescing engines for various automobiles with 23,000 times kg weight m / sec.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and the high-pressure turbine is driven with high-temperature mercury (1d) to output the same pressure output at the atmospheric pressure with steam. Various energy storage cycle coalescing engines for various automobiles with 23,000 times kg weight m / sec.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31X) of the turbine blade cross section (4D), and high-pressure turbine driving is performed with high-temperature mercury (1d), and the atmospheric pressure and the same speed output is steam-driven. Various energy conservation cycle coalescing engines that make gravity acceleration to 23,000 times kg weight m / second and supply equipment for additional heat, electricity and cold.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and the high-pressure turbine is driven with high-temperature mercury (1d) to output the same pressure output at the atmospheric pressure with steam. Various energy conservation cycle coalescing engines, which are made into various automobiles that use 23,000 times kg weight m / sec as gravity acceleration and supply equipment for additional heat, electricity and cold.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the turbine blade cross section (4D) of the turbine blade cross section (4D), and a high-pressure turbine is driven by high-temperature mercury (1d) to drive the atmospheric pressure at the same speed by steam. Various energy storage cycle coalescence engine that makes gravity acceleration to 23,000 times kg weight m / second of additional heat, electricity and cold supply equipment.   Provided bearing (80) thrust bearing (80a) corresponding to application in all rotor blade combustion section (32Y) of turbine blade cross section (4D), high-pressure turbine driven with high-temperature mercury (1d), steam-driven at atmospheric pressure and same speed output Various energy storage cycle coalescence engine that makes gravity acceleration to 23,000 times kg weight m / second of additional heat, electricity and cold supply equipment.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the turbine blade cross section (4D) of the turbine blade cross section (4D), and a high-pressure turbine is driven by high-temperature mercury (1d) to drive the atmospheric pressure at the same speed by steam. Various energy conservation cycle coalescing engines to make various ships equipped with gravity acceleration addition at 23,000 times kg weight m / sec.   Provided bearing (80) thrust bearing (80a) corresponding to application in all rotor blade combustion section (32Y) of turbine blade cross section (4D), high-pressure turbine driven with high-temperature mercury (1d), steam-driven at atmospheric pressure and same speed output Various energy conservation cycle coalescing engines to make various ships equipped with gravity acceleration addition at 23,000 times kg weight m / sec.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31X) of the turbine blade cross section (4D), and high-pressure turbine driving is performed with high-temperature mercury (1d), and the atmospheric pressure and the same speed output is steam-driven. Various energy conservation cycle coalescing engines to make various ships equipped with gravity acceleration addition at 23,000 times kg weight m / sec.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and the high-pressure turbine is driven with high-temperature mercury (1d) to output the same pressure output at the atmospheric pressure with steam. Various energy conservation cycle coalescing engines to make various ships equipped with gravity acceleration addition at 23,000 times kg weight m / sec.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31X) of the turbine blade cross section (4D), and high-pressure turbine driving is performed with high-temperature mercury (1d), and the atmospheric pressure and the same speed output is steam-driven. Various energy conservation cycle coalescing engines to make various airplanes equipped with gravity acceleration addition at 23,000 times kg weight m / sec.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and the high-pressure turbine is driven with high-temperature mercury (1d) to output the same pressure output at the atmospheric pressure with steam. Various energy conservation cycle coalescing engines to make various airplanes equipped with gravity acceleration addition at 23,000 times kg weight m / sec.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the turbine blade cross section (4D) of the turbine blade cross section (4D), and a high-pressure turbine is driven by high-temperature mercury (1d) to drive the atmospheric pressure at the same speed by steam. Various energy storage cycle coalescing engines to make various airplanes equipped with gravity acceleration addition at 23,000 times kg weight m / sec.   Provided bearing (80) thrust bearing (80a) corresponding to application in all rotor blade combustion section (32Y) of turbine blade cross section (4D), high-pressure turbine driven with high-temperature mercury (1d), steam-driven at atmospheric pressure and same speed output Various energy storage cycle coalescing engines to make various airplanes equipped with gravity acceleration addition at 23,000 times kg weight m / sec.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the turbine blade cross section (4D) of the turbine blade cross section (4D), and a high-pressure turbine is driven with high-temperature water (52b) to drive the atmospheric pressure at the same speed output by steam. 1700 times kg weight m / sec. Various energy conservation cycle coalescing engines to make various airplanes equipped with gravity acceleration addition.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the turbine blade cross section (4Y) of the turbine blade cross section (4D), and high-pressure turbine driving is performed with high-temperature water (52b) to drive the atmospheric pressure at the same speed output by steam. 1700 times kg weight m / sec. Various energy conservation cycle coalescing engines to make various airplanes equipped with gravity acceleration addition.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31X) of the turbine blade cross section (4D), and the high-pressure turbine is driven with high-temperature water (52b) to generate the same-pressure output at the atmospheric pressure with steam. Various energy conservation cycle coalescing engines to make various airplanes equipped with gravity acceleration addition at 1700 times kg weight m / sec.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and high-pressure turbine driving is performed with high-temperature water (52b) to generate the same pressure output at atmospheric pressure as steam. Various energy conservation cycle coalescing engines to make various airplanes equipped with gravity acceleration addition at 1700 times kg weight m / sec.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31X) of the turbine blade cross section (4D), and the high-pressure turbine is driven with high-temperature water (52b) to generate the same-pressure output at the atmospheric pressure with steam. Various energy conservation cycle coalescing engines that make various ships equipped with gravity acceleration addition at 1700 times kg weight m / sec.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and high-pressure turbine driving is performed with high-temperature water (52b) to generate the same pressure output at atmospheric pressure as steam. Various energy conservation cycle coalescing engines that make various ships equipped with gravity acceleration addition at 1700 times kg weight m / sec.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the turbine blade cross section (4D) of the turbine blade cross section (4D), and a high-pressure turbine is driven with high-temperature water (52b) to drive the atmospheric pressure at the same speed output by steam. 1700 times kg weight m / sec. Various energy conservation cycle coalescing engines to make various ships equipped with gravity acceleration addition.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the turbine blade cross section (4Y) of the turbine blade cross section (4D), and high-pressure turbine driving is performed with high-temperature water (52b) to drive the atmospheric pressure at the same speed output by steam. 1700 times kg weight m / sec. Various energy conservation cycle coalescing engines to make various ships equipped with gravity acceleration addition.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the turbine blade cross section (4D) of the turbine blade cross section (4D), and a high-pressure turbine is driven with high-temperature water (52b) to drive the atmospheric pressure at the same speed output by steam. An energy conservation cycle coalescence engine that makes gravity acceleration to 1700 times the weight of m / second and supplies various additional heat, electricity and cold.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the turbine blade cross section (4Y) of the turbine blade cross section (4D), and high-pressure turbine driving is performed with high-temperature water (52b) to drive the atmospheric pressure at the same speed output by steam. 1700 times kg weight m / sec. Various energy storage cycle coalescing engines that make use of various heat, electricity and cold supply facilities with additional gravitational acceleration.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31X) of the turbine blade cross section (4D), and the high-pressure turbine is driven with high-temperature water (52b) to generate the same-pressure output at the atmospheric pressure with steam. Various energy storage cycle coalescing engines that use various heat, electricity, and cold supply facilities with gravity acceleration added to 1700 times kg weight m / sec.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and high-pressure turbine driving is performed with high-temperature water (52b) to generate the same pressure output at atmospheric pressure as steam. Various energy storage cycle coalescing engines that use various heat, electricity, and cold supply facilities with gravity acceleration added to 1700 times kg weight m / sec.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31X) of the turbine blade cross section (4D), and the high-temperature mercury (1d) is driven by a high-pressure turbine at a critical temperature or less to reduce the amount of heat consumed by about 1. / Energy storage cycle coalescing engine that adds gravity acceleration to 72 etc. to make various heat, electricity and cold supply facilities.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and the high-temperature mercury (1d) is driven by a high-pressure turbine below the critical temperature to reduce the amount of heat consumed by about 1 / Energy storage cycle coalescing engine that adds gravity acceleration to 72 etc. to make various heat, electricity and cold supply facilities.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32X) of the turbine blade cross section (4D), and the high-temperature mercury (1d) is driven by a high-pressure turbine below the critical temperature to reduce the amount of heat consumed. Various energy storage cycle coalescing engine that adds gravitational acceleration to 1/72 etc. to provide various heat, electricity and cold supply facilities.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32Y) of the turbine blade cross section (4D), and the high-temperature mercury (1d) is driven by a high-pressure turbine below the critical temperature to reduce the amount of heat consumed. Various energy storage cycle coalescing engine that adds gravitational acceleration to 1/72 etc. to provide various heat, electricity and cold supply facilities.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32X) of the turbine blade cross section (4D), and the high-temperature mercury (1d) is driven by a high-pressure turbine below the critical temperature to reduce the amount of heat consumed. Various energy conservation cycle coalescing engines to make various ships by adding gravity acceleration to 1/72 etc.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32Y) of the turbine blade cross section (4D), and the high-temperature mercury (1d) is driven by a high-pressure turbine below the critical temperature to reduce the amount of heat consumed. Various energy conservation cycle coalescing engines to make various ships by adding gravity acceleration to 1/72 etc.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31X) of the turbine blade cross section (4D), and the high-temperature mercury (1d) is driven by a high-pressure turbine at a critical temperature or less to reduce the amount of heat consumed by about 1. / Energy conservation cycle coalescing engine to add gravity acceleration to 72 etc. to make various ships.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and the high-temperature mercury (1d) is driven by a high-pressure turbine below the critical temperature to reduce the amount of heat consumed by about 1 / Energy conservation cycle coalescing engine to add gravity acceleration to 72 etc. to make various ships.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31X) of the turbine blade cross section (4D), and the high-temperature mercury (1d) is driven by a high-pressure turbine at a critical temperature or less to reduce the amount of heat consumed by about 1. / Energy conservation cycle coalescing engine to make various airplanes by adding gravity acceleration to 72 etc.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and the high-temperature mercury (1d) is driven by a high-pressure turbine below the critical temperature to reduce the amount of heat consumed by about 1 / Energy conservation cycle coalescing engine to make various airplanes by adding gravity acceleration to 72 etc.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32X) of the turbine blade cross section (4D), and the high-temperature mercury (1d) is driven by a high-pressure turbine below the critical temperature to reduce the amount of heat consumed. Various energy conservation cycle coalescing engines to make various airplanes by adding gravity acceleration to 1/72 etc.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32Y) of the turbine blade cross section (4D), and the high-temperature mercury (1d) is driven by a high-pressure turbine below the critical temperature to reduce the amount of heat consumed. Various energy conservation cycle coalescing engines to make various airplanes by adding gravity acceleration to 1/72 etc.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32X) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at 1000 degrees Celsius or less to reduce the amount of heat consumed. Various energy conservation cycle coalescing engines to make various airplanes with gravity acceleration added to about 1/72 etc.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32Y) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at 1000 degrees Celsius or less to reduce the amount of heat consumed. Various energy conservation cycle coalescing engines to make various airplanes with gravity acceleration added to about 1/72 etc.   A combined bearing (80) thrust bearing (80a) for the combined engine combustion section (31X) of the turbine blade cross section (4D) is provided, and high-temperature mercury (1d) is driven by a high-pressure turbine at 1000 degrees Celsius or less to reduce heat consumption. Various energy conservation cycle coalescing engines to make various airplanes with gravity acceleration added to 1/72 etc.   A combined bearing (80) thrust bearing (80a) for the combined engine combustion section (31Y) of the turbine blade cross section (4D) is provided, and high-temperature mercury (1d) is driven by a high-pressure turbine at 1000 degrees Celsius or less to reduce the amount of heat consumed. Various energy conservation cycle coalescing engines to make various airplanes with gravity acceleration added to 1/72 etc.   A combined bearing (80) thrust bearing (80a) for the combined engine combustion section (31X) of the turbine blade cross section (4D) is provided, and high-temperature mercury (1d) is driven by a high-pressure turbine at 1000 degrees Celsius or less to reduce heat consumption. Various energy conservation cycle coalescing engines to make various ships with gravity acceleration added to 1/72 etc.   A combined bearing (80) thrust bearing (80a) for the combined engine combustion section (31Y) of the turbine blade cross section (4D) is provided, and high-temperature mercury (1d) is driven by a high-pressure turbine at 1000 degrees Celsius or less to reduce the amount of heat consumed. Various energy conservation cycle coalescing engines to make various ships with gravity acceleration added to 1/72 etc.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32X) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at 1000 degrees Celsius or less to reduce the amount of heat consumed. Various energy conservation cycle coalescing engines that make various ships with gravity acceleration added to about 1/72 etc.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32Y) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at 1000 degrees Celsius or less to reduce the amount of heat consumed. Various energy conservation cycle coalescing engines that make various ships with gravity acceleration added to about 1/72 etc.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32X) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at 1000 degrees Celsius or less to reduce the amount of heat consumed. Various energy storage cycle coalescing engines that provide various heat, electricity and cold supply facilities with gravity acceleration added to about 1/72.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32Y) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at 1000 degrees Celsius or less to reduce the amount of heat consumed. Various energy storage cycle coalescing engines that provide various heat, electricity and cold supply facilities with gravity acceleration added to about 1/72.   A combined bearing (80) thrust bearing (80a) for the combined engine combustion section (31X) of the turbine blade cross section (4D) is provided, and high-temperature mercury (1d) is driven by a high-pressure turbine at 1000 degrees Celsius or less to reduce heat consumption. Various energy storage cycle coalescence engine that uses various heat, electricity and cold supply facilities with gravity acceleration added to 1/72 etc.   A combined bearing (80) thrust bearing (80a) for the combined engine combustion section (31Y) of the turbine blade cross section (4D) is provided, and high-temperature mercury (1d) is driven by a high-pressure turbine at 1000 degrees Celsius or less to reduce the amount of heat consumed. Various energy storage cycle coalescence engine that uses various heat, electricity and cold supply facilities with gravity acceleration added to 1/72 etc.   A combined bearing (80) thrust bearing (80a) is installed in the combined engine combustion section (31X) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at a temperature of 800 degrees Celsius or less to reduce heat consumption. Various energy storage cycle coalescence engine that uses various heat, electricity and cold supply facilities with gravity acceleration added to 1/72 etc.   A combined bearing (80) thrust bearing (80a) is installed in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at 800 degrees Celsius or less to reduce the amount of heat consumed. Various energy storage cycle coalescence engine that uses various heat, electricity and cold supply facilities with gravity acceleration added to 1/72 etc.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32X) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at 800 degrees Celsius or less to reduce heat consumption. Various energy storage cycle coalescing engines that provide various heat, electricity and cold supply facilities with gravity acceleration added to about 1/72.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32Y) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at 800 degrees Celsius or less to reduce the amount of heat consumed. Various energy storage cycle coalescing engines that provide various heat, electricity and cold supply facilities with gravity acceleration added to about 1/72.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32X) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at 800 degrees Celsius or less to reduce heat consumption. Various energy conservation cycle coalescing engines that make various ships with gravity acceleration added to about 1/72 etc.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32Y) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at 800 degrees Celsius or less to reduce the amount of heat consumed. Various energy conservation cycle coalescing engines that make various ships with gravity acceleration added to about 1/72 etc.   A combined bearing (80) thrust bearing (80a) is installed in the combined engine combustion section (31X) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at a temperature of 800 degrees Celsius or less to reduce heat consumption. Various energy conservation cycle coalescing engines to make various ships with gravity acceleration added to 1/72 etc.   A combined bearing (80) thrust bearing (80a) is installed in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at 800 degrees Celsius or less to reduce the amount of heat consumed. Various energy conservation cycle coalescing engines to make various ships with gravity acceleration added to 1/72 etc.   A combined bearing (80) thrust bearing (80a) is installed in the combined engine combustion section (31X) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at a temperature of 800 degrees Celsius or less to reduce heat consumption. Various energy conservation cycle coalescing engines to make various airplanes with gravity acceleration added to 1/72 etc.   A combined bearing (80) thrust bearing (80a) is installed in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at 800 degrees Celsius or less to reduce the amount of heat consumed. Various energy conservation cycle coalescing engines to make various airplanes with gravity acceleration added to 1/72 etc.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32X) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at 800 degrees Celsius or less to reduce heat consumption. Various energy conservation cycle coalescing engines to make various airplanes with gravity acceleration added to about 1/72 etc.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32Y) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at 800 degrees Celsius or less to reduce the amount of heat consumed. Various energy conservation cycle coalescing engines to make various airplanes with gravity acceleration added to about 1/72 etc.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32X) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at 600 degrees Celsius or less to reduce the amount of heat consumed. Various energy conservation cycle coalescing engines to make various airplanes with gravity acceleration added to about 1/72 etc.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32Y) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at 600 degrees Celsius or less to reduce the amount of heat consumed. Various energy conservation cycle coalescing engines to make various airplanes with gravity acceleration added to about 1/72 etc.   A combined bearing (80) thrust bearing (80a) is installed in the combined engine combustion section (31X) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at 600 degrees Celsius or less to reduce heat consumption. Various energy conservation cycle coalescing engines to make various airplanes with gravity acceleration added to 1/72 etc.   A combined bearing (80) thrust bearing (80a) is installed in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at 600 degrees Celsius or less to reduce heat consumption. Various energy conservation cycle coalescing engines to make various airplanes with gravity acceleration added to 1/72 etc.   A combined bearing (80) thrust bearing (80a) is installed in the combined engine combustion section (31X) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at 600 degrees Celsius or less to reduce heat consumption. Various energy conservation cycle coalescing engines to make various ships with gravity acceleration added to 1/72 etc.   A combined bearing (80) thrust bearing (80a) is installed in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at 600 degrees Celsius or less to reduce heat consumption. Various energy conservation cycle coalescing engines to make various ships with gravity acceleration added to 1/72 etc.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32X) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at 600 degrees Celsius or less to reduce the amount of heat consumed. Various energy conservation cycle coalescing engines that make various ships with gravity acceleration added to about 1/72 etc.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32Y) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at 600 degrees Celsius or less to reduce the amount of heat consumed. Various energy conservation cycle coalescing engines that make various ships with gravity acceleration added to about 1/72 etc.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32X) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at 600 degrees Celsius or less to reduce the amount of heat consumed. Various energy storage cycle coalescing engines that provide various heat, electricity and cold supply facilities with gravity acceleration added to about 1/72.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32Y) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at 600 degrees Celsius or less to reduce the amount of heat consumed. Various energy storage cycle coalescing engines that provide various heat, electricity and cold supply facilities with gravity acceleration added to about 1/72.   A combined bearing (80) thrust bearing (80a) is installed in the combined engine combustion section (31X) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at 600 degrees Celsius or less to reduce heat consumption. Various energy storage cycle coalescence engine that uses various heat, electricity and cold supply facilities with gravity acceleration added to 1/72 etc.   A combined bearing (80) thrust bearing (80a) is installed in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and high-temperature mercury (1d) is driven by a high-pressure turbine at 600 degrees Celsius or less to reduce heat consumption. Various energy storage cycle coalescence engine that uses various heat, electricity and cold supply facilities with gravity acceleration added to 1/72 etc.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31X) of the turbine blade cross section (4D), and the high-temperature water (52b) is driven at a high pressure turbine below the critical temperature to reduce the amount of heat consumed by about 1. / 539 etc. Various energy storage cycle coalescence engine to make various heat, electricity and cold supply facilities with additional gravity acceleration.   A combined bearing (80) thrust bearing (80a) corresponding to the application is provided in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and the high-temperature water (52b) is driven by a high-pressure turbine at a critical temperature or less to reduce the amount of heat consumed by about 1. / 539 etc. Various energy storage cycle coalescence engine to make various heat, electricity and cold supply facilities with additional gravity acceleration.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32X) of the turbine blade cross section (4D), and the high temperature water (52b) is driven by a high pressure turbine below the critical temperature to reduce the amount of heat consumed. Various energy storage cycle coalescing engines to make various heat, electricity and cold supply facilities with gravity acceleration added to 1/539 etc.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the turbine blade cross section (4Y) of the turbine blade cross section (4D), and the high temperature water (52b) is driven by a high pressure turbine below the critical temperature to reduce the amount of heat consumed. Various energy storage cycle coalescing engines to make various heat, electricity and cold supply facilities with gravity acceleration added to 1/539 etc.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32X) of the turbine blade cross section (4D), and the high temperature water (52b) is driven by a high pressure turbine below the critical temperature to reduce the amount of heat consumed. Various energy conservation cycle coalescing engines to make various ships with gravity acceleration added to 1/539 etc.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the turbine blade cross section (4Y) of the turbine blade cross section (4D), and the high temperature water (52b) is driven by a high pressure turbine below the critical temperature to reduce the amount of heat consumed. Various energy conservation cycle coalescing engines to make various ships with gravity acceleration added to 1/539 etc.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31X) of the turbine blade cross section (4D), and the high-temperature water (52b) is driven at a high pressure turbine below the critical temperature to reduce the amount of heat consumed by about 1. / 539 etc. Various energy conservation cycle coalescence engine to make various ships with gravity acceleration added.   A combined bearing (80) thrust bearing (80a) corresponding to the application is provided in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and the high-temperature water (52b) is driven by a high-pressure turbine at a critical temperature or less to reduce the amount of heat consumed by about 1. / 539 etc. Various energy conservation cycle coalescence engine to make various ships with gravity acceleration added.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31X) of the turbine blade cross section (4D), and the high-temperature water (52b) is driven at a high pressure turbine below the critical temperature to reduce the amount of heat consumed by about 1. / 539 etc. Various energy conservation cycle coalescence engine to make various airplanes with gravity acceleration added.   A combined bearing (80) thrust bearing (80a) corresponding to the application is provided in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and the high-temperature water (52b) is driven by a high-pressure turbine at a critical temperature or less to reduce the amount of heat consumed by about 1. / 539 etc. Various energy conservation cycle coalescence engine to make various airplanes with gravity acceleration added.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32X) of the turbine blade cross section (4D), and the high temperature water (52b) is driven by a high pressure turbine below the critical temperature to reduce the amount of heat consumed. Various energy conservation cycle coalescing engines to make various airplanes with gravity acceleration added to 1/539 etc.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the turbine blade cross section (4Y) of the turbine blade cross section (4D), and the high temperature water (52b) is driven by a high pressure turbine below the critical temperature to reduce the amount of heat consumed. Various energy conservation cycle coalescing engines to make various airplanes with gravity acceleration added to 1/539 etc.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32X) of the turbine blade cross section (4D), and the high-pressure turbine is driven by high-temperature water (52b) to reduce the amount of heat consumed by approximately 1/539, etc. Various energy conservation cycle coalescing engines to make various airplanes with gravity acceleration added.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire rotor blade combustion section (32Y) of the turbine blade cross section (4D), and the high-pressure turbine is driven with high-temperature water (52b) to reduce the heat consumption by approximately 1/539, etc. Various energy conservation cycle coalescing engines to make various airplanes with gravity acceleration added.   Provide a bearing (80) thrust bearing (80a) corresponding to the application in the combined engine combustion section (31X) of the turbine blade cross section (4D) and drive the high-pressure turbine with high-temperature water (52b) to reduce the heat consumption to approximately 1/539, etc. Various energy conservation cycle coalescing engines to make various airplanes with gravity acceleration added.   Provide a bearing (80) thrust bearing (80a) corresponding to the application in the combined engine combustion section (31Y) of the turbine blade cross section (4D) and drive the high-pressure turbine with high-temperature water (52b) to reduce the heat consumption to approximately 1/539, etc. Various energy conservation cycle coalescing engines to make various airplanes with gravity acceleration added.   Provide a bearing (80) thrust bearing (80a) corresponding to the application in the combined engine combustion section (31X) of the turbine blade cross section (4D) and drive the high-pressure turbine with high-temperature water (52b) to reduce the heat consumption to approximately 1/539, etc. Various energy conservation cycle coalescing engines for various ships with added gravitational acceleration.   Provide a bearing (80) thrust bearing (80a) corresponding to the application in the combined engine combustion section (31Y) of the turbine blade cross section (4D) and drive the high-pressure turbine with high-temperature water (52b) to reduce the heat consumption to approximately 1/539, etc. Various energy conservation cycle coalescing engines for various ships with added gravitational acceleration.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32X) of the turbine blade cross section (4D), and the high-pressure turbine is driven by high-temperature water (52b) to reduce the amount of heat consumed by approximately 1/539, etc. Various energy conservation cycle coalescing engines for various ships with additional gravitational acceleration.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire rotor blade combustion section (32Y) of the turbine blade cross section (4D), and the high-pressure turbine is driven with high-temperature water (52b) to reduce the heat consumption by approximately 1/539, etc. Various energy conservation cycle coalescing engines for various ships with additional gravitational acceleration.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32X) of the turbine blade cross section (4D), and the high-pressure turbine is driven by high-temperature water (52b) to reduce the amount of heat consumed by approximately 1/539, etc. Combined with various energy conservation cycle engines to provide various heat, electricity and cold supply facilities with additional gravity acceleration.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire rotor blade combustion section (32Y) of the turbine blade cross section (4D), and the high-pressure turbine is driven with high-temperature water (52b) to reduce the heat consumption by approximately 1/539, etc. Combined with various energy conservation cycle engines to provide various heat, electricity and cold supply facilities with additional gravity acceleration.   Provide a bearing (80) thrust bearing (80a) corresponding to the application in the combined engine combustion section (31X) of the turbine blade cross section (4D) and drive the high-pressure turbine with high-temperature water (52b) to reduce the heat consumption to approximately 1/539, etc. Various energy storage cycle coalescing engines to provide various heat, electricity and cold supply facilities with additional gravity acceleration.   Provide a bearing (80) thrust bearing (80a) corresponding to the application in the combined engine combustion section (31Y) of the turbine blade cross section (4D) and drive the high-pressure turbine with high-temperature water (52b) to reduce the heat consumption to approximately 1/539, etc. Various energy storage cycle coalescing engines to provide various heat, electricity and cold supply facilities with additional gravity acceleration.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31X) of the turbine blade cross section (4D), and the high-pressure turbine is driven with high-temperature water (52b) to generate the same-pressure output at the atmospheric pressure with steam. Various energy storage cycle coalescence engine to make various additional heat, electricity and cold supply facilities in a vacuum of 19.8 times kg weight m / sec in a gravity acceleration of 9.8 m / sec.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and high-pressure turbine driving is performed with high-temperature water (52b) to generate the same pressure output at atmospheric pressure as steam. Various energy storage cycle coalescence engine to make various additional heat, electricity and cold supply facilities in a vacuum of 19.8 times kg weight m / sec in a gravity acceleration of 9.8 m / sec.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the turbine blade cross section (4D) of the turbine blade cross section (4D), and a high-pressure turbine is driven with high-temperature water (52b) to drive the atmospheric pressure at the same speed output by steam. Various energy storage cycle coalescing engines that provide additional heat, electricity, and cold supply facilities in a vacuum at a gravity acceleration of 9.8 m / sec.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the turbine blade cross section (4Y) of the turbine blade cross section (4D), and high-pressure turbine driving is performed with high-temperature water (52b) to drive the atmospheric pressure at the same speed output by steam. Various energy storage cycle coalescing engines that provide additional heat, electricity, and cold supply facilities in a vacuum at a gravity acceleration of 9.8 m / sec.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the turbine blade cross section (4D) of the turbine blade cross section (4D), and a high-pressure turbine is driven with high-temperature water (52b) to drive the atmospheric pressure at the same speed output by steam. Various energy conservation cycle coalescing engines to make various kinds of ships added to gravity acceleration of 9.8m / second per second in vacuum to 1700 times kg weight m / second.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the turbine blade cross section (4Y) of the turbine blade cross section (4D), and high-pressure turbine driving is performed with high-temperature water (52b) to drive the atmospheric pressure at the same speed output by steam. Various energy conservation cycle coalescing engines to make various kinds of ships added to gravity acceleration of 9.8m / second per second in vacuum to 1700 times kg weight m / second.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31X) of the turbine blade cross section (4D), and the high-pressure turbine is driven with high-temperature water (52b) to generate the same-pressure output at the atmospheric pressure with steam. Various energy storage cycle coalescing engines to make various kinds of ships added to gravity acceleration 9.8m / second per second in vacuum at 1700 times kg weight m / second.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and high-pressure turbine driving is performed with high-temperature water (52b) to generate the same pressure output at atmospheric pressure as steam. Various energy storage cycle coalescing engines to make various kinds of ships added to gravity acceleration 9.8m / second per second in vacuum at 1700 times kg weight m / second.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31X) of the turbine blade cross section (4D), and the high-pressure turbine is driven with high-temperature water (52b) to generate the same-pressure output at the atmospheric pressure with steam. Various energy conservation cycle coalescing engines that make various airplanes with gravity acceleration of 9.8m / second per second in vacuum at 1700 times kg weight m / second, etc.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and high-pressure turbine driving is performed with high-temperature water (52b) to generate the same pressure output at atmospheric pressure as steam. Various energy conservation cycle coalescing engines that make various airplanes with gravity acceleration of 9.8m / second per second in vacuum at 1700 times kg weight m / second, etc.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the turbine blade cross section (4D) of the turbine blade cross section (4D), and a high-pressure turbine is driven with high-temperature water (52b) to drive the atmospheric pressure at the same speed output by steam. Various energy storage cycle coalescing engines that make various airplanes with a gravitational acceleration of 9.8 m / sec.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the turbine blade cross section (4Y) of the turbine blade cross section (4D), and high-pressure turbine driving is performed with high-temperature water (52b) to drive the atmospheric pressure at the same speed output by steam. Various energy storage cycle coalescing engines that make various airplanes with a gravitational acceleration of 9.8 m / sec.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the turbine blade cross section (4D) of the turbine blade cross section (4D), and a high-pressure turbine is driven by high-temperature mercury (1d) to drive the atmospheric pressure at the same speed by steam. Various energy conservation cycle coalescing engines to make various airplanes with a gravitational acceleration of 9.8 m / sec.   Provided bearing (80) thrust bearing (80a) corresponding to application in all rotor blade combustion section (32Y) of turbine blade cross section (4D), high-pressure turbine driven with high-temperature mercury (1d), steam-driven at atmospheric pressure and same speed output Various energy conservation cycle coalescing engines to make various airplanes with a gravitational acceleration of 9.8 m / sec.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31X) of the turbine blade cross section (4D), and high-pressure turbine driving is performed with high-temperature mercury (1d), and the atmospheric pressure and the same speed output is steam-driven. Various energy storage cycle coalescing engines to make various airplanes with a gravity acceleration of 9.8m / sec per second in a vacuum of 23,000 times kg weight m / sec.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and the high-pressure turbine is driven with high-temperature mercury (1d) to output the same pressure output at the atmospheric pressure with steam. Various energy storage cycle coalescing engines to make various airplanes with a gravity acceleration of 9.8m / sec per second in a vacuum of 23,000 times kg weight m / sec.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31X) of the turbine blade cross section (4D), and high-pressure turbine driving is performed with high-temperature mercury (1d), and the atmospheric pressure and the same speed output is steam-driven. Various energy storage cycle coalescing engines to make various ships with additional gravity acceleration of 9.8m / second per second in vacuum at 23,000 times kg weight m / second.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and the high-pressure turbine is driven with high-temperature mercury (1d) to output the same pressure output at the atmospheric pressure with steam. Various energy storage cycle coalescing engines to make various ships with additional gravity acceleration of 9.8m / second per second in vacuum at 23,000 times kg weight m / second.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the turbine blade cross section (4D) of the turbine blade cross section (4D), and a high-pressure turbine is driven by high-temperature mercury (1d) to drive the atmospheric pressure at the same speed by steam. Various energy storage cycle coalescing engines to make various ships with additional gravity acceleration of 9.8m / second per second in vacuum to 23,000 times kg weight m / second.   Provided bearing (80) thrust bearing (80a) corresponding to application in all rotor blade combustion section (32Y) of turbine blade cross section (4D), high-pressure turbine driven with high-temperature mercury (1d), steam-driven at atmospheric pressure and same speed output Various energy storage cycle coalescing engines to make various ships with additional gravity acceleration of 9.8m / second per second in vacuum to 23,000 times kg weight m / second.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the turbine blade cross section (4D) of the turbine blade cross section (4D), and a high-pressure turbine is driven by high-temperature mercury (1d) to drive the atmospheric pressure at the same speed by steam. Various energy storage cycle coalescing engines to provide additional heat, electricity and cold supply facilities in a vacuum at a gravity acceleration of 9.8 m / sec.   Provided bearing (80) thrust bearing (80a) corresponding to application in all rotor blade combustion section (32Y) of turbine blade cross section (4D), high-pressure turbine driven with high-temperature mercury (1d), steam-driven at atmospheric pressure and same speed output Various energy storage cycle coalescing engines to provide additional heat, electricity and cold supply facilities in a vacuum at a gravity acceleration of 9.8 m / sec.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31X) of the turbine blade cross section (4D), and high-pressure turbine driving is performed with high-temperature mercury (1d), and the atmospheric pressure and the same speed output is steam-driven. Various energy storage cycle coalescing engine to supply various heat, electricity and cold supply facilities in a vacuum at a gravity acceleration of 9.8 m / sec in a vacuum of 23,000 times kg weight m / sec.   A combined bearing (80) thrust bearing (80a) is provided in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and the high-pressure turbine is driven with high-temperature mercury (1d) to output the same pressure output at the atmospheric pressure with steam. Various energy storage cycle coalescing engine to supply various heat, electricity and cold supply facilities in a vacuum at a gravity acceleration of 9.8 m / sec in a vacuum of 23,000 times kg weight m / sec.   A combined bearing (80) thrust bearing (80a) for the combined engine combustion section (31X) of the turbine blade cross section (4D) is provided, and high-temperature mercury (1d) is sprayed vertically downward in a vacuum, and the gravitational acceleration is 9.8 m / sec. Various energy storage cycle coalescing engines that drive high-pressure turbines with acceleration added every second.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and high-temperature mercury (1d) is sprayed vertically downward in a vacuum in a gravity acceleration of 9.8 m / sec. Various energy storage cycle coalescing engines that drive high-pressure turbines with acceleration added every second.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32X) of the turbine blade cross section (4D), and high-temperature mercury (1d) is sprayed vertically downward in a vacuum to a gravity acceleration of 9.8 m / Various energy storage cycle coalescing engines that drive high pressure turbines with acceleration added every second.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32Y) of the turbine blade cross section (4D), and high-temperature mercury (1d) is sprayed vertically downward in a vacuum to a gravitational acceleration of 9.8 m / Various energy storage cycle coalescing engines that drive high pressure turbines with acceleration added every second.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32X) of the turbine blade cross section (4D), and high-temperature mercury (1d) is sprayed vertically downward in a vacuum to a gravity acceleration of 9.8 m / Various energy storage cycle coalescing engines that use high-pressure turbine-driven various heat, electricity, and cold supply facilities with acceleration added every second.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32Y) of the turbine blade cross section (4D), and high-temperature mercury (1d) is sprayed vertically downward in a vacuum to a gravitational acceleration of 9.8 m / Various energy storage cycle coalescing engines that use high-pressure turbine-driven various heat, electricity, and cold supply facilities with acceleration added every second.   A combined bearing (80) thrust bearing (80a) for the combined engine combustion section (31X) of the turbine blade cross section (4D) is provided, and high-temperature mercury (1d) is sprayed vertically downward in a vacuum, and the gravitational acceleration is 9.8 m / sec. Various energy conservation cycle coalescing engines that use high-pressure turbine-driven various heat, electricity and cold supply facilities with acceleration added every second.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and high-temperature mercury (1d) is sprayed vertically downward in a vacuum in a gravity acceleration of 9.8 m / sec. Various energy conservation cycle coalescing engines that use high-pressure turbine-driven various heat, electricity and cold supply facilities with acceleration added every second.   A combined bearing (80) thrust bearing (80a) for the combined engine combustion section (31X) of the turbine blade cross section (4D) is provided, and high-temperature mercury (1d) is sprayed vertically downward in a vacuum, and the gravitational acceleration is 9.8 m / sec. Various energy storage cycle coalescing engines that make high-speed turbine-driven vessels with acceleration added every second.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and high-temperature mercury (1d) is sprayed vertically downward in a vacuum in a gravity acceleration of 9.8 m / sec. Various energy storage cycle coalescing engines that make high-speed turbine-driven vessels with acceleration added every second.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32X) of the turbine blade cross section (4D), and high-temperature mercury (1d) is sprayed vertically downward in a vacuum to a gravity acceleration of 9.8 m / Various energy conservation cycle coalescing engines that make various vessels driven by high-pressure turbines with acceleration added every second.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32Y) of the turbine blade cross section (4D), and high-temperature mercury (1d) is sprayed vertically downward in a vacuum to a gravitational acceleration of 9.8 m / Various energy conservation cycle coalescing engines that make various vessels driven by high-pressure turbines with acceleration added every second.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32X) of the turbine blade cross section (4D), and high-temperature mercury (1d) is sprayed vertically downward in a vacuum to a gravity acceleration of 9.8 m / Various energy storage cycle coalescing engines that make high-speed turbine-driven airplanes with acceleration added every second.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32Y) of the turbine blade cross section (4D), and high-temperature mercury (1d) is sprayed vertically downward in a vacuum to a gravitational acceleration of 9.8 m / Various energy storage cycle coalescing engines that make high-speed turbine-driven airplanes with acceleration added every second.   A combined bearing (80) thrust bearing (80a) for the combined engine combustion section (31X) of the turbine blade cross section (4D) is provided, and high-temperature mercury (1d) is sprayed vertically downward in a vacuum, and the gravitational acceleration is 9.8 m / sec. Various energy storage cycle coalescing engines that make high-speed turbine-driven airplanes with acceleration added every second.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and high-temperature mercury (1d) is sprayed vertically downward in a vacuum in a gravity acceleration of 9.8 m / sec. Various energy storage cycle coalescing engines that make high-speed turbine-driven airplanes with acceleration added every second.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the combined engine combustion section (31X) of the turbine blade cross section (4D), and high-temperature water (52b) is sprayed vertically downward in a vacuum, and the gravitational acceleration is 9.8 m / sec. Various energy storage cycle coalescing engines that make high-speed turbine-driven airplanes with acceleration added every second.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and hot water (52b) is sprayed vertically downward in a vacuum in a gravity acceleration of 9.8 m / sec. Various energy storage cycle coalescing engines that make high-speed turbine-driven airplanes with acceleration added every second.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32X) of the turbine blade cross section (4D), and high-temperature water (52b) is sprayed vertically downward in a vacuum to achieve a gravitational acceleration of 9.8 m / Various energy storage cycle coalescing engines that make high-speed turbine-driven airplanes with acceleration added every second.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32Y) of the turbine blade cross section (4D), and high-temperature water (52b) is sprayed vertically downward in a vacuum to achieve a gravitational acceleration of 9.8 m / Various energy storage cycle coalescing engines that make high-speed turbine-driven airplanes with acceleration added every second.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32X) of the turbine blade cross section (4D), and high-temperature water (52b) is sprayed vertically downward in a vacuum to achieve a gravitational acceleration of 9.8 m / Various energy conservation cycle coalescing engines that make various vessels driven by high-pressure turbines with acceleration added every second.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32Y) of the turbine blade cross section (4D), and high-temperature water (52b) is sprayed vertically downward in a vacuum to achieve a gravitational acceleration of 9.8 m / Various energy conservation cycle coalescing engines that make various vessels driven by high-pressure turbines with acceleration added every second.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the combined engine combustion section (31X) of the turbine blade cross section (4D), and high-temperature water (52b) is sprayed vertically downward in a vacuum, and the gravitational acceleration is 9.8 m / sec. Various energy storage cycle coalescing engines that make high-speed turbine-driven vessels with acceleration added every second.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and hot water (52b) is sprayed vertically downward in a vacuum in a gravity acceleration of 9.8 m / sec. Various energy storage cycle coalescing engines that make high-speed turbine-driven vessels with acceleration added every second.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the combined engine combustion section (31X) of the turbine blade cross section (4D), and high-temperature water (52b) is sprayed vertically downward in a vacuum, and the gravitational acceleration is 9.8 m / sec. Various energy conservation cycle coalescing engines that use high-pressure turbine-driven various heat, electricity and cold supply facilities with acceleration added every second.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and hot water (52b) is sprayed vertically downward in a vacuum in a gravity acceleration of 9.8 m / sec. Various energy conservation cycle coalescing engines that use high-pressure turbine-driven various heat, electricity and cold supply facilities with acceleration added every second.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32X) of the turbine blade cross section (4D), and high-temperature water (52b) is sprayed vertically downward in a vacuum to achieve a gravitational acceleration of 9.8 m / Various energy storage cycle coalescing engines that use high-pressure turbine-driven various heat, electricity, and cold supply facilities with acceleration added every second.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32Y) of the turbine blade cross section (4D), and high-temperature water (52b) is sprayed vertically downward in a vacuum to achieve a gravitational acceleration of 9.8 m / Various energy storage cycle coalescing engines that use high-pressure turbine-driven various heat, electricity, and cold supply facilities with acceleration added every second.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32X) of the turbine blade cross section (4D), and high-temperature water (52b) is sprayed vertically downward in a vacuum to achieve a gravitational acceleration of 9.8 m / Various energy storage cycle coalescing engines that drive high pressure turbines with acceleration added every second.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire blade combustion section (32Y) of the turbine blade cross section (4D), and high-temperature water (52b) is sprayed vertically downward in a vacuum to achieve a gravitational acceleration of 9.8 m / Various energy storage cycle coalescing engines that drive high pressure turbines with acceleration added every second.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the combined engine combustion section (31X) of the turbine blade cross section (4D), and high-temperature water (52b) is sprayed vertically downward in a vacuum, and the gravitational acceleration is 9.8 m / sec. Various energy storage cycle coalescing engines that drive high-pressure turbines with acceleration added every second.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and hot water (52b) is sprayed vertically downward in a vacuum in a gravity acceleration of 9.8 m / sec. Various energy storage cycle coalescing engines that drive high-pressure turbines with acceleration added every second.   A combined bearing (80) thrust bearing (80a) for the combined engine combustion section (31X) of the turbine blade cross section (4D) is provided, and the intake air is heated by the high-temperature mercury (1d) exhaust heat quantity, and the best heat of compression heat recovery theory Various energy storage cycle coalescing engines for various automobiles with gravity acceleration added to the pump (1G).   A combined bearing (80) thrust bearing (80a) is installed in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and the intake air is heated by the high-temperature mercury (1d) exhaust heat quantity. Various energy storage cycle coalescing engines for various automobiles with gravity acceleration added to the pump (1G).   The turbine blade cross section (4D) all rotor blade combustion part (32X) is equipped with a bearing (80) thrust bearing (80a) corresponding to the application, and the intake air is heated by the high-temperature mercury (1d) exhaust heat quantity, and the compression heat recovery theory is the best Various energy storage cycle coalescing engines for various automobiles with gravity acceleration added to heat pump (1G).   The turbine blade cross section (4D) is equipped with a bearing (80) thrust bearing (80a) corresponding to the application in the all blade combustion section (32Y), and the intake air is heated by the high-temperature mercury (1d) exhaust heat quantity, so that the best compression heat recovery theory is achieved. Various energy storage cycle coalescing engines for various automobiles with gravity acceleration added to heat pump (1G).   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the whole blade combustion section (32X) of the turbine blade cross section (4D), and the intake air is heated by the exhaust heat quantity near 230 degrees high temperature mercury (1d) to compress the heat. Recovery theory Best heat pump (1G) Combined with various energy storage cycle engines for various automobiles with gravitational acceleration added.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire rotor blade combustion section (32Y) of the turbine blade cross section (4D), and the intake air is heated by high-temperature mercury (1d) exhaust heat near 230 degrees to compress heat. Recovery theory Best heat pump (1G) Combined with various energy storage cycle engines for various automobiles with gravitational acceleration added.   A combined bearing (80) thrust bearing (80a) is installed in the combined engine combustion section (31X) of the turbine blade cross section (4D), and the intake air is heated by high-temperature mercury (1d) near 230 degrees of exhaust heat to compress the heat. Various energy storage cycle coalescing engines for various automobiles with gravity acceleration added to the theoretical best heat pump (1G).   A combined bearing (80) thrust bearing (80a) is installed in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and the intake air is heated by exhaust heat near 230 degrees of high temperature mercury (1d) to recover the compression heat. Various energy storage cycle coalescing engines for various automobiles with gravity acceleration added to the theoretical best heat pump (1G).   A combined bearing (80) thrust bearing (80a) is installed in the combined engine combustion section (31X) of the turbine blade cross section (4D), and the intake air is heated by high-temperature mercury (1d) near 230 degrees of exhaust heat to compress the heat. Various energy storage cycle coalescing engine to supply various heat, electricity and cold supply facilities with gravity acceleration added to the theoretical best heat pump (1G).   A combined bearing (80) thrust bearing (80a) is installed in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and the intake air is heated by exhaust heat near 230 degrees of high temperature mercury (1d) to recover the compression heat. Various energy storage cycle coalescing engine to supply various heat, electricity and cold supply facilities with gravity acceleration added to the theoretical best heat pump (1G).   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the whole blade combustion section (32X) of the turbine blade cross section (4D), and the intake air is heated by the exhaust heat quantity near 230 degrees high temperature mercury (1d) to compress the heat. Recovery theory Best heat pump (1G) Combines various energy storage cycle engines to provide various heat, electricity and cold supply facilities with additional gravitational acceleration.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire rotor blade combustion section (32Y) of the turbine blade cross section (4D), and the intake air is heated by high-temperature mercury (1d) exhaust heat near 230 degrees to compress heat. Recovery theory Best heat pump (1G) Combines various energy storage cycle engines to provide various heat, electricity and cold supply facilities with additional gravitational acceleration.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the whole blade combustion section (32X) of the turbine blade cross section (4D), and the intake air is heated by the exhaust heat quantity near 230 degrees high temperature mercury (1d) to compress the heat. Recovery theory Best heat pump (1G) Various energy storage cycle coalescing engines to make various ships with gravitational acceleration added.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire rotor blade combustion section (32Y) of the turbine blade cross section (4D), and the intake air is heated by high-temperature mercury (1d) exhaust heat near 230 degrees to compress heat. Recovery theory Best heat pump (1G) Various energy storage cycle coalescing engines to make various ships with gravitational acceleration added.   A combined bearing (80) thrust bearing (80a) is installed in the combined engine combustion section (31X) of the turbine blade cross section (4D), and the intake air is heated by high-temperature mercury (1d) near 230 degrees of exhaust heat to compress the heat. Various energy storage cycle coalescing engines to make various ships with gravity acceleration added to the theoretical best heat pump (1G).   A combined bearing (80) thrust bearing (80a) is installed in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and the intake air is heated by exhaust heat near 230 degrees of high temperature mercury (1d) to recover the compression heat. Various energy storage cycle coalescing engines to make various ships with gravity acceleration added to the theoretical best heat pump (1G).   A combined bearing (80) thrust bearing (80a) is installed in the combined engine combustion section (31X) of the turbine blade cross section (4D), and the intake air is heated by high-temperature mercury (1d) near 230 degrees of exhaust heat to compress the heat. Various energy storage cycle coalescing engines that make various airplanes with gravity acceleration added to the theoretical best heat pump (1G).   A combined bearing (80) thrust bearing (80a) is installed in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and the intake air is heated by exhaust heat near 230 degrees of high temperature mercury (1d) to recover the compression heat. Various energy storage cycle coalescing engines that make various airplanes with gravity acceleration added to the theoretical best heat pump (1G).   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the whole blade combustion section (32X) of the turbine blade cross section (4D), and the intake air is heated by the exhaust heat quantity near 230 degrees high temperature mercury (1d) to compress the heat. Recovery theory Best heat pump (1G) Combines various energy storage cycle engines into various aircraft with gravitational acceleration added.   A bearing (80) thrust bearing (80a) corresponding to the application is provided in the entire rotor blade combustion section (32Y) of the turbine blade cross section (4D), and the intake air is heated by high-temperature mercury (1d) exhaust heat near 230 degrees to compress heat. Recovery theory Best heat pump (1G) Combines various energy storage cycle engines into various aircraft with gravitational acceleration added.   A combined bearing (80) thrust bearing (80a) for the combined engine combustion section (31X) of the turbine blade cross section (4D) is provided, and the intake air is heated by the high-temperature mercury (1d) exhaust heat quantity, and the best heat of compression heat recovery theory Various energy storage cycle coalescing engines that use various heat, electricity, and cold supply facilities that add gravity acceleration to the pump (1G).   A combined bearing (80) thrust bearing (80a) is installed in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and the intake air is heated by the high-temperature mercury (1d) exhaust heat quantity. Various energy storage cycle coalescing engines that use various heat, electricity, and cold supply facilities that add gravity acceleration to the pump (1G).   The turbine blade cross section (4D) all rotor blade combustion part (32X) is equipped with a bearing (80) thrust bearing (80a) corresponding to the application, and the intake air is heated by the high-temperature mercury (1d) exhaust heat quantity, and the compression heat recovery theory is the best Various energy storage cycle coalescing engines that use various heat, electricity, and cold supply facilities that add gravity acceleration to the heat pump (1G).   The turbine blade cross section (4D) is equipped with a bearing (80) thrust bearing (80a) corresponding to the application in the all blade combustion section (32Y), and the intake air is heated by the high-temperature mercury (1d) exhaust heat quantity, so that the best compression heat recovery theory is achieved. Various energy storage cycle coalescing engines that use various heat, electricity, and cold supply facilities that add gravity acceleration to the heat pump (1G).   The turbine blade cross section (4D) all rotor blade combustion part (32X) is equipped with a bearing (80) thrust bearing (80a) corresponding to the application, and the intake air is heated by the high-temperature mercury (1d) exhaust heat quantity, and the compression heat recovery theory is the best Various energy storage cycle coalescing engines for various types of ships with gravity acceleration added to heat pump (1G).   The turbine blade cross section (4D) is equipped with a bearing (80) thrust bearing (80a) corresponding to the application in the all blade combustion section (32Y), and the intake air is heated by the high-temperature mercury (1d) exhaust heat quantity, so that the best compression heat recovery theory is achieved. Various energy storage cycle coalescing engines for various types of ships with gravity acceleration added to heat pump (1G).   A combined bearing (80) thrust bearing (80a) for the combined engine combustion section (31X) of the turbine blade cross section (4D) is provided, and the intake air is heated by the high-temperature mercury (1d) exhaust heat quantity, and the best heat of compression heat recovery theory Various energy storage cycle coalescing engines for various ships with additional gravity acceleration added to the pump (1G).   A combined bearing (80) thrust bearing (80a) is installed in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and the intake air is heated by the high-temperature mercury (1d) exhaust heat quantity. Various energy storage cycle coalescing engines for various ships with additional gravity acceleration added to the pump (1G).   A combined bearing (80) thrust bearing (80a) for the combined engine combustion section (31X) of the turbine blade cross section (4D) is provided, and the intake air is heated by the high-temperature mercury (1d) exhaust heat quantity, and the best heat of compression heat recovery theory Various energy storage cycle coalescing engines to make various airplanes with gravity acceleration added to the pump (1G).   A combined bearing (80) thrust bearing (80a) is installed in the combined engine combustion section (31Y) of the turbine blade cross section (4D), and the intake air is heated by the high-temperature mercury (1d) exhaust heat quantity. Various energy storage cycle coalescing engines to make various airplanes with gravity acceleration added to the pump (1G).   The turbine blade cross section (4D) all rotor blade combustion part (32X) is equipped with a bearing (80) thrust bearing (80a) corresponding to the application, and the intake air is heated by the high-temperature mercury (1d) exhaust heat quantity, and the compression heat recovery theory is the best Various energy storage cycle coalescing engines to make various airplanes with gravity acceleration added to heat pump (1G).   The turbine blade cross section (4D) is equipped with a bearing (80) thrust bearing (80a) corresponding to the application in the all blade combustion section (32Y), and the intake air is heated by the high-temperature mercury (1d) exhaust heat quantity, so that the best compression heat recovery theory is achieved. Various energy storage cycle coalescing engines to make various airplanes with gravity acceleration added to heat pump (1G).   Gravity acceleration for recovering cold heat by providing a bearing (80) thrust bearing (80a) for the application, and providing a cold heat recovery means (3C) on the turbine blade (8c) of the turbine blade cross section (4D) of the turbine blade cross section (4D) Various energy storage cycle coalescing engines to make various additional cars.   Application-specific bearing (80) Thrust bearing (80a) is provided, and the turbine blade (8c) of the turbine blade cross section (4D) of the turbine blade cross section (4D) is provided with cold heat recovery means (3C) to add gravity acceleration to heating. Various energy conservation cycle coalescing engines for various automobiles.   A bearing (80) thrust bearing (80a) corresponding to the application is provided, and a cold heat recovery means (3C) is provided on the turbine blade (8c) of the entire rotor blade gas turbine of the turbine blade cross section (4D), and alcohol (1C) is used. Various energy conservation cycle coalescing engines that make various automobiles with gravity acceleration added to recovering cold heat.   A bearing (80) thrust bearing (80a) corresponding to the application is provided, and a cold heat recovery means (3C) is provided on the turbine blade (8c) of the entire rotor blade gas turbine of the turbine blade cross section (4D), and alcohol (1C) is used. Various energy conservation cycle coalescing engines for various automobiles that add gravity acceleration to heating.   A bearing (80) thrust bearing (80a) corresponding to the application is provided, and a cold heat recovery means (3C) is provided on the turbine blade (8c) of the entire rotor blade gas turbine of the turbine blade cross section (4D), and alcohol (1C) is used. Various energy storage cycle coalescing engines that make various automobiles add gravity acceleration to increase recovery output of cold.   A bearing (80) thrust bearing (80a) corresponding to the application is provided, and a cold heat recovery means (3C) is provided on the turbine blade (8c) of the entire rotor blade gas turbine of the turbine blade cross section (4D), and alcohol (1C) is used. Various energy storage cycle coalescing engines that increase the heating output and increase the gravitational acceleration.   A bearing (80) thrust bearing (80a) corresponding to the application is provided, and a cold heat recovery means (3C) is provided on the turbine blade (8c) of the entire rotor blade gas turbine of the turbine blade cross section (4D), and alcohol (1C) is used. Recovers cold energy. Combines various energy storage cycle engines to prevent various types of automobiles with additional gravity acceleration to prevent sticking of dry ice and moisture.   A bearing (80) thrust bearing (80a) corresponding to the application is provided, and a cold heat recovery means (3C) is provided on the turbine blade (8c) of the entire rotor blade gas turbine of the turbine blade cross section (4D), and alcohol (1C) is used. Various energy storage cycle coalescing engines to make various automobiles with additional gravity acceleration to prevent sticking of heated dry ice and moisture.   Application-specific bearings (80) Thrust bearings (80a) are provided, and turbine blades (8c) of the turbine blade cross section (4D) of the turbine blade cross section (4D) are provided with heating high temperature means (3B) to add gravity acceleration to heating. Various energy conservation cycle coalescing engines for various automobiles.   Application-specific bearing (80) Thrust bearing (80a) is provided, and turbine blade (8c) of turbine blade cross section (4D) of turbine blade cross section (4D) is provided with water repellent action (3A) to add gravity acceleration to water repellent Various energy conservation cycle coalescing engines for various automobiles.   A bearing (80) suitable for the application (80a) is provided, and a high temperature heating means (3B) is provided on the turbine blade (8c) of the turbine blade cross section (4D) of the turbine blade cross section (4D) to make rolling contact with the heating vaporized film. Various energy conservation cycle coalescing engines for various automobiles with gravity acceleration added to the rotation output.   Provided bearing (80) thrust bearing (80a) for application, and provided water repellent action (3A) to turbine blade (8c) of all rotor blade water turbine of turbine blade cross section (4D) to make rolling contact by water repellent action Various energy conservation cycle coalescing engines for various automobiles with gravity acceleration added to the rotation output.   Application-specific bearings (80) Thrust bearings (80a) are provided, and various automobiles with gravity acceleration added to cool (52e) cooling around the exhaust saturation temperature of the turbine blade cross section (4D) of the entire rotor blade water turbine at 30 degrees Various energy conservation cycle coalescence engine.   Gravity acceleration to prevent application of bearing (80) thrust bearing (80a) for application, and cooling (52e) near the exhaust saturation temperature of the turbine blade cross section (4D) for all rotor blade water turbines to cool (52e) Various energy storage cycle coalescing engines to make various additional cars.   Application-specific bearing (80) Thrust bearing (80a) is provided, and alcohol cold heat (52e) is recovered and stored in all rotor blade gas turbine with turbine blade cross section (4D) to make various automobiles with additional gravity acceleration for use. Various energy conservation cycle coalescence engine.   Application-specific bearings (80) Thrust bearings (80a) are provided, and the compressed air cold heat (52e) is recovered and stored in all rotor blade gas turbines with a turbine blade cross section (4D). Various energy conservation cycle coalescing engines.   Application-specific bearing (80) Thrust bearing (80a) is provided, and ice-cooled heat (52e) is recovered and stored in a turbine blade cross-section (4D) full blade gas turbine for use in various vehicles with additional gravitational acceleration. Various energy conservation cycle coalescence engine.   Application-specific bearings (80) Thrust bearings (80a) are provided, and cold heat (52e) is recovered and stored in all blade gas turbines with a turbine blade cross section (4D) to add gravity acceleration for use as various refrigeration equipment. Various energy conservation cycle coalescing engines for various automobiles.   Application-specific bearings (80) Thrust bearings (80a) are provided, and cold heat (52e) is recovered and stored in all rotor blade gas turbines with a turbine blade cross section (4D) to add gravity acceleration for use as various refrigeration equipment. Various energy conservation cycle coalescing engines for various automobiles.   Application-specific bearings (80) Thrust bearings (80a) are provided, and cold heat (52e) is collected and stored in all rotor blade gas turbines with a turbine blade cross section (4D) to add gravity acceleration for use as various cooling equipment. Various energy conservation cycle coalescing engines for various automobiles.   Application-specific bearings (80) Thrust bearings (80a) are provided, and cold heat (52e) is recovered and stored in all rotor blade gas turbines with a turbine blade cross section (4D) to add gravity acceleration for use as various cooling equipment. Various energy conservation cycle coalescing engines for various automobiles.   Application-specific bearings (80) Thrust bearings (80a) are provided, and cold heat (52e) is recovered and stored in all rotor blade gas turbines with a turbine blade cross section (4D) to add gravity acceleration for use as various ice making equipment. Various energy conservation cycle coalescing engines for various automobiles.   Gravity acceleration for use as various compressed air cold piping buildings by providing bearing (80) thrust bearing (80a) for application, collecting and storing cold heat (52e) in a turbine blade cross section (4D) full blade gas turbine Various energy storage cycle coalescing engines to make various additional cars.   Various bearings (80) and thrust bearings (80a) are provided, and all the rotor blade gas turbine exhaust of the turbine blade cross section (4D) is supplied to the seabed as CO2 and other combustion gas dissolved water (52 g). Various energy conservation cycle coalescence engine for automobiles.   Various bearings (80) and thrust bearings (80a) are provided, and all the rotor blade gas turbine exhaust of the turbine blade cross section (4D) is supplied to the seabed as CO2 and other combustion gas dissolved water (52 g). Various energy conservation cycle coalescence engine that propagates seaweed in automobiles.   Various bearings (80) and thrust bearings (80a) are provided, and all the rotor blade gas turbine exhaust of the turbine blade cross section (4D) is supplied to the seabed as CO2 and other combustion gas dissolved water (52 g). Various energy conservation cycle coalescence engine that grows algae in automobiles.   The bearing (80) thrust bearing (80a) corresponding to the application is provided and the whole blade gas turbine exhaust of the turbine blade cross section (4D) is supplied to the seabed etc. as combustion gas dissolved water (52 g) such as CO2 to provide phytoplanktons. Various energy conservation cycle coalescing engines for various automobiles that add gravity acceleration to proliferation.   A bearing (80) suitable for application (80a) is provided, and for the rotational output of the turbine blade cross section (4E) only, excess heat is recovered and stored at various temperatures (52d) of 300 degrees or less, and gravitational acceleration is added for use. Various energy conservation cycle coalescing engines for various automobiles.   Provided bearing (80) thrust bearing (80a) for application, specially used for rotating output of turbine blade cross section (4E), recovering and storing surplus heat with various heat (52d) of 300 degrees or less as various heating equipment Various energy conservation cycle coalescing engines for use in various automobiles with additional gravitational acceleration.   Provided bearings (80) and thrust bearings (80a) corresponding to the application, and dedicated to the rotational output of the turbine blade cross section (4E), the excess heat is recovered and stored at various temperatures (52d) of 300 degrees or less as various cooking equipment. Various energy conservation cycle coalescing engines for use in various automobiles with additional gravitational acceleration.   Provided bearings (80) and thrust bearings (80a) for use, and dedicated to rotational output of the turbine blade cross section (4E), recovering and storing surplus heat with various temperatures (52d) of 300 degrees or less as various types of hot water equipment Various energy conservation cycle coalescing engines for use in various automobiles with additional gravitational acceleration.   A bearing (80) for thrust application (80a) is provided, and the turbine blade cross section (4E) is used exclusively for the rotational output. The excess heat is recovered and stored at various temperatures (52d) below 300 degrees and used as various dishwashers. Various energy conservation cycle coalescing engines for various automobiles with additional gravitational acceleration.   Provided bearings (80) and thrust bearings (80a) for use, and dedicated to rotational output of the turbine blade cross section (4E), recovering and storing excess heat at various temperatures (52d) of 300 degrees or less as various washing dryers Various energy conservation cycle coalescing engines for use in various automobiles with additional gravitational acceleration.   Provided bearing (80) thrust bearing (80a) for use, and specially used for rotating output of turbine blade cross section (4E), recovering and storing surplus heat with various temperatures (52d) of 300 degrees or less, and various water-heat pipe buildings As a combined engine with various energy conservation cycles to use as various vehicles with additional gravitational acceleration.   Provided bearings (80) and thrust bearings (80a) for use, and dedicated to rotational output of the turbine blade cross section (4E), the excess heat is recovered and stored at various temperatures (52d) of 300 degrees or less to distill various water such as seawater. Various energy conservation cycle coalescing engines for various automobiles with additional gravity acceleration for use as water.   Provided bearings (80) and thrust bearings (80a) for use, and dedicated to rotational output of the turbine blade cross section (4E), the excess heat is recovered and stored at various temperatures (52d) of 300 degrees or less to distill various water such as seawater. Various energy conservation cycle coalescing engines to be used as water and salt for various automobiles with added gravitational acceleration.   A turbine bearing (80) thrust bearing (80a) for turbine blade cross section (4D) application is provided, the amount of compressed air heat (28b) is recovered by intake air (28a), and the heat is compressed by heat pump (1G). Various energy conservation cycle coalescing engines for various acceleration-added automobiles.   A bearing (80) thrust bearing (80a) corresponding to the application of the turbine blade cross section (4D) is provided, and the heat pump (1G) collects the mercury exhaust heat amount (5A) + compressed air heat amount (28b) by the intake air (28a). ) Combines various energy storage cycle engines into various automobiles that add gravity acceleration to compression heat recovery.   A turbine blade section (4D) bearing (80) thrust bearing (80a) corresponding to the application is provided, the amount of compressed air heat (28b) is recovered by intake air (28a), and compressed by a heat pump (1G) at 500 to 1000 degrees Various energy storage cycle coalescing engines to make various automobiles with gravity acceleration added to heat recovery etc.   A bearing (80) thrust bearing (80a) corresponding to the application of the turbine blade cross section (4D) is provided, and the heat pump (1G) collects the mercury exhaust heat amount (5A) + compressed air heat amount (28b) by the intake air (28a). ) Various energy storage cycle coalescing engines to make various automobiles with a gravitational acceleration added to heat recovery by compression 500-1000 degrees.   A turbine blade section (4D) bearing (80) thrust bearing (80a) corresponding to the application is provided, the amount of compressed air heat (28b) is recovered by intake air (28a), and compressed by a heat pump (1G) at 500 to 1000 degrees Various energy conservation cycle coalescing engines that recover heat as a drive to drive all rotor blade water turbines and add various types of acceleration to gravity acceleration.   A turbine blade section (4D) bearing (80) thrust bearing (80a) corresponding to the application is provided, the amount of compressed air heat (28b) is recovered by intake air (28a), and compressed by a heat pump (1G) at 500 to 1000 degrees Various energy conservation cycle coalescing engines that recover heat as a driving force and drive all-turbine mercury turbines into various vehicles with additional gravitational acceleration.   A turbine blade section (4D) bearing (80) thrust bearing (80a) corresponding to the application is provided, the amount of compressed air heat (28b) is recovered by intake air (28a), and compressed by a heat pump (1G) at 500 to 1000 degrees Various energy conservation cycle coalescing engines that recover heat as a vehicle and drive all turbine blade gas turbines into various vehicles with additional gravitational acceleration.   The turbine blade cross section (4D) bearing (80) thrust bearing (80a) corresponding to the application is provided, and the carbon fiber is applied to all the portions that are high in temperature when returning to the earth, such as the flying blade (38b) and the flying tail blade (38c). Various energy storage cycle coalescing engines that make water (52a) pipes that have been reduced in weight to high pressure, etc., and make high-pressure lightweight containers into various automobiles that add gravity acceleration to heat recovery.   The turbine blade cross section (4D) bearing (80) thrust bearing (80a) corresponding to the application is provided, and the carbon fiber is applied to all the portions that are high in temperature when returning to the earth, such as the flying blade (38b) and the flying tail blade (38c). Various energy storage cycle coalescing engines that make super high pressure light weight containers into various automobiles that add gravity acceleration to heat recovery by piping superheated steam (50) pipes that have been reduced in weight to high pressure.   The turbine blade cross section (4D) bearing (80) thrust bearing (80a) corresponding to the application is provided, and the carbon fiber is applied to all the portions that are high in temperature when returning to the earth, such as the flying blade (38b) and the flying tail blade (38c). Various energy storage cycle coalescing engines that make high-pressure light weight containers into various automobiles that add gravity acceleration to heat recovery by piping high-temperature mercury (1d) pipes that have been reduced in weight to high pressure.   The turbine blade cross section (4D) bearing (80) thrust bearing (80a) corresponding to the application is provided, and the carbon fiber is applied to all the portions that are high in temperature when returning to the earth, such as the flying blade (38b) and the flying tail blade (38c). Various energy storage cycle coalescence engines that make combustion gas pipes lightened by high pressure, etc., and make high-pressure lightweight containers constitute various automobiles that add gravity acceleration to heat recovery.   The turbine blade cross section (4D) bearing (80) thrust bearing (80a) corresponding to the application is provided, and the carbon nanotubes are formed on all portions of the flying wing (38b), the flying tail (38c), etc., which are heated at the time of return to the earth at the flying speed. Various energy storage cycle coalescing engines that make water (52a) pipes that have been reduced in weight to high pressure, etc., and make high-pressure lightweight containers into various automobiles that add gravity acceleration to heat recovery.   The turbine blade cross section (4D) bearing (80) thrust bearing (80a) corresponding to the application is provided, and the carbon nanotubes are formed on all portions of the flying wing (38b), the flying tail (38c), etc., which are heated at the time of return to the earth at the flying speed. Various energy storage cycle coalescing engines that make super high pressure light weight containers into various automobiles that add gravity acceleration to heat recovery by piping superheated steam (50) pipes that have been reduced in weight to high pressure.   The turbine blade cross section (4D) bearing (80) thrust bearing (80a) corresponding to the application is provided, and the carbon nanotubes are formed on all portions of the flying wing (38b), the flying tail (38c), etc., which are heated at the time of return to the earth at the flying speed. Various energy storage cycle coalescing engines that make high-pressure light weight containers into various automobiles that add gravity acceleration to heat recovery by piping high-temperature mercury (1d) pipes that have been reduced in weight to high pressure.   The turbine blade cross-section (4D) application bearing (80) thrust bearing (80a) is provided, and the flight wing (38b), flight tail (38c) and other parts that become hot at the time of return to the earth at the flight speed are all zero. Various energy conservation cycle coalescing engines that make combustion gas pipes lightened with nanotubes etc., and make high-pressure lightweight containers into various automobiles that add gravity acceleration to heat recovery.   The turbine blade cross section (4D) bearing (80) thrust bearing (80a) corresponding to the application is provided, the combustion gas (49) is recovered by the intake air (28a), and compressed by the heat pump (1G) at 500 to 1000 degrees. Various energy conservation cycle coalescing engines that recover heat as a drive to drive all rotor blade water turbines and add various types of acceleration to gravity acceleration.   The turbine blade cross section (4D) bearing (80) thrust bearing (80a) corresponding to the application is provided, the combustion gas (49) is recovered by the intake air (28a), and compressed by the heat pump (1G) at 500 to 1000 degrees. Various energy conservation cycle coalescing engines that recover heat as a driving force and drive all-turbine mercury turbines into various vehicles with additional gravitational acceleration.   The turbine blade cross section (4D) bearing (80) thrust bearing (80a) corresponding to the application is provided, the combustion gas (49) is recovered by the intake air (28a), and compressed by the heat pump (1G) at 500 to 1000 degrees. Various energy conservation cycle coalescing engines that recover heat as a vehicle and drive all turbine blade gas turbines into various vehicles with additional gravitational acceleration.   The turbine blade cross section (4D) bearing (80) thrust bearing (80a) corresponding to the application is provided, the combustion gas (49) is recovered by the intake air (28a), and compressed by the heat pump (1G) at 500 to 1000 degrees. Various energy storage cycle coalescing engines that recover heat and make the coalesced engine injection part (79K) into various automobiles with gravity acceleration added to drive.   The turbine blade cross section (4D) bearing (80) thrust bearing (80a) corresponding to the application is provided, the combustion gas (49) is recovered by the intake air (28a), and compressed by the heat pump (1G) at 500 to 1000 degrees. Various energy conservation cycle coalescence engines that recover heat as a water jet (79M) all-moving blade mercury turbine to drive various automobiles with added gravitational acceleration.   A turbine blade section (4D) bearing (80) thrust bearing (80a) corresponding to the application is provided, the amount of compressed air heat (28b) is recovered by intake air (28a), and compressed by a heat pump (1G) at 500 to 1000 degrees Various energy storage cycle coalescing engines that recover heat and make the coalesced engine injection part (79K) into various automobiles with gravity acceleration added to drive.   A turbine blade section (4D) bearing (80) thrust bearing (80a) corresponding to the application is provided, the amount of compressed air heat (28b) is recovered by intake air (28a), and compressed by a heat pump (1G) at 500 to 1000 degrees Various energy storage cycle coalescing engines for recovering heat, etc., and converting the water jet (79M) into various automobiles with gravity acceleration added to drive.   A bearing (80) thrust bearing (80a) corresponding to the application is provided to drive a full blade turbine, and a full blade combustion section (32X) vertical blade gas turbine (8A) with a turbine blade cross section (4D) is provided. Various energy conservation cycle coalescing engines that drive various airplanes.   The bearing (80) thrust bearing (80a) corresponding to the application is provided to drive the entire rotor blade turbine, and the entire rotor blade combustion section (32Y) vertical all blade air turbine (8A) of the turbine blade cross section (4D) is provided. Various energy conservation cycle coalescing engines that drive various airplanes.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive a full rotor blade turbine, and a combined engine combustion section (31Y) full rotor blade propeller gas turbine (8a) with a turbine blade cross section (4D) is provided and driven. Various energy conservation cycle coalescing engines for various airplanes.   A bearing (80) thrust bearing (80a) corresponding to the application is provided to drive a full rotor blade turbine, and a combined engine combustion section (31X) full rotor blade propeller gas turbine (8a) with a turbine blade cross section (4D) is provided and driven. Various energy conservation cycle coalescing engines for various airplanes.   A bearing (80) thrust bearing (80a) corresponding to the application is provided to drive a full blade turbine, and a full blade combustion section (32X) vertical blade gas turbine (8A) with a turbine blade cross section (4D) is provided. Various energy conservation cycle coalescing engines that drive various airplanes.   The bearing (80) thrust bearing (80a) corresponding to the application is provided to drive the entire rotor blade turbine, and the entire rotor blade combustion section (32Y) vertical all blade air turbine (8A) of the turbine blade cross section (4D) is provided. Various energy conservation cycle coalescing engines that drive various airplanes.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive a full rotor blade turbine, and a combined engine combustion section (31Y) full rotor blade propeller gas turbine (8a) with a turbine blade cross section (4D) is provided and driven. Various energy conservation cycle coalescing engines for various airplanes.   A bearing (80) thrust bearing (80a) corresponding to the application is provided to drive a full rotor blade turbine, and a combined engine combustion section (31X) full rotor blade propeller gas turbine (8a) with a turbine blade cross section (4D) is provided and driven. Various energy conservation cycle coalescing engines for various airplanes.   A bearing (80) thrust bearing (80a) corresponding to the application is provided to drive a full blade turbine, and a full blade combustion section (32X) vertical blade gas turbine (8A) with a turbine blade cross section (4D) is provided. Various energy conservation cycle coalescing engines that drive various airplanes.   The bearing (80) thrust bearing (80a) corresponding to the application is provided to drive the entire rotor blade turbine, and the entire rotor blade combustion section (32Y) vertical all blade air turbine (8A) of the turbine blade cross section (4D) is provided. Various energy conservation cycle coalescing engines that drive various airplanes.   A bearing (80) thrust bearing (80a) corresponding to the application is provided to drive a full rotor blade turbine, and a combined engine combustion section (31X) full rotor blade propeller gas turbine (8a) with a turbine blade cross section (4D) is provided and driven. Various energy conservation cycle coalescing engines for various airplanes.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive a full rotor blade turbine, and a combined engine combustion section (31Y) full rotor blade propeller gas turbine (8a) with a turbine blade cross section (4D) is provided and driven. Various energy conservation cycle coalescing engines for various airplanes.   A bearing (80) thrust bearing (80a) corresponding to the application is provided to drive a full blade turbine, and a full blade combustion section (32X) vertical blade gas turbine (8A) with a turbine blade cross section (4D) is provided. Various energy conservation cycle coalescing engines that drive various airplanes.   The bearing (80) thrust bearing (80a) corresponding to the application is provided to drive the entire rotor blade turbine, and the entire rotor blade combustion section (32Y) vertical all blade air turbine (8A) of the turbine blade cross section (4D) is provided. Various energy conservation cycle coalescing engines that drive various airplanes.   A bearing (80) thrust bearing (80a) corresponding to the application is provided to drive a full rotor blade turbine, and a combined engine combustion section (31X) full rotor blade propeller gas turbine (8a) with a turbine blade cross section (4D) is provided and driven. Various energy conservation cycle coalescing engines for various airplanes.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive a full rotor blade turbine, and a combined engine combustion section (31Y) full rotor blade propeller gas turbine (8a) with a turbine blade cross section (4D) is provided and driven. Various energy conservation cycle coalescing engines for various airplanes.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all-blade turbines. Combined engine combustion section (31X) full-blade propeller gas turbine (8a) with turbine blade cross section (4D) is around 150 degrees Celsius Various energy storage cycle coalescing engines as various airplanes driven by 24-300 MPa combustion gas (49).   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all-blade turbines. Combined engine combustion section (31Y) full-blade propeller gas turbine (8a) with turbine blade cross section (4D) is around 150 degrees Celsius Various energy storage cycle coalescing engines as various airplanes driven by 24-300 MPa combustion gas (49).   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blades, and all blade combustion section (32X) vertical blade gas turbine (8A) of turbine blade cross section (4D) is 150 degrees Celsius. Various energy storage cycle coalescing engines as various airplanes driven by 24-300 MPa combustion gas (49).   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all-blade turbine, and all-blade combustion section (32Y) vertical all-blade gas turbine (8A) of turbine blade cross section (4D) is 150 degrees Celsius Various energy storage cycle coalescing engines as various airplanes driven by 24-300 MPa combustion gas (49).   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all-blade turbines. Combined engine combustion section (31X) full-blade propeller gas turbine (8a) with turbine blade cross section (4D) is around 200 degrees Celsius Various energy storage cycle coalescing engines as various airplanes driven by 24-300 MPa combustion gas (49).   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all-blade turbines, and the combined engine combustion section (31Y) full-blade propeller gas turbine (8a) in the turbine blade cross section (4D) is around 200 degrees Celsius. Various energy storage cycle coalescing engines as various airplanes driven by 24-300 MPa combustion gas (49).   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines, and the turbine blade cross section (4D) full blade combustion section (32X) vertical all blade gas turbine (8A) is 200 degrees Celsius. Various energy storage cycle coalescing engines as various airplanes driven by 24-300 MPa combustion gas (49).   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbine, and all blade combustion section (32Y) vertical all blade gas turbine (8A) of turbine blade cross section (4D) is 200 degrees Celsius. Various energy storage cycle coalescing engines as various airplanes driven by 24-300 MPa combustion gas (49).   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbine, and all blade combustion section (32X) vertical all blade gas turbine (8A) of turbine blade cross section (4D) is 300 degrees Celsius. Various energy storage cycle coalescing engines as various airplanes driven by 24-300 MPa combustion gas (49).   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbine, and all blade combustion section (32Y) vertical blade gas turbine (8A) of turbine blade cross section (4D) is 300 degrees Celsius. Various energy storage cycle coalescing engines as various airplanes driven by 24-300 MPa combustion gas (49).   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all-blade turbines. Combined engine combustion section (31X) full-blade propeller gas turbine (8a) with turbine blade cross section (4D) is around 300 degrees Celsius Various energy storage cycle coalescing engines as various airplanes driven by 24-300 MPa combustion gas (49).   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all-blade turbines. Combined engine combustion section (31Y) full-blade propeller gas turbine (8a) with turbine blade cross section (4D) is around 300 degrees Celsius Various energy storage cycle coalescing engines as various airplanes driven by 24-300 MPa combustion gas (49).   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided to drive the entire rotor blade, and the combined engine combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven to a high-pressure turbine below the critical temperature. Various energy storage cycle coalescing engines with various types of airplanes that consume approximately 1/72 of heat.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided to drive all blades, and the combined engine combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven to a high-pressure turbine below the critical temperature. Various energy storage cycle coalescing engines with various types of airplanes that consume approximately 1/72 of heat.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbine, and all blade combustion section (32X) high-temperature mercury (1d) of turbine blade cross section (4D) is driven to high pressure turbine below critical temperature Various energy storage cycle coalescing engines with various types of airplanes that reduce heat consumption to approximately 1/72.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all blades, and all blade combustion parts (32Y) high-temperature mercury (1d) in the turbine blade cross section (4D) are driven to high pressure turbines below the critical temperature. Various energy storage cycle coalescing engines with various types of airplanes that reduce heat consumption to approximately 1/72.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all rotor blade turbines, and the turbine blade cross section (4D) full rotor blade combustion section (32X) high-temperature mercury (1d) is 1000 degrees Celsius or less high-pressure turbine Various energy storage cycle coalescing engines that are driven to reduce the amount of heat consumed to approximately 1/72.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all blades, and all blade combustion parts (32Y) high-temperature mercury (1d) in the turbine blade cross-section (4D) is 1000 degrees Celsius or less. Various energy storage cycle coalescing engines that are driven to reduce the amount of heat consumed to approximately 1/72.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines. Combined engine combustion section (31X) high-temperature mercury (1d) of turbine blade cross section (4D) is driven to high-pressure turbine at 1000 degrees Celsius or less Various energy storage cycle coalescing engines with various types of airplanes that reduce heat consumption to approximately 1/72.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blades, and the combined combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven to a high-pressure turbine at 1000 degrees Celsius or less. Various energy storage cycle coalescing engines with various types of airplanes that reduce heat consumption to approximately 1/72.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blades, and the combined combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven to a high-pressure turbine at 800 degrees Celsius or less. Various energy storage cycle coalescing engines with various types of airplanes that reduce heat consumption to approximately 1/72.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all blades, and the combined engine combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven to a high-pressure turbine at 800 degrees Celsius or less. Various energy storage cycle coalescing engines with various types of airplanes that reduce heat consumption to approximately 1/72.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines, and all blade combustion section (32X) high-temperature mercury (1d) of turbine blade cross section (4D) is high pressure turbine at 800 degrees Celsius or less Various energy storage cycle coalescing engines that are driven to reduce the amount of heat consumed to approximately 1/72.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbine, and all blade combustion section (32Y) high temperature mercury (1d) of turbine blade cross section (4D) is high pressure turbine at 800 degrees centigrade or less Various energy storage cycle coalescing engines that are driven to reduce the amount of heat consumed to approximately 1/72.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbine, and all blade combustion section (32X) high-temperature mercury (1d) of turbine blade cross section (4D) is high pressure turbine at 600 degrees Celsius or less Various energy storage cycle coalescing engines that are driven to reduce the amount of heat consumed to approximately 1/72.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines, and all blade combustion section (32Y) high-temperature mercury (1d) in turbine blade cross section (4D) is high-pressure turbine at 600 degrees Celsius or less Various energy storage cycle coalescing engines that are driven to reduce the amount of heat consumed to approximately 1/72.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all blade turbines, and the combined combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven to a high-pressure turbine at 600 degrees Celsius or less. Various energy storage cycle coalescing engines with various types of airplanes that reduce heat consumption to approximately 1/72.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all blades, and the combined combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven to a high-pressure turbine at 600 degrees Celsius or less. Various energy storage cycle coalescing engines with various types of airplanes that reduce heat consumption to approximately 1/72.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided to drive the turbine blade, and the combined engine combustion section (31X) high-temperature water (52b) of the turbine blade cross section (4D) is driven to a high-pressure turbine below the critical temperature. Various energy storage cycle coalescing engines with various types of airplanes that reduce heat consumption to approximately 1/539.   A bearing (80) for thrust application (80a) is provided to drive the entire rotor blade turbine, and the combined engine combustion section (31Y) high-temperature water (52b) in the turbine blade cross section (4D) is driven to a high-pressure turbine below the critical temperature. Various energy storage cycle coalescing engines with various types of airplanes that reduce heat consumption to approximately 1/539.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines, and all blade combustion section (32X) high-temperature water (52b) on turbine blade cross section (4D) is driven to high pressure turbine below critical temperature As a result, various types of energy storage cycle coalescing engines that reduce the amount of heat consumed to approximately 1/539, etc.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all blades, and all blade combustion parts (32Y) high-temperature water (52b) in the turbine blade cross section (4D) is driven to high pressure turbine below the critical temperature. As a result, various types of energy storage cycle coalescing engines that reduce the amount of heat consumed to approximately 1/539, etc.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines, and all blade combustion section (32X) of turbine blade cross section (4D) is driven to high-pressure turbine by high-temperature water (52b) to consume heat. Various energy conservation cycle coalescing engines, which are various airplanes that reduce the size to approximately 1/539.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines, and all blade combustion section (32Y) high temperature water (52b) in turbine blade cross section (4D) to drive high pressure turbine to consume heat Various energy conservation cycle coalescing engines, which are various airplanes with a 1/539 grade.   A bearing (80) thrust bearing (80a) corresponding to the application is provided to drive the entire rotor blade turbine, and the high pressure turbine is driven by the combined engine combustion section (31X) high temperature water (52b) of the turbine blade cross section (4D) to reduce the amount of heat consumed. Various energy conservation cycle coalescing engines, which are various airplanes of about 1/539 etc.   A bearing (80) thrust bearing (80a) corresponding to the application is provided to drive the entire rotor blade turbine, and the high pressure turbine is driven by the combined engine combustion section (31Y) high temperature water (52b) of the turbine blade cross section (4D) to reduce the amount of heat consumed. Various energy conservation cycle coalescing engines, which are various airplanes of about 1/539 etc.   Provided bearing (80) thrust bearing (80a) for all applications to drive all rotor blade turbines, high pressure turbine driven by combined engine combustion section (31X) high temperature water (52b) of turbine blade cross section (4D) Various energy storage cycle coalescing engines with various speeds that make the speed output 1700 times kg weight m / sec of steam drive.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are used to drive the entire rotor blade, and the high pressure turbine is driven by the combined engine combustion section (31Y) high-temperature water (52b) in the turbine blade cross section (4D). Various energy storage cycle coalescing engines with various speeds that make the speed output 1700 times kg weight m / sec of steam drive.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbine, and all blade combustion section (32X) of turbine blade cross section (4D) is driven to high pressure turbine by high temperature water (52b) and atmospheric pressure Various energy storage cycle coalescing engines with various speeds that make the same speed output 1700 times kg weight m / sec of steam drive.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbine, and all blade combustion section (32Y) of turbine blade cross section (4D) is driven to high pressure turbine by high temperature water (52b) and atmospheric pressure Various energy storage cycle coalescing engines with various speeds that make the same speed output 1700 times kg weight m / sec of steam drive.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all rotor blade turbines, and all blade combustion sections (32X) of turbine blade cross section (4D) are driven to high-pressure turbine by high-temperature mercury (1d) and atmospheric pressure Various energy storage cycle coalescing engines with various speeds that make the speed output 23,000 times the weight of steam driven m / s.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbine, and all blade combustion section (32Y) of turbine blade cross section (4D) is driven to high-pressure turbine by high-temperature mercury (1d) and atmospheric pressure Various energy storage cycle coalescing engines with various speeds that make the speed output 23,000 times the weight of steam driven m / s.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines. Combined engine combustion part (31X) of turbine blade cross section (4D) High-pressure turbine drive with high-temperature mercury (1d) Various energy storage cycle coalescing engines with various speeds that make the speed output 23,000 times kg weight m / sec of steam drive.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines. Combined engine combustion section (31Y) of turbine blade cross section (4D) High-pressure turbine drive with high-temperature mercury (1d) Various energy storage cycle coalescing engines with various speeds that make the speed output 23,000 times kg weight m / sec of steam drive.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines. Combined engine combustion part (31X) of turbine blade cross section (4D) High-pressure turbine drive with high-temperature mercury (1d) Various energy storage cycle coalescing engines with a speed output of 23,000 times the weight of steam driven by steam and a gravity acceleration of 9.8 m / second and additional heat, electricity and cold supply facilities per second.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines. Combined engine combustion section (31Y) of turbine blade cross section (4D) High-pressure turbine drive with high-temperature mercury (1d) Various energy storage cycle coalescing engines with a speed output of 23,000 times the weight of steam driven by steam and a gravity acceleration of 9.8 m / second and additional heat, electricity and cold supply facilities per second.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all rotor blade turbines, and all blade combustion sections (32X) of turbine blade cross section (4D) are driven to high-pressure turbine by high-temperature mercury (1d) and atmospheric pressure Various energy storage cycle coalescing engines with the same speed output, 23,000 times the weight of steam driven kg weight m / sec, and a gravitational acceleration of 9.8 m / sec and additional heat, electricity and cold supply facilities per second.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbine, and all blade combustion section (32Y) of turbine blade cross section (4D) is driven to high-pressure turbine by high-temperature mercury (1d) and atmospheric pressure Various energy storage cycle coalescing engines with the same speed output, 23,000 times the weight of steam driven kg weight m / sec, and a gravitational acceleration of 9.8 m / sec and additional heat, electricity and cold supply facilities per second.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all rotor blade turbines, and all blade combustion sections (32X) of turbine blade cross section (4D) are driven to high-pressure turbine by high-temperature mercury (1d) and atmospheric pressure Various energy conservation cycle coalescing engines with various speeds, 23,000 times the weight of steam driven by the steam, and 9.8m / s of gravity acceleration added per second.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbine, and all blade combustion section (32Y) of turbine blade cross section (4D) is driven to high-pressure turbine by high-temperature mercury (1d) and atmospheric pressure Various energy conservation cycle coalescing engines with various speeds, 23,000 times the weight of steam driven by the steam, and 9.8m / s of gravity acceleration added per second.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines. Combined engine combustion part (31X) of turbine blade cross section (4D) High-pressure turbine drive with high-temperature mercury (1d) Various energy storage cycle coalescing engines that make the speed output 23,000 times the weight of water vapor driven kg weight m / second and the gravitational acceleration 9.8m / second addition every second.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines. Combined engine combustion section (31Y) of turbine blade cross section (4D) High-pressure turbine drive with high-temperature mercury (1d) Various energy storage cycle coalescing engines that make the speed output 23,000 times the weight of water vapor driven kg weight m / second and the gravitational acceleration 9.8m / second addition every second.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines. Combined engine combustion part (31X) of turbine blade cross section (4D) High-pressure turbine drive with high-temperature mercury (1d) Various energy conservation cycle coalescing engines that make speed output 23,000 times the weight of water vapor driven kg weight m / second and gravitational acceleration 9.8m / second addition every second.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines. Combined engine combustion section (31Y) of turbine blade cross section (4D) High-pressure turbine drive with high-temperature mercury (1d) Various energy conservation cycle coalescing engines that make speed output 23,000 times the weight of water vapor driven kg weight m / second and gravitational acceleration 9.8m / second addition every second.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all rotor blade turbines, and all blade combustion sections (32X) of turbine blade cross section (4D) are driven to high-pressure turbine by high-temperature mercury (1d) and atmospheric pressure Various energy conservation cycle coalescing engines that have the same speed output, 23,000 times the weight of water vapor driven kg weight m / second, and a variety of airplanes with a gravitational acceleration of 9.8 m / second per second.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbine, and all blade combustion section (32Y) of turbine blade cross section (4D) is driven to high-pressure turbine by high-temperature mercury (1d) and atmospheric pressure Various energy conservation cycle coalescing engines that have the same speed output, 23,000 times the weight of water vapor driven kg weight m / second, and a variety of airplanes with a gravitational acceleration of 9.8 m / second per second.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbine, and all blade combustion section (32X) of turbine blade cross section (4D) is driven to high pressure turbine by high temperature water (52b) and atmospheric pressure Various energy conservation cycle coalescing engines that make various airplanes equipped with the same speed output 1700 times kg weight m / second of steam drive and gravity acceleration 9.8m / second addition per second.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbine, and all blade combustion section (32Y) of turbine blade cross section (4D) is driven to high pressure turbine by high temperature water (52b) and atmospheric pressure Various energy conservation cycle coalescing engines that make various airplanes equipped with the same speed output 1700 times kg weight m / second of steam drive and gravity acceleration 9.8m / second addition per second.   Provided bearing (80) thrust bearing (80a) for all applications to drive all rotor blade turbines, high pressure turbine driven by combined engine combustion section (31X) high temperature water (52b) of turbine blade cross section (4D) Various energy conservation cycle coalescing engines that make speed output 1700 times the weight of steam-driven m / s and gravity acceleration of 9.8m / s per second added to various airplanes.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are used to drive the entire rotor blade, and the high pressure turbine is driven by the combined engine combustion section (31Y) high-temperature water (52b) in the turbine blade cross section (4D). Various energy conservation cycle coalescing engines that make speed output 1700 times the weight of steam-driven m / s and gravity acceleration of 9.8m / s per second added to various airplanes.   Provided bearing (80) thrust bearing (80a) for all applications to drive all rotor blade turbines, high pressure turbine driven by combined engine combustion section (31X) high temperature water (52b) of turbine blade cross section (4D) Various energy conservation cycle coalescing engines with various kinds of ships equipped with a speed output of 1700 times the weight of steam driven and weighing 9.8 m / s per second per second.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are used to drive the entire rotor blade, and the high pressure turbine is driven by the combined engine combustion section (31Y) high-temperature water (52b) in the turbine blade cross section (4D). Various energy conservation cycle coalescing engines with various kinds of ships equipped with a speed output of 1700 times the weight of steam driven and weighing 9.8 m / s per second per second.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbine, and all blade combustion section (32X) of turbine blade cross section (4D) is driven to high pressure turbine by high temperature water (52b) and atmospheric pressure Various energy conservation cycle coalescing engines that make the same speed output 1700 times the weight of steam-driven 1 kg weight m / second and gravitation acceleration 9.8m / second addition every second.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbine, and all blade combustion section (32Y) of turbine blade cross section (4D) is driven to high pressure turbine by high temperature water (52b) and atmospheric pressure Various energy conservation cycle coalescing engines that make the same speed output 1700 times the weight of steam-driven 1 kg weight m / second and gravitation acceleration 9.8m / second addition every second.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbine, and all blade combustion section (32X) of turbine blade cross section (4D) is driven to high pressure turbine by high temperature water (52b) and atmospheric pressure Various energy storage cycle coalescing engines that use the same speed output as the supply equipment for various heat, electricity, and cold at 1,700 times the weight of steam driven m / sec.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbine, and all blade combustion section (32Y) of turbine blade cross section (4D) is driven to high pressure turbine by high temperature water (52b) and atmospheric pressure Various energy storage cycle coalescing engine that makes the same speed output 1700 times kg weight m / sec of steam drive and gravitational acceleration 9.8m / sec and additional heat, electricity and cold supply facilities.   Provided bearing (80) thrust bearing (80a) for all applications to drive all rotor blade turbines, high pressure turbine driven by combined engine combustion section (31X) high temperature water (52b) of turbine blade cross section (4D) Various energy storage cycle coalescence engine that makes the speed output 1700 times kg weight m / sec of steam drive and gravitational acceleration 9.8m / sec and additional heat, electricity and cold supply facilities.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are used to drive the entire rotor blade, and the high pressure turbine is driven by the combined engine combustion section (31Y) high-temperature water (52b) in the turbine blade cross section (4D). Various energy storage cycle coalescence engine that makes the speed output 1700 times kg weight m / sec of steam drive and gravitational acceleration 9.8m / sec and additional heat, electricity and cold supply facilities.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided to drive the entire rotor blade, and the combined engine combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven to a high-pressure turbine below the critical temperature. Various energy storage cycle coalescing engines with a heat supply of approximately 1/72 and a gravitational acceleration of 9.8 m / sec.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided to drive all blades, and the combined engine combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven to a high-pressure turbine below the critical temperature. Various energy storage cycle coalescing engines with a heat supply of approximately 1/72 and a gravitational acceleration of 9.8 m / sec.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbine, and all blade combustion section (32X) high-temperature mercury (1d) of turbine blade cross section (4D) is driven to high pressure turbine below critical temperature Various energy storage cycle coalescence engines that use a heat / electricity / cold heat supply facility with a gravitational acceleration of 9.8 m / sec.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all blades, and all blade combustion parts (32Y) high-temperature mercury (1d) in the turbine blade cross section (4D) are driven to high pressure turbines below the critical temperature. Various energy storage cycle coalescence engines that use a heat / electricity / cold heat supply facility with a gravitational acceleration of 9.8 m / sec.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbine, and all blade combustion section (32X) high-temperature mercury (1d) of turbine blade cross section (4D) is driven to high pressure turbine below critical temperature Various energy storage cycle coalescing engines to make various ships by adding a gravitational acceleration of 9.8 m / sec.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all blades, and all blade combustion parts (32Y) high-temperature mercury (1d) in the turbine blade cross section (4D) are driven to high pressure turbines below the critical temperature. Various energy storage cycle coalescing engines to make various ships by adding a gravitational acceleration of 9.8 m / sec.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided to drive the entire rotor blade, and the combined engine combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven to a high-pressure turbine below the critical temperature. Various energy storage cycle coalescing engines with various caloric consumption by adding 9.8m / s / sec to a gravitational acceleration of approximately 1/72 etc.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided to drive all blades, and the combined engine combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven to a high-pressure turbine below the critical temperature. Various energy storage cycle coalescing engines with various caloric consumption by adding 9.8m / s / sec to a gravitational acceleration of approximately 1/72 etc.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided to drive the entire rotor blade, and the combined engine combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven to a high-pressure turbine below the critical temperature Various energy storage cycle coalescing engines with various heat planes by adding a gravitational acceleration of 9.8 m / second per second to approximately 1/72 etc.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided to drive all blades, and the combined engine combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven to a high-pressure turbine below the critical temperature. Various energy storage cycle coalescing engines with various heat planes by adding a gravitational acceleration of 9.8 m / second per second to approximately 1/72 etc.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbine, and all blade combustion section (32X) high-temperature mercury (1d) of turbine blade cross section (4D) is driven to high pressure turbine below critical temperature Various energy storage cycle coalescing engines to make various airplanes by adding a gravitational acceleration of 9.8 m / sec.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all blades, and all blade combustion parts (32Y) high-temperature mercury (1d) in the turbine blade cross section (4D) are driven to high pressure turbines below the critical temperature. Various energy storage cycle coalescing engines to make various airplanes by adding a gravitational acceleration of 9.8 m / sec.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all rotor blade turbines, and the turbine blade cross section (4D) full rotor blade combustion section (32X) high-temperature mercury (1d) is 1000 degrees Celsius or less high-pressure turbine Various energy conservation cycle coalescing engines that are driven to make various types of airplanes with a gravitational acceleration of 9.8 m / sec.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all blades, and all blade combustion parts (32Y) high-temperature mercury (1d) in the turbine blade cross-section (4D) is 1000 degrees Celsius or less. Various energy conservation cycle coalescing engines that are driven to make various types of airplanes with a gravitational acceleration of 9.8 m / sec.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines. Combined engine combustion section (31X) high-temperature mercury (1d) of turbine blade cross section (4D) is driven to high-pressure turbine at 1000 degrees Celsius or less Various energy storage cycle coalescing engines that make various types of airplanes with a gravitational acceleration of 9.8 m / sec.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blades, and the combined combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven to a high-pressure turbine at 1000 degrees Celsius or less. Various energy storage cycle coalescing engines that make various types of airplanes with a gravitational acceleration of 9.8 m / sec.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines. Combined engine combustion section (31X) high-temperature mercury (1d) of turbine blade cross section (4D) is driven to high-pressure turbine at 1000 degrees Celsius or less Various energy storage cycle coalescing engines that make the various kinds of ships added to a gravitational acceleration of 9.8 m / sec.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blades, and the combined combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven to a high-pressure turbine at 1000 degrees Celsius or less. Various energy storage cycle coalescing engines that make the various kinds of ships added to a gravitational acceleration of 9.8 m / sec.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all rotor blade turbines, and the turbine blade cross section (4D) full rotor blade combustion section (32X) high-temperature mercury (1d) is 1000 degrees Celsius or less high-pressure turbine Various energy storage cycle coalescing engines that drive to make various types of ships with a gravitational acceleration of 9.8 m / sec.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all blades, and all blade combustion parts (32Y) high-temperature mercury (1d) in the turbine blade cross-section (4D) is 1000 degrees Celsius or less. Various energy storage cycle coalescing engines that drive to make various types of ships with a gravitational acceleration of 9.8 m / sec.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all rotor blade turbines, and the turbine blade cross section (4D) full rotor blade combustion section (32X) high-temperature mercury (1d) is 1000 degrees Celsius or less high-pressure turbine Various energy storage cycle coalescing engines that drive to make various heat, electricity and cold supply facilities with a gravitational acceleration of 9.8 m / second per second and a heat consumption of approximately 1/72.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all blades, and all blade combustion parts (32Y) high-temperature mercury (1d) in the turbine blade cross-section (4D) is 1000 degrees Celsius or less. Various energy storage cycle coalescing engines that drive to make various heat, electricity and cold supply facilities with a gravitational acceleration of 9.8 m / second per second and a heat consumption of approximately 1/72.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all rotor blade turbines. Combined engine combustion section (31X) high-temperature mercury (1d) of turbine blade cross section (4D) is driven to high-pressure turbine at 1000 degrees Celsius or less As a result, the energy storage cycle coalescing engine has a heat consumption of approximately 1/72 and the gravitational acceleration is 9.8 m / sec.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blades, and the combined combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven to a high-pressure turbine at 1000 degrees Celsius or less. As a result, the energy storage cycle coalescing engine has a heat consumption of approximately 1/72 and the gravitational acceleration is 9.8 m / sec.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines. Combined engine combustion section (31X) high-temperature mercury (1d) of turbine blade cross section (4D) is driven to high-pressure turbine at 800 degrees Celsius or less As a result, the energy storage cycle coalescing engine has a heat consumption of approximately 1/72 and the gravitational acceleration is 9.8 m / sec.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all blades, and the combined engine combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven to a high-pressure turbine at 800 degrees Celsius or less. As a result, the energy storage cycle coalescing engine has a heat consumption of approximately 1/72 and the gravitational acceleration is 9.8 m / sec.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines, and all blade combustion section (32X) high-temperature mercury (1d) of turbine blade cross section (4D) is high pressure turbine at 800 degrees Celsius or less Various energy storage cycle coalescing engines that drive to make various heat, electricity and cold supply facilities with a gravitational acceleration of 9.8 m / second per second and a heat consumption of approximately 1/72.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbine, and all blade combustion section (32Y) high temperature mercury (1d) of turbine blade cross section (4D) is high pressure turbine at 800 degrees centigrade or less Various energy storage cycle coalescing engines that drive to make various heat, electricity and cold supply facilities with a gravitational acceleration of 9.8 m / second per second and a heat consumption of approximately 1/72.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines, and all blade combustion section (32X) high-temperature mercury (1d) of turbine blade cross section (4D) is high pressure turbine at 800 degrees Celsius or less Various energy storage cycle coalescing engines that drive to make various types of ships with a gravitational acceleration of 9.8 m / sec.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbine, and all blade combustion section (32Y) high temperature mercury (1d) of turbine blade cross section (4D) is high pressure turbine at 800 degrees centigrade or less Various energy storage cycle coalescing engines that drive to make various types of ships with a gravitational acceleration of 9.8 m / sec.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blades, and the combined combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven to a high-pressure turbine at 800 degrees Celsius or less. Various energy storage cycle coalescing engines that make the various kinds of ships added to a gravitational acceleration of 9.8 m / sec.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all blades, and the combined engine combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven to a high-pressure turbine at 800 degrees Celsius or less. Various energy storage cycle coalescing engines that make the various kinds of ships added to a gravitational acceleration of 9.8 m / sec.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blades, and the combined combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven to a high-pressure turbine at 800 degrees Celsius or less. Various energy storage cycle coalescing engines that make various types of airplanes with a gravitational acceleration of 9.8 m / sec.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all blades, and the combined engine combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven to a high-pressure turbine at 800 degrees Celsius or less. Various energy storage cycle coalescing engines that make various types of airplanes with a gravitational acceleration of 9.8 m / sec.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines, and all blade combustion section (32X) high-temperature mercury (1d) of turbine blade cross section (4D) is high pressure turbine at 800 degrees Celsius or less Various energy conservation cycle coalescing engines that are driven to make various types of airplanes with a gravitational acceleration of 9.8 m / sec.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbine, and all blade combustion section (32Y) high temperature mercury (1d) of turbine blade cross section (4D) is high pressure turbine at 800 degrees centigrade or less Various energy conservation cycle coalescing engines that are driven to make various types of airplanes with a gravitational acceleration of 9.8 m / sec.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbine, and all blade combustion section (32X) high-temperature mercury (1d) of turbine blade cross section (4D) is high pressure turbine at 600 degrees Celsius or less Various energy conservation cycle coalescing engines that are driven to make various types of airplanes with a gravitational acceleration of 9.8 m / sec.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines, and all blade combustion section (32Y) high-temperature mercury (1d) in turbine blade cross section (4D) is high-pressure turbine at 600 degrees Celsius or less Various energy conservation cycle coalescing engines that are driven to make various types of airplanes with a gravitational acceleration of 9.8 m / sec.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all blade turbines, and the combined combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven to a high-pressure turbine at 600 degrees Celsius or less. Various energy storage cycle coalescing engines that make various types of airplanes with a gravitational acceleration of 9.8 m / sec.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all blades, and the combined combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven to a high-pressure turbine at 600 degrees Celsius or less. Various energy storage cycle coalescing engines that make various types of airplanes with a gravitational acceleration of 9.8 m / sec.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all blade turbines, and the combined combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven to a high-pressure turbine at 600 degrees Celsius or less. Various energy storage cycle coalescing engines that make the various kinds of ships added to a gravitational acceleration of 9.8 m / sec.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines. Combined engine combustion section (31Y) high-temperature mercury (1d) of turbine blade cross section (4D) is driven to high-pressure turbine at 600 degrees Celsius or less Various energy storage cycle coalescing engines that make the various kinds of ships added to a gravitational acceleration of 9.8 m / sec.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbine, and all blade combustion section (32X) high-temperature mercury (1d) of turbine blade cross section (4D) is high pressure turbine at 600 degrees Celsius or less Various energy storage cycle coalescing engines that drive to make various types of ships with a gravitational acceleration of 9.8 m / sec.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines, and all blade combustion section (32Y) high-temperature mercury (1d) in turbine blade cross section (4D) is high-pressure turbine at 600 degrees Celsius or less Various energy storage cycle coalescing engines that drive to make various types of ships with a gravitational acceleration of 9.8 m / sec.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbine, and all blade combustion section (32X) high-temperature mercury (1d) of turbine blade cross section (4D) is high pressure turbine at 600 degrees Celsius or less Various energy storage cycle coalescing engines that drive to make various heat, electricity and cold supply facilities with a gravitational acceleration of 9.8 m / second per second and a heat consumption of approximately 1/72.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines, and all blade combustion section (32Y) high-temperature mercury (1d) in turbine blade cross section (4D) is high-pressure turbine at 600 degrees Celsius or less Various energy storage cycle coalescing engines that drive to make various heat, electricity and cold supply facilities with a gravitational acceleration of 9.8 m / second per second and a heat consumption of approximately 1/72.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all blade turbines, and the combined combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven to a high-pressure turbine at 600 degrees Celsius or less. As a result, the energy storage cycle coalescing engine has a heat consumption of approximately 1/72 and the gravitational acceleration is 9.8 m / sec.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines. Combined engine combustion section (31Y) high-temperature mercury (1d) of turbine blade cross section (4D) is driven to high-pressure turbine at 600 degrees Celsius or less As a result, the energy storage cycle coalescing engine has a heat consumption of approximately 1/72 and the gravitational acceleration is 9.8 m / sec.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided to drive the turbine blade, and the combined engine combustion section (31X) high-temperature water (52b) of the turbine blade cross section (4D) is driven to a high-pressure turbine below the critical temperature Combined with various energy storage cycle engines that make the heat consumption approximately 1/539, etc., and the acceleration of gravity is 9.8 m / sec.   A bearing (80) for thrust application (80a) is provided to drive the entire rotor blade turbine, and the combined engine combustion section (31Y) high-temperature water (52b) in the turbine blade cross section (4D) is driven to a high-pressure turbine below the critical temperature. Combined with various energy storage cycle engines that make the heat consumption approximately 1/539, etc., and the acceleration of gravity is 9.8 m / sec.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines, and all blade combustion section (32X) high-temperature water (52b) on turbine blade cross section (4D) is driven to high pressure turbine below critical temperature As a result, a combined energy storage cycle engine with a heat consumption of approximately 1/539, a gravitational acceleration of 9.8 m / second, and various additional heat, electricity, and cold supply facilities.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all blades, and all blade combustion parts (32Y) high-temperature water (52b) in the turbine blade cross section (4D) is driven to high pressure turbine below the critical temperature. As a result, a combined energy storage cycle engine with a heat consumption of approximately 1/539, a gravitational acceleration of 9.8 m / second, and various additional heat, electricity, and cold supply facilities.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines, and all blade combustion section (32X) high-temperature water (52b) on turbine blade cross section (4D) is driven to high pressure turbine below critical temperature Various energy storage cycle coalescing engines, which make the amount of heat consumed approximately 1/539, etc., and gravitational acceleration of 9.8 m / second and additional ships per second.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all blades, and all blade combustion parts (32Y) high-temperature water (52b) in the turbine blade cross section (4D) is driven to high pressure turbine below the critical temperature. Various energy storage cycle coalescing engines, which make the amount of heat consumed approximately 1/539, etc., and gravitational acceleration of 9.8 m / second and additional ships per second.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided to drive the turbine blade, and the combined engine combustion section (31X) high-temperature water (52b) of the turbine blade cross section (4D) is driven to a high-pressure turbine below the critical temperature. Various energy conservation cycle coalescing engines that make the amount of heat consumed approximately 1/539, etc., and gravitational acceleration of 9.8 m / second and additional ships per second.   A bearing (80) for thrust application (80a) is provided to drive the entire rotor blade turbine, and the combined engine combustion section (31Y) high-temperature water (52b) in the turbine blade cross section (4D) is driven to a high-pressure turbine below the critical temperature. Various energy conservation cycle coalescing engines that make the amount of heat consumed approximately 1/539, etc., and gravitational acceleration of 9.8 m / second and additional ships per second.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided to drive the turbine blade, and the combined engine combustion section (31X) high-temperature water (52b) of the turbine blade cross section (4D) is driven to a high-pressure turbine below the critical temperature Various energy storage cycle coalescing engines that make the various types of airplanes with a gravitational acceleration of 9.8 m / sec.   A bearing (80) for thrust application (80a) is provided to drive the entire rotor blade turbine, and the combined engine combustion section (31Y) high-temperature water (52b) in the turbine blade cross section (4D) is driven to a high-pressure turbine below the critical temperature. Various energy storage cycle coalescing engines that make the various types of airplanes with a gravitational acceleration of 9.8 m / sec.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines, and all blade combustion section (32X) high-temperature water (52b) on turbine blade cross section (4D) is driven to high pressure turbine below critical temperature Various energy conservation cycle coalescing engines that make the various types of airplanes with a gravitational acceleration of 9.8 m / sec and an additional heat consumption of approximately 1/539, etc.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all blades, and all blade combustion parts (32Y) high-temperature water (52b) in the turbine blade cross section (4D) is driven to high pressure turbine below the critical temperature. Various energy conservation cycle coalescing engines that make the various types of airplanes with a gravitational acceleration of 9.8 m / sec and an additional heat consumption of approximately 1/539, etc.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines, and all blade combustion section (32X) of turbine blade cross section (4D) is driven to high-pressure turbine by high-temperature water (52b) to consume heat. Various energy conservation cycle coalescing engines which make various airplanes with a gravitational acceleration of 9.8 m / sec.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines, and all blade combustion section (32Y) high temperature water (52b) in turbine blade cross section (4D) to drive high pressure turbine to consume heat Various energy conservation cycle coalescing engines which make various airplanes with a gravitational acceleration of 9.8 m / sec.   A bearing (80) thrust bearing (80a) corresponding to the application is provided to drive the entire rotor blade turbine, and the high pressure turbine is driven by the combined engine combustion section (31X) high temperature water (52b) of the turbine blade cross section (4D) to reduce the amount of heat consumed. Various energy storage cycle coalescing engines that make various airplanes with gravity acceleration of 9.8m / sec.   A bearing (80) thrust bearing (80a) corresponding to the application is provided to drive the entire rotor blade turbine, and the high pressure turbine is driven by the combined engine combustion section (31Y) high temperature water (52b) of the turbine blade cross section (4D) to reduce the amount of heat consumed. Various energy storage cycle coalescing engines that make various airplanes with gravity acceleration of 9.8m / sec.   A bearing (80) thrust bearing (80a) corresponding to the application is provided to drive the entire rotor blade turbine, and the high pressure turbine is driven by the combined engine combustion section (31X) high temperature water (52b) of the turbine blade cross section (4D) to reduce the amount of heat consumed. Various energy conservation cycle coalescing engines to make various ships of about 1/539 etc. with a gravitational acceleration of 9.8 m / second per second.   A bearing (80) thrust bearing (80a) corresponding to the application is provided to drive the entire rotor blade turbine, and the high pressure turbine is driven by the combined engine combustion section (31Y) high temperature water (52b) of the turbine blade cross section (4D) to reduce the amount of heat consumed. Various energy conservation cycle coalescing engines to make various ships of about 1/539 etc. with a gravitational acceleration of 9.8 m / second per second.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines, and all blade combustion section (32X) of turbine blade cross section (4D) is driven to high-pressure turbine by high-temperature water (52b) to consume heat. Various energy conservation cycle coalescing engines that make gravity acceleration 9.8m / sec.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines, and all blade combustion section (32Y) high temperature water (52b) in turbine blade cross section (4D) to drive high pressure turbine to consume heat Various energy conservation cycle coalescing engines that make gravity acceleration 9.8m / sec.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines, and all blade combustion section (32X) of turbine blade cross section (4D) is driven to high-pressure turbine by high-temperature water (52b) to consume heat. Various energy storage cycle coalescing engines which make the supply of various heat, electricity and cold to about 1/539 etc. and gravity acceleration 9.8m / second per second.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines, and all blade combustion section (32Y) high temperature water (52b) in turbine blade cross section (4D) to drive high pressure turbine to consume heat Various energy storage cycle coalescing engines which make the supply of various heat, electricity and cold to about 1/539 etc. and gravity acceleration 9.8m / second per second.   A bearing (80) thrust bearing (80a) corresponding to the application is provided to drive the entire rotor blade turbine, and the high pressure turbine is driven by the combined engine combustion section (31X) high temperature water (52b) of the turbine blade cross section (4D) to reduce the amount of heat consumed. Various energy storage cycle coalescing engines that provide various heat, electricity, and cold supply facilities of about 1/539 etc. with a gravitational acceleration of 9.8 m / sec.   A bearing (80) thrust bearing (80a) corresponding to the application is provided to drive the entire rotor blade turbine, and the high pressure turbine is driven by the combined engine combustion section (31Y) high temperature water (52b) of the turbine blade cross section (4D) to reduce the amount of heat consumed. Various energy storage cycle coalescing engines that provide various heat, electricity, and cold supply facilities of about 1/539 etc. with a gravitational acceleration of 9.8 m / sec.   Provided bearing (80) thrust bearing (80a) for all applications to drive all rotor blade turbines, high pressure turbine driven by combined engine combustion section (31X) high temperature water (52b) of turbine blade cross section (4D) Various energy conservation cycle coalescence engine that makes the output of the same heat speed 1700 times kg weight m / sec * 539 = about 910,000 times of steam drive and makes various heat, electricity and cold supply facilities with gravity acceleration in vacuum.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are used to drive the entire rotor blade, and the high pressure turbine is driven by the combined engine combustion section (31Y) high-temperature water (52b) in the turbine blade cross section (4D). Various energy conservation cycle coalescence engine that makes the output of the same heat speed 1700 times kg weight m / sec * 539 = about 910,000 times of steam drive and makes various heat, electricity and cold supply facilities with gravity acceleration in vacuum.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbine, and all blade combustion section (32X) of turbine blade cross section (4D) is driven to high pressure turbine by high temperature water (52b) and atmospheric pressure Various energy conservation cycle coalescence engine that makes the same speed and the same calorie output 1700 times kg weight m / sec * 539 = about 910,000 times the steam drive, etc. to supply various heat, electricity and cold supply equipment with gravity acceleration in vacuum .   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbine, and all blade combustion section (32Y) of turbine blade cross section (4D) is driven to high pressure turbine by high temperature water (52b) and atmospheric pressure Various energy conservation cycle coalescence engine that makes the same speed and the same calorie output 1700 times kg weight m / sec * 539 = about 910,000 times the steam drive, etc. to supply various heat, electricity and cold supply equipment with gravity acceleration in vacuum .   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbine, and all blade combustion section (32X) of turbine blade cross section (4D) is driven to high pressure turbine by high temperature water (52b) and atmospheric pressure Various energy storage cycle coalescing engines that make the same speed and calorie output 1700 times kg weight m / sec * 539 = about 910,000 times steam-driven various ships with gravity acceleration added in vacuum.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbine, and all blade combustion section (32Y) of turbine blade cross section (4D) is driven to high pressure turbine by high temperature water (52b) and atmospheric pressure Various energy storage cycle coalescing engines that make the same speed and calorie output 1700 times kg weight m / sec * 539 = about 910,000 times steam-driven various ships with gravity acceleration added in vacuum.   Provided bearing (80) thrust bearing (80a) for all applications to drive all rotor blade turbines, high pressure turbine driven by combined engine combustion section (31X) high temperature water (52b) of turbine blade cross section (4D) Various energy conservation cycle coalescing engines that make the speed and heat output 1700 times the weight of steam driven m / sec * 539 = about 910,000 times, etc. to make various ships with gravity acceleration added in vacuum.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are used to drive the entire rotor blade, and the high pressure turbine is driven by the combined engine combustion section (31Y) high-temperature water (52b) in the turbine blade cross section (4D). Various energy conservation cycle coalescing engines that make the speed and heat output 1700 times the weight of steam driven m / sec * 539 = about 910,000 times, etc. to make various ships with gravity acceleration added in vacuum.   Provided bearing (80) thrust bearing (80a) for all applications to drive all rotor blade turbines, high pressure turbine driven by combined engine combustion section (31X) high temperature water (52b) of turbine blade cross section (4D) Various energy storage cycle coalescing engines that make the speed and heat output 1700 times the weight of steam driven m / sec * 539 = about 910,000 times etc. to make various airplanes with gravity acceleration added in vacuum.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are used to drive the entire rotor blade, and the high pressure turbine is driven by the combined engine combustion section (31Y) high-temperature water (52b) in the turbine blade cross section (4D). Various energy storage cycle coalescing engines that make the speed and heat output 1700 times the weight of steam driven m / sec * 539 = about 910,000 times etc. to make various airplanes with gravity acceleration added in vacuum.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbine, and all blade combustion section (32X) of turbine blade cross section (4D) is driven to high pressure turbine by high temperature water (52b) and atmospheric pressure Various energy storage cycle coalescing engines that make the same speed and heat output 1700 times the weight of steam driven m / sec * 539 = about 910,000 times etc. to make various airplanes with gravity acceleration added in vacuum.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbine, and all blade combustion section (32Y) of turbine blade cross section (4D) is driven to high pressure turbine by high temperature water (52b) and atmospheric pressure Various energy storage cycle coalescing engines that make the same speed and heat output 1700 times the weight of steam driven m / sec * 539 = about 910,000 times etc. to make various airplanes with gravity acceleration added in vacuum.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all rotor blade turbines, and all blade combustion sections (32X) of turbine blade cross section (4D) are driven to high-pressure turbine by high-temperature mercury (1d) and atmospheric pressure Various energy storage cycle coalescing engines with the same speed and heat output of 23,000 times kg weight m / sec * 72 = approx.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbine, and all blade combustion section (32Y) of turbine blade cross section (4D) is driven to high-pressure turbine by high-temperature mercury (1d) and atmospheric pressure Various energy storage cycle coalescing engines with the same speed and heat output of 23,000 times kg weight m / sec * 72 = approx.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines. Combined engine combustion part (31X) of turbine blade cross section (4D) High-pressure turbine drive with high-temperature mercury (1d) Various energy storage cycle coalescing engines that make the speed and heat output 23,000 times kg weight m / sec * 72 = approx.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines. Combined engine combustion section (31Y) of turbine blade cross section (4D) High-pressure turbine drive with high-temperature mercury (1d) Various energy storage cycle coalescing engines that make the speed and heat output 23,000 times kg weight m / sec * 72 = approx.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines. Combined engine combustion part (31X) of turbine blade cross section (4D) High-pressure turbine drive with high-temperature mercury (1d) Various energy storage cycle coalescing engines that make the speed and heat output 23,000 times kg weight m / sec * 72 = approx.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines. Combined engine combustion section (31Y) of turbine blade cross section (4D) High-pressure turbine drive with high-temperature mercury (1d) Various energy storage cycle coalescing engines that make the speed and heat output 23,000 times kg weight m / sec * 72 = approx.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all rotor blade turbines, and all blade combustion sections (32X) of turbine blade cross section (4D) are driven to high-pressure turbine by high-temperature mercury (1d) and atmospheric pressure Various energy storage cycle coalescing engines with the same speed and heat output of 23,000 times kg weight m / sec * 72 = approx.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbine, and all blade combustion section (32Y) of turbine blade cross section (4D) is driven to high-pressure turbine by high-temperature mercury (1d) and atmospheric pressure Various energy storage cycle coalescing engines with the same speed and heat output of 23,000 times kg weight m / sec * 72 = approx.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all rotor blade turbines, and all blade combustion sections (32X) of turbine blade cross section (4D) are driven to high-pressure turbine by high-temperature mercury (1d) and atmospheric pressure The same speed and the same amount of heat output 23,000 times the weight of steam driven kg weight m / sec * 72 = about 166,000 times, etc. Energy conservation cycle coalescence engine.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbine, and all blade combustion section (32Y) of turbine blade cross section (4D) is driven to high-pressure turbine by high-temperature mercury (1d) and atmospheric pressure The same speed and the same amount of heat output 23,000 times the weight of steam driven kg weight m / sec * 72 = about 166,000 times, etc. Energy conservation cycle coalescence engine.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines. Combined engine combustion part (31X) of turbine blade cross section (4D) High-pressure turbine drive with high-temperature mercury (1d) Velocity and heat output is 23,000 times the weight of steam driven kg weight m / sec * 72 = approx. 166,000 times, etc. Conservation cycle coalescence organization.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines. Combined engine combustion section (31Y) of turbine blade cross section (4D) High-pressure turbine drive with high-temperature mercury (1d) Velocity and heat output is 23,000 times the weight of steam driven kg weight m / sec * 72 = approx. 166,000 times, etc. Conservation cycle coalescence organization.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all rotor blade turbines. Combined engine combustion section (31X) high-temperature mercury (1d) of turbine blade cross section (4D) is sprayed vertically downward in gravity vacuum Various energy conservation cycle coalescing engines that increase the output of high-pressure turbine drive at the same atmospheric pressure and speed and heat output by about 16656,000 times that of steam drive.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines, and the combined combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) is sprayed vertically downward in the vacuum Various energy conservation cycle coalescing engines that increase the output of high-pressure turbine drive at the same atmospheric pressure and speed and heat output by about 16656,000 times that of steam drive.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all blades, and all blade combustion section (32X) high-temperature mercury (1d) in turbine blade cross section (4D) is injected vertically downward in vacuum Various energy conservation cycle coalescence engines that increase the output of high-pressure turbine drive at the same atmospheric pressure and speed and heat output by approximately 166,000 times that of steam drive by adding acceleration of gravity.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all blades, and all blade combustion section (32Y) high-temperature mercury (1d) in turbine blade cross section (4D) is injected vertically downward in vacuum Various energy conservation cycle coalescence engines that increase the output of high-pressure turbine drive at the same atmospheric pressure and speed and heat output by approximately 166,000 times that of steam drive by adding acceleration of gravity.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all blades, and all blade combustion section (32X) high-temperature mercury (1d) in turbine blade cross section (4D) is injected vertically downward in vacuum High-speed turbine driven atmospheric pressure, same speed, and same calorie output with acceleration added by gravitational acceleration. Combined with various energy conservation cycle coalescence engines that provide various heat, electricity, and cold supply facilities such as about 166,000 times that of steam drive.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all blades, and all blade combustion section (32Y) high-temperature mercury (1d) in turbine blade cross section (4D) is injected vertically downward in vacuum High-speed turbine driven atmospheric pressure, same speed, and same calorie output with acceleration added by gravitational acceleration. Combined with various energy conservation cycle coalescence engines that provide various heat, electricity, and cold supply facilities such as about 166,000 times that of steam drive.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all rotor blade turbines. Combined engine combustion section (31X) high-temperature mercury (1d) of turbine blade cross section (4D) is sprayed vertically downward in gravity vacuum High-speed turbine-driven atmospheric pressure, same-speed, and same-heat output is accelerated by adding acceleration to approximately 16,656,000 times that of steam-driven, and various energy storage cycle coalescing engines.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines, and the combined combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) is sprayed vertically downward in the vacuum High-speed turbine-driven atmospheric pressure, same-speed, and same-heat output is accelerated by adding acceleration to approximately 16,656,000 times that of steam-driven, and various energy storage cycle coalescing engines.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all rotor blade turbines. Combined engine combustion section (31X) high-temperature mercury (1d) of turbine blade cross section (4D) is sprayed vertically downward in gravity vacuum Various energy storage cycle coalescing engines that make high-speed turbine drive atmospheric pressure same speed same heat quantity output about 16656,000 times that of steam drive by acceleration with added acceleration.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines, and the combined combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) is sprayed vertically downward in the vacuum Various energy storage cycle coalescing engines that make high-speed turbine drive atmospheric pressure same speed same heat quantity output about 16656,000 times that of steam drive by acceleration with added acceleration.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all blades, and all blade combustion section (32X) high-temperature mercury (1d) in turbine blade cross section (4D) is injected vertically downward in vacuum Various energy conservation cycle coalescing engines that make high-pressure turbine-driven atmospheric pressure, same-velocity, and same-heat output about 16656,000 times that of steam-driven, with the addition of gravitational acceleration.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all blades, and all blade combustion section (32Y) high-temperature mercury (1d) in turbine blade cross section (4D) is injected vertically downward in vacuum Various energy conservation cycle coalescing engines that make high-pressure turbine-driven atmospheric pressure, same-velocity, and same-heat output about 16656,000 times that of steam-driven, with the addition of gravitational acceleration.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all blades, and all blade combustion section (32X) high-temperature mercury (1d) in turbine blade cross section (4D) is injected vertically downward in vacuum Various energy storage cycle coalescing engines that make high-speed turbine driven atmospheric pressure, same speed, and same calorific power output about 1656,000 times that of steam driven by acceleration with gravity acceleration added.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all blades, and all blade combustion section (32Y) high-temperature mercury (1d) in turbine blade cross section (4D) is injected vertically downward in vacuum Various energy storage cycle coalescing engines that make high-speed turbine driven atmospheric pressure, same speed, and same calorific power output about 1656,000 times that of steam driven by acceleration with gravity acceleration added.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all rotor blade turbines. Combined engine combustion section (31X) high-temperature mercury (1d) of turbine blade cross section (4D) is sprayed vertically downward in gravity vacuum Various energy conservation cycle coalescing engines that make high-speed turbine driven atmospheric pressure, same speed, and same calorific power output about 16656,000 times that of steam driven by acceleration with added acceleration.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines, and the combined combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) is sprayed vertically downward in the vacuum Various energy conservation cycle coalescing engines that make high-speed turbine driven atmospheric pressure, same speed, and same calorific power output about 16656,000 times that of steam driven by acceleration with added acceleration.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blades, and the combined engine combustion section (31X) high-temperature water (52b) on the turbine blade cross section (4D) is gravity vertically in the jet vacuum. Various energy conservation cycle coalescing engines that make high-speed turbine-driven atmospheric pressure, same-speed, and same-heat output approximately 910,000 times that of steam-driven aircraft by adding acceleration.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blades, and the combined engine combustion section (31Y) high-temperature water (52b) on the turbine blade cross section (4D) is vertically gravity sprayed in the vacuum. Various energy conservation cycle coalescing engines that make high-speed turbine-driven atmospheric pressure, same-speed, and same-heat output approximately 910,000 times that of steam-driven aircraft by adding acceleration.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all blades, and all blade combustion parts (32X) high-temperature water (52b) in the turbine blade cross section (4D) are injected vertically downward in a vacuum. Various energy conservation cycle coalescing engines that make high-speed turbine-driven atmospheric pressure, same-speed, and same-heat output about 910,000 times that of steam-driven airplanes with acceleration by adding gravitational acceleration.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all blades, and all blade combustion section (32Y) high-temperature water (52b) in turbine blade cross section (4D) is injected vertically downward in a vacuum. Various energy conservation cycle coalescing engines that make high-speed turbine-driven atmospheric pressure, same-speed, and same-heat output about 910,000 times that of steam-driven airplanes with acceleration by adding gravitational acceleration.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all blades, and all blade combustion parts (32X) high-temperature water (52b) in the turbine blade cross section (4D) are injected vertically downward in a vacuum. Various energy conservation cycle coalescing engines that make high-pressure turbine-driven atmospheric pressure, same-velocity, and same-heat power output about 910,000 times that of steam-driven vessels, with the addition of gravitational acceleration.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all blades, and all blade combustion section (32Y) high-temperature water (52b) in turbine blade cross section (4D) is injected vertically downward in a vacuum. Various energy conservation cycle coalescing engines that make high-pressure turbine-driven atmospheric pressure, same-velocity, and same-heat power output about 910,000 times that of steam-driven vessels, with the addition of gravitational acceleration.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blades, and the combined engine combustion section (31X) high-temperature water (52b) on the turbine blade cross section (4D) is gravity vertically in the jet vacuum. Various energy storage cycle coalescing engines that make high-speed turbine driven atmospheric pressure same speed and same calorie power output about 910,000 times that of water vapor drive by adding acceleration.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blades, and the combined engine combustion section (31Y) high-temperature water (52b) on the turbine blade cross section (4D) is vertically gravity sprayed in the vacuum. High-speed turbine-driven atmospheric pressure, same-speed, and same-heat output is about 910,000 times that of steam-driven, and various energy storage cycle coalescing engines.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blades, and the combined engine combustion section (31X) high-temperature water (52b) on the turbine blade cross section (4D) is gravity vertically in the jet vacuum. High-speed turbine-driven atmospheric pressure, same-speed, and same-heat output is about 910,000 times that of steam-driven, with acceleration added, and various energy storage cycle coalescing engines that supply various types of heat, electricity, and cold.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blades, and the combined engine combustion section (31Y) high-temperature water (52b) on the turbine blade cross section (4D) is vertically gravity sprayed in the vacuum. High-speed turbine-driven atmospheric pressure, same-speed, and same-heat output is about 910,000 times that of steam-driven, with acceleration added, and various energy storage cycle coalescing engines that supply various types of heat, electricity, and cold.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all blades, and all blade combustion parts (32X) high-temperature water (52b) in the turbine blade cross section (4D) are injected vertically downward in a vacuum. High-speed turbine-driven atmospheric pressure, same-speed, and same-heat output is about 910,000 times that of steam-driven, with the addition of gravitational acceleration.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all blades, and all blade combustion section (32Y) high-temperature water (52b) in turbine blade cross section (4D) is injected vertically downward in a vacuum. High-speed turbine-driven atmospheric pressure, same-speed, and same-heat output is about 910,000 times that of steam-driven, with the addition of gravitational acceleration.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all blades, and all blade combustion parts (32X) high-temperature water (52b) in the turbine blade cross section (4D) are injected vertically downward in a vacuum. High-speed turbine-driven atmospheric pressure, same-speed, and same-heat output is about 910,000 times that of steam-driven by acceleration with added gravitational acceleration.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all blades, and all blade combustion section (32Y) high-temperature water (52b) in turbine blade cross section (4D) is injected vertically downward in a vacuum. High-speed turbine-driven atmospheric pressure, same-speed, and same-heat output is about 910,000 times that of steam-driven by acceleration with added gravitational acceleration.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blades, and the combined engine combustion section (31X) high-temperature water (52b) on the turbine blade cross section (4D) is gravity vertically in the jet vacuum. Various energy conservation cycle coalescing engines that increase the output of high pressure turbine drive at the same atmospheric pressure and speed and heat output by about 910,000 times that of steam driven by acceleration with added acceleration.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blades, and the combined engine combustion section (31Y) high-temperature water (52b) on the turbine blade cross section (4D) is vertically gravity sprayed in the vacuum. Various energy conservation cycle coalescing engines that increase the output of high pressure turbine drive at the same atmospheric pressure and speed and heat output by about 910,000 times that of steam driven by acceleration with added acceleration.   A bearing for the application (80) Thrust bearing (80a) is provided to drive the entire rotor blade turbine, and the intake air is heated by the combined engine combustion part (31X) high-temperature mercury (1d) exhaust heat quantity of the turbine blade cross section (4D) Compression heat recovery theory The best heat pump (1G) and various energy storage cycle coalescing engines that make the atmospheric pressure, the same speed, and the same calorie output about 166,000 times the steam drive.   A bearing for the application (80) Thrust bearing (80a) is provided to drive the entire rotor blade turbine, and the intake air is heated by the combined engine combustion section (31Y) high-temperature mercury (1d) exhaust heat quantity of the turbine blade cross section (4D) Compression heat recovery theory The best heat pump (1G) and various energy storage cycle coalescing engines that make the atmospheric pressure, the same speed, and the same calorie output about 166,000 times the steam drive.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all rotor blade turbines, and the intake air is heated by the entire blade combustion section (32X) high-temperature mercury (1d) exhaust heat quantity of the turbine blade cross section (4D). Compression heat recovery theory The best heat pump (1G) and various energy storage cycle coalescing engines that make the atmospheric pressure, the same speed, and the same calorie output approximately 16565 times the steam drive.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all blades, and the intake air is heated by the entire blade combustion section (32Y) high-temperature mercury (1d) exhaust heat of the turbine blade cross section (4D). Compression heat recovery theory The best heat pump (1G) and various energy storage cycle coalescing engines that make the atmospheric pressure, the same speed, and the same calorie output approximately 16565 times the steam drive.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all blades, and all blade combustion parts (32X) high-temperature mercury (1d) in the turbine blade cross section (4D) high-temperature mercury (1d) near 230 degrees of intake air Compressed heat recovery theory best heat pump (1G) and various energy storage cycle coalescing engines that make the atmospheric pressure, the same speed, and the same calorie output about 166,000 times the steam drive.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all blades, and all blade combustion parts (32Y) high-temperature mercury (1d) in the turbine blade cross section (4D) high-temperature mercury (1d) near 230 degrees of intake air Compressed heat recovery theory best heat pump (1G) and various energy storage cycle coalescing engines that make the atmospheric pressure, the same speed, and the same calorie output about 166,000 times the steam drive.   The bearing (80) thrust bearing (80a) for the application is provided to drive the entire rotor blade turbine, and the combined engine combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D) is heated by the exhaust heat amount near 230 degrees. A combined heat storage cycle engine that heats and produces the best heat pump (1G) for compressive heat recovery and the atmospheric pressure, the same speed, and the same calorie output, approximately 166,000 times the steam drive.   A bearing (80) thrust bearing (80a) corresponding to the application is provided to drive the entire rotor blade turbine, and the combined engine combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) is heated by the exhaust heat amount near 230 degrees. A combined heat storage cycle engine that heats and produces the best heat pump (1G) for compressive heat recovery and the atmospheric pressure, the same speed, and the same calorie output, approximately 166,000 times the steam drive.   The bearing (80) thrust bearing (80a) for the application is provided to drive the entire rotor blade turbine, and the combined engine combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D) is heated by the exhaust heat amount near 230 degrees. Combined engine with various energy storage cycles that heat and compress heat recovery theory to achieve the best heat pump (1G) and atmospheric pressure, same speed, and same calorie output, approximately 166,000 times that of steam drive, etc. .   A bearing (80) thrust bearing (80a) corresponding to the application is provided to drive the entire rotor blade turbine, and the combined engine combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) is heated by the exhaust heat amount near 230 degrees. Combined engine with various energy storage cycles that heat and compress heat recovery theory to achieve the best heat pump (1G) and atmospheric pressure, same speed, and same calorie output, approximately 166,000 times that of steam drive, etc. .   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all blades, and all blade combustion parts (32X) high-temperature mercury (1d) in the turbine blade cross section (4D) high-temperature mercury (1d) near 230 degrees of intake air Compressed heat recovery theory Best heat pump (1G) and atmospheric pressure, same speed and same calorie output to make various heat, electricity and cold supply facilities such as steam drive, etc. organ.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all blades, and all blade combustion parts (32Y) high-temperature mercury (1d) in the turbine blade cross section (4D) high-temperature mercury (1d) near 230 degrees of intake air Compressed heat recovery theory Best heat pump (1G) and atmospheric pressure, same speed and same calorie output to make various heat, electricity and cold supply facilities such as steam drive, etc. organ.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all blades, and all blade combustion parts (32X) high-temperature mercury (1d) in the turbine blade cross section (4D) high-temperature mercury (1d) near 230 degrees of intake air Compressed heat recovery theory best heat pump (1G) and various energy storage cycle coalescing engines that make the atmospheric pressure, the same speed, and the same calorie output about 16656,000 times that of steam drive.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all blades, and all blade combustion parts (32Y) high-temperature mercury (1d) in the turbine blade cross section (4D) high-temperature mercury (1d) near 230 degrees of intake air Compressed heat recovery theory best heat pump (1G) and various energy storage cycle coalescing engines that make the atmospheric pressure, the same speed, and the same calorie output about 16656,000 times that of steam drive.   The bearing (80) thrust bearing (80a) for the application is provided to drive the entire rotor blade turbine, and the combined engine combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D) is heated by the exhaust heat amount near 230 degrees. Combined engine with various energy storage cycles to heat and make the best heat pump (1G) of compression heat recovery and atmospheric pressure, same speed and same calorie output to about 166,000 times more than steam drive.   A bearing (80) thrust bearing (80a) corresponding to the application is provided to drive the entire rotor blade turbine, and the combined engine combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) is heated by the exhaust heat amount near 230 degrees. Combined engine with various energy storage cycles to heat and make the best heat pump (1G) of compression heat recovery and atmospheric pressure, same speed and same calorie output to about 166,000 times more than steam drive.   The bearing (80) thrust bearing (80a) for the application is provided to drive the entire rotor blade turbine, and the combined engine combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D) is heated by the exhaust heat amount near 230 degrees. Various energy storage cycle coalescing engines that heat and produce a variety of airplanes such as the best heat pump (1G) for compression heat recovery and atmospheric pressure, the same speed and the same calorie output, approximately 166,000 times the steam drive.   A bearing (80) thrust bearing (80a) corresponding to the application is provided to drive the entire rotor blade turbine, and the combined engine combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) is heated by the exhaust heat amount near 230 degrees. Various energy storage cycle coalescing engines that heat and produce a variety of airplanes such as the best heat pump (1G) for compression heat recovery and atmospheric pressure, the same speed and the same calorie output, approximately 166,000 times the steam drive.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all blades, and all blade combustion parts (32X) high-temperature mercury (1d) in the turbine blade cross section (4D) high-temperature mercury (1d) near 230 degrees of intake air Compressed heat recovery theory best heat pump (1G) and various energy storage cycle coalescing engine that makes atmospheric pressure, same speed and same calorie output about 16656,000 times that of steam drive.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all blades, and all blade combustion parts (32Y) high-temperature mercury (1d) in the turbine blade cross section (4D) high-temperature mercury (1d) near 230 degrees of intake air Compressed heat recovery theory best heat pump (1G) and various energy storage cycle coalescing engine that makes atmospheric pressure, same speed and same calorie output about 16656,000 times that of steam drive.   A bearing for the application (80) Thrust bearing (80a) is provided to drive the entire rotor blade turbine, and the intake air is heated by the combined engine combustion part (31X) high-temperature mercury (1d) exhaust heat quantity of the turbine blade cross section (4D) Compressed heat recovery theory Best heat pump (1G) and various energy storage cycle coalescing engines that use various heat, electricity, and cold supply facilities such as the atmospheric pressure, the same speed, and the same calorie output, approximately 166,000 times the steam drive.   A bearing for the application (80) Thrust bearing (80a) is provided to drive the entire rotor blade turbine, and the intake air is heated by the combined engine combustion section (31Y) high-temperature mercury (1d) exhaust heat quantity of the turbine blade cross section (4D) Compressed heat recovery theory Best heat pump (1G) and various energy storage cycle coalescing engines that use various heat, electricity, and cold supply facilities such as the atmospheric pressure, the same speed, and the same calorie output, approximately 166,000 times the steam drive.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all rotor blade turbines, and the intake air is heated by the entire blade combustion section (32X) high-temperature mercury (1d) exhaust heat quantity of the turbine blade cross section (4D). Compression heat recovery theory The best heat pump (1G) and various energy storage cycle coalescing engines that use various heat, electricity, and cold supply facilities such as the atmospheric pressure, the same speed, and the same amount of heat output, approximately 166,000 times the steam drive.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all blades, and the intake air is heated by the entire blade combustion section (32Y) high-temperature mercury (1d) exhaust heat of the turbine blade cross section (4D). Compression heat recovery theory The best heat pump (1G) and various energy storage cycle coalescing engines that use various heat, electricity, and cold supply facilities such as the atmospheric pressure, the same speed, and the same amount of heat output, approximately 166,000 times the steam drive.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all rotor blade turbines, and the intake air is heated by the entire blade combustion section (32X) high-temperature mercury (1d) exhaust heat quantity of the turbine blade cross section (4D). Compressed heat recovery theory The best heat pump (1G) and various energy storage cycle coalescing engines that make the atmospheric pressure, the same speed, and the same calorific power output about 16656,000 times the steam drive.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all blades, and the intake air is heated by the entire blade combustion section (32Y) high-temperature mercury (1d) exhaust heat of the turbine blade cross section (4D). Compressed heat recovery theory The best heat pump (1G) and various energy storage cycle coalescing engines that make the atmospheric pressure, the same speed, and the same calorific power output about 16656,000 times the steam drive.   A bearing for the application (80) Thrust bearing (80a) is provided to drive the entire rotor blade turbine, and the intake air is heated by the combined engine combustion part (31X) high-temperature mercury (1d) exhaust heat quantity of the turbine blade cross section (4D) Compression heat recovery theory The best heat pump (1G) and various energy storage cycle coalescing engines that make the atmospheric pressure, the same speed, and the same calorie output about 16656,000 times the steam drive.   A bearing for the application (80) Thrust bearing (80a) is provided to drive the entire rotor blade turbine, and the intake air is heated by the combined engine combustion section (31Y) high-temperature mercury (1d) exhaust heat quantity of the turbine blade cross section (4D) Compression heat recovery theory The best heat pump (1G) and various energy storage cycle coalescing engines that make the atmospheric pressure, the same speed, and the same calorie output about 16656,000 times the steam drive.   A bearing for the application (80) Thrust bearing (80a) is provided to drive the entire rotor blade turbine, and the intake air is heated by the combined engine combustion part (31X) high-temperature mercury (1d) exhaust heat quantity of the turbine blade cross section (4D) Compressed heat recovery theory The best heat pump (1G) and various energy storage cycle coalescing engines that make the atmospheric pressure, the same speed and the same calorie output about 166,000 times the steam drive, etc.   A bearing for the application (80) Thrust bearing (80a) is provided to drive the entire rotor blade turbine, and the intake air is heated by the combined engine combustion section (31Y) high-temperature mercury (1d) exhaust heat quantity of the turbine blade cross section (4D) Compressed heat recovery theory The best heat pump (1G) and various energy storage cycle coalescing engines that make the atmospheric pressure, the same speed and the same calorie output about 166,000 times the steam drive, etc.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all rotor blade turbines, and the intake air is heated by the entire blade combustion section (32X) high-temperature mercury (1d) exhaust heat quantity of the turbine blade cross section (4D). Compressed heat recovery theory The best heat pump (1G) and various energy storage cycle coalescing engines that make the atmospheric pressure, the same speed, and the same calorific power output about 16,656,000 times that of steam drive.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all blades, and the intake air is heated by the entire blade combustion section (32Y) high-temperature mercury (1d) exhaust heat of the turbine blade cross section (4D). Compressed heat recovery theory The best heat pump (1G) and various energy storage cycle coalescing engines that make the atmospheric pressure, the same speed, and the same calorific power output about 16,656,000 times that of steam drive.   A bearing (80) thrust bearing (80a) corresponding to the application is provided to drive the entire rotor blade turbine, and a cold heat recovery means (3C) is provided to the turbine blade (8c) of the entire rotor blade gas turbine of the turbine blade cross section (4D). Various energy conservation cycle coalescing engines that recover cold energy and output the same amount of heat at the same pressure and atmospheric pressure about 166,000 times that of steam drive.   A bearing (80) thrust bearing (80a) corresponding to the application is provided to drive the entire rotor blade turbine, and a cold heat recovery means (3C) is provided to the turbine blade (8c) of the entire rotor blade gas turbine of the turbine blade cross section (4D). Various energy storage cycle coalescing engines that make heating and atmospheric pressure, same speed, and same calorie output 166.5 times the steam drive.   A bearing (80) thrust bearing (80a) corresponding to the application is provided to drive the entire rotor blade turbine, and a cold heat recovery means (3C) is provided to the turbine blade (8c) of the entire rotor blade gas turbine of the turbine blade cross section (4D). Various energy conservation cycle coalescing engines that collect cold energy with alcohol (1C), etc., and make the atmospheric pressure, the same speed, and the same amount of heat output about 166,000 times that of steam drive.   A bearing (80) thrust bearing (80a) corresponding to the application is provided to drive the entire rotor blade turbine, and a cold heat recovery means (3C) is provided to the turbine blade (8c) of the entire rotor blade gas turbine of the turbine blade cross section (4D). Various energy storage cycle coalescing engines that use alcohol (1C) etc. to make heating and atmospheric pressure at the same speed and heat output about 166,000 times that of steam drive.   A bearing (80) thrust bearing (80a) corresponding to the application is provided to drive the entire rotor blade turbine, and a cold heat recovery means (3C) is provided to the turbine blade (8c) of the entire rotor blade gas turbine of the turbine blade cross section (4D). Various energy storage cycle coalescing engines that increase the recovery output of cold heat with alcohol (1C) and the like, and increase the atmospheric pressure, the same speed, and the same calorie output to about 166,000 times the steam drive.   A bearing (80) thrust bearing (80a) corresponding to the application is provided to drive the entire rotor blade turbine, and a cold heat recovery means (3C) is provided to the turbine blade (8c) of the entire rotor blade gas turbine of the turbine blade cross section (4D). Various energy storage cycle coalescing engines that increase the heating output with alcohol (1C) and the like, and make the atmospheric pressure, the same speed, and the same amount of heat output about 166,000 times that of steam drive.   A bearing (80) thrust bearing (80a) corresponding to the application is provided to drive the entire rotor blade turbine, and a cold heat recovery means (3C) is provided to the turbine blade (8c) of the entire rotor blade gas turbine of the turbine blade cross section (4D). Collecting cold energy with alcohol (1C), etc. Various energy storage cycle coalescing engines that prevent sticking of dry ice, moisture, etc., and make the atmospheric pressure, the same speed, and the same calorie output about 166,000 times that of steam drive.   A bearing (80) thrust bearing (80a) corresponding to the application is provided to drive the entire rotor blade turbine, and a cold heat recovery means (3C) is provided to the turbine blade (8c) of the entire rotor blade gas turbine of the turbine blade cross section (4D). Various energy storage cycle coalescence engines that prevent the adhesion of heated dry ice, moisture, etc. with alcohol (1C), etc., and make the atmospheric pressure, the same speed, and the same calorie output about 166,000 times that of water vapor drive.   A bearing (80) thrust bearing (80a) corresponding to the application is provided to drive the entire rotor blade turbine, and a heating high temperature means (3B) is provided to the turbine blade (8c) of the entire rotor blade water turbine of the turbine blade cross section (4D). Various energy storage cycle coalescing engines that make heating and atmospheric pressure, same speed, and same calorie output 166.5 times the steam drive.   A bearing (80) thrust bearing (80a) corresponding to the application is provided to drive the entire rotor blade turbine, and a water repellency action (3A) is provided to the turbine blade (8c) of the entire rotor blade water turbine of the turbine blade section (4D). Various energy storage cycle coalescing engines that make water repellent and atmospheric pressure and speed and heat output approximately 166,000 times that of water vapor drive.   A bearing (80) thrust bearing (80a) corresponding to the application is provided to drive the entire rotor blade turbine, and a heating high temperature means (3B) is provided to the turbine blade (8c) of the entire rotor blade water turbine of the turbine blade cross section (4D). Various energy storage cycle coalescing engines that make rolling contact rotation output and atmospheric pressure same speed and same calorie output about 16656,000 times of steam driven by heating vaporization film.   A bearing (80) thrust bearing (80a) corresponding to the application is provided to drive the entire rotor blade turbine, and a water repellency action (3A) is provided to the turbine blade (8c) of the entire rotor blade water turbine of the turbine blade section (4D). Various energy storage cycle coalescing engines that make rolling contact rotation output and atmospheric pressure, same speed, and same calorie output by water repellent effect about 166,000 times the steam drive.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all rotor blade turbines. Cooling (52e) cooling and atmospheric pressure around the exhaust saturation temperature of all rotor blade water turbines in the turbine blade cross section (4D) Various energy storage cycle coalescing engines with the same speed and heat output of about 166,000 times the steam drive.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all rotor blade turbines, and the seawater temperature is determined by cooling (52e) cooling around 30 degrees of exhaust saturation temperature of all rotor blade water turbines in the turbine blade cross section (4D) Various energy conservation cycle coalescing engines that prevent the rise and output the atmospheric pressure, the same speed, and the same amount of heat about 166,000 times the steam drive.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all rotor blade turbines, and alcohol cold heat (52e) is recovered and stored in an all-blade gas turbine with a turbine blade cross section (4D) at the same atmospheric pressure as used. Various energy storage cycle coalescing engines that make the output of the same amount of heat about 166,000 times the steam drive.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines, and compressed air cold heat (52e) is recovered and stored in a turbine blade cross section (4D) full blade gas turbine for use and atmospheric pressure Various energy storage cycle coalescing engines that make the output of the same speed and the same amount of heat about 166,000 times the steam drive.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all blades, and ice-cooled heat (52e) is recovered and stored in a turbine blade cross-section (4D) full blade gas turbine. Various energy storage cycle coalescing engines that make the output of the same amount of heat about 166,000 times the steam drive.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all rotor blade turbines, and cold heat (52e) is recovered and stored in all rotor blade gas turbines with a turbine blade cross section (4D) as various refrigeration equipment. Various energy storage cycle coalescing engines that use and output at the same pressure and heat at atmospheric pressure approximately 166,000 times the steam drive.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all rotor blade turbines, and cold heat (52e) is recovered and stored in all rotor blade gas turbines with a turbine blade cross section (4D) as various refrigeration equipment. Various energy storage cycle coalescing engines that use and output at the same pressure and heat at atmospheric pressure approximately 166,000 times the steam drive.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all rotor blade turbines, and cold heat (52e) is recovered and stored in all rotor blade gas turbines with a turbine blade cross section (4D) as various cooling equipment. Various energy storage cycle coalescing engines that use and output at the same pressure and heat at atmospheric pressure approximately 166,000 times the steam drive.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive all blades, and cold heat (52e) is recovered and stored in all blades gas turbine with turbine blade cross section (4D) as various cooling equipment Various energy storage cycle coalescing engines that use and output at the same pressure and heat at atmospheric pressure approximately 166,000 times the steam drive.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all blades, and cold heat (52e) is collected and stored in all blades turbines with a turbine blade cross section (4D) as various ice making equipment. Various energy storage cycle coalescing engines that use and output at the same pressure and heat at atmospheric pressure approximately 166,000 times the steam drive.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all rotor blade turbines, and cold air (52e) is recovered and stored in all blade gas turbines with a turbine blade cross section (4D). Various energy storage cycle coalescing engines that can be used as a class and have the same atmospheric pressure, same speed, and same calorie output, approximately 166,000 times the steam drive.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all rotor blade turbines, and all rotor blade gas turbine exhaust with a turbine blade cross-section (4D) is supplied to the seabed as combustion gas dissolved water (52 g) such as CO2. Combined with various energy storage cycle engines that make the output of the same pressure and heat at atmospheric pressure about 166,000 times the steam drive.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all rotor blade turbines, and all rotor blade gas turbine exhaust with a turbine blade cross-section (4D) is supplied to the seabed as combustion gas dissolved water (52 g) such as CO2. A variety of energy conservation cycle coalescing engines that increase seaweeds and output atmospheric pressure at the same speed and heat output by approximately 166,000 times that of steam drive.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all rotor blade turbines, and all rotor blade gas turbine exhaust with a turbine blade cross-section (4D) is supplied to the seabed as combustion gas dissolved water (52 g) such as CO2. Various energy conservation cycle coalescence engines that increase algae growth and atmospheric pressure at the same speed and heat output approximately 166,000 times that of steam drive.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all rotor blade turbines, and all rotor blade gas turbine exhaust with a turbine blade cross-section (4D) is supplied to the seabed as combustion gas dissolved water (52 g) such as CO2. Various energy conservation cycle coalescence engines that increase phytoplankton and increase the atmospheric pressure, the same speed, and the same calorie output to about 166,000 times that of water vapor drive.   A bearing (80) thrust bearing (80a) for the application is provided to drive the entire rotor blade turbine, and for the rotational output of the turbine blade cross section (4E), the excess heat is recovered and stored at various temperatures (52d) of 300 degrees or less. Various energy storage cycle coalescing engines that use and output at the same pressure and heat at atmospheric pressure approximately 166,000 times the steam drive.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all rotor blade turbines, and dedicated to the rotational output of the turbine blade cross section (4E), the excess heat can be recovered and stored at various temperatures (52d) of 300 degrees or less. Various energy storage cycle coalescing engines that are used as various types of heating equipment by setting the same pressure and heat output at atmospheric pressure to approximately 166,000 times the steam drive.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all rotor blade turbines, and dedicated to the rotational output of the turbine blade cross section (4E), the excess heat can be recovered and stored at various temperatures (52d) of 300 degrees or less. Various energy storage cycle coalescing engines that are used as various types of cooking equipment with the same pressure and heat output at atmospheric pressure, approximately 166,000 times the steam drive.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all rotor blade turbines, and dedicated to the rotational output of the turbine blade cross section (4E), the excess heat can be recovered and stored at various temperatures (52d) of 300 degrees or less. Various energy storage cycle coalescing engines that are used as various types of hot water equipment by setting the same pressure and heat output at atmospheric pressure to about 166,000 times the steam drive.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all rotor blade turbines, and dedicated to the rotational output of the turbine blade cross section (4E), the excess heat can be recovered and stored at various temperatures (52d) of 300 degrees or less. Various energy storage cycle coalescing engines that are used as various dishwashers, with the same pressure and heat output at atmospheric pressure about 166,000 times the steam drive.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all rotor blade turbines, and dedicated to the rotational output of the turbine blade cross section (4E), the excess heat can be recovered and stored at various temperatures (52d) of 300 degrees or less. Various energy storage cycle coalescing engines that are used as various types of washing and drying machines with the same pressure and heat output at the atmospheric pressure, approximately 166,000 times the steam drive.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all rotor blade turbines, and dedicated to the rotational output of the turbine blade cross section (4E), the excess heat can be recovered and stored at various temperatures (52d) of 300 degrees or less. Various energy storage cycle coalescing engines that can be used as various water temperature and heat piping buildings with the same pressure and heat output at atmospheric pressure about 166,000 times the steam drive.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all rotor blade turbines, and dedicated to the rotational output of the turbine blade cross section (4E), the excess heat can be recovered and stored at various temperatures (52d) of 300 degrees or less. Various energy storage cycle coalescing engines using various water such as seawater as distilled water with the same pressure and heat output at atmospheric pressure about 166,000 times that of steam drive.   Application-specific bearings (80) Thrust bearings (80a) are provided to drive all rotor blade turbines, and dedicated to the rotational output of the turbine blade cross section (4E), the excess heat can be recovered and stored at various temperatures (52d) of 300 degrees or less. Various energy storage cycle coalescing engines that use various water such as seawater as distilled water or salt with the same pressure and speed and heat output of approximately 166,000 times the steam drive.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive the turbine blade cross section (4D) for full rotor blade turbine, and the amount of compressed air (28b) is recovered by intake air (28a) to obtain a heat pump (1G) Various energy storage cycle coalescing engines that make compression heat recovery and atmospheric pressure, same speed, and same calorie output approximately 166,000 times that of steam drive.   Application-specific bearing (80) Thrust bearing (80a) is provided for turbine blade cross section (4D) full rotor blade drive and mercury exhaust heat (5A) + compressed air heat (28b) is recovered by intake air (28a) Various energy storage cycle coalescing engines, which use a heat pump (1G) to recover the heat of compression and output the same pressure and heat at atmospheric pressure approximately 166,000 times the steam drive.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive the turbine blade cross section (4D) for full rotor blade turbine, and the amount of compressed air (28b) is recovered by intake air (28a) to obtain a heat pump (1G) Various energy storage cycle coalescing engines that make the heat recovery and the atmospheric pressure, the same speed, and the same calorific power output approximately 16656,000 times that of the steam drive, etc. by compressing 500-1000 degrees.   Application-specific bearing (80) Thrust bearing (80a) is provided for turbine blade cross section (4D) full rotor blade drive and mercury exhaust heat (5A) + compressed air heat (28b) is recovered by intake air (28a) Then, various energy storage cycle coalescence engines that make the heat recovery and the atmospheric pressure, the same speed, and the same calorie output by about 16.56,000 times of the steam drive, etc. by compression with a heat pump (1G) 500-1000 degrees.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive the turbine blade cross section (4D) for full rotor blade turbine, and the amount of compressed air (28b) is recovered by intake air (28a) to obtain a heat pump (1G) Various energy storage cycle coalescing engines that recover heat at a compression of 500 to 1000 degrees, etc., and drive all rotor blade water turbines and output atmospheric pressure at the same speed and the same amount of heat about 166,000 times that of steam drive.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive the turbine blade cross section (4D) for full rotor blade turbine, and the amount of compressed air (28b) is recovered by intake air (28a) to obtain a heat pump (1G) Various energy storage cycle coalescing engines that recover heat at a compression of 500 to 1000 degrees, etc., and drive the whole moving blade mercury turbine to produce the same atmospheric pressure at the same speed and the same calorific power output as approximately 166,000 times that of the steam drive.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive the turbine blade cross section (4D) for full rotor blade turbine, and the amount of compressed air (28b) is recovered by intake air (28a) to obtain a heat pump (1G) Various energy storage cycle coalescing engines that recover heat at a compression of 500 to 1000 degrees, etc., and drive all rotor blade gas turbines to produce the same atmospheric pressure, same speed, and same calorie output, approximately 166,000 times that of steam drive.   Application-specific bearing (80) Thrust bearing (80a) is provided to make the turbine blade cross section (4D) full-blade turbine drive, and it becomes high temperature when returning to the earth at the flight speed such as flight blade (38b) and flight tail (38c). A water (52a) pipe that has been reduced in weight to high pressure with carbon fiber, etc., is piped on all parts, and a high-pressure lightweight container is constructed. Heat recovery and atmospheric pressure, the same speed, and the same amount of heat output are approximately 166,000 times that of water vapor drive. Various energy conservation cycle coalescing engines.   Application-specific bearing (80) Thrust bearing (80a) is provided to make the turbine blade cross section (4D) full-blade turbine drive, and it becomes high temperature when returning to the earth at the flight speed such as flight blade (38b) and flight tail (38c). A superheated steam (50) pipe that has been reduced in weight to high pressure with carbon fiber or the like is connected to all parts, and a high-pressure lightweight container is constructed. Heat recovery and atmospheric pressure, the same speed, and the same amount of heat output are about 1,656,000 driven by steam. Various energy conservation cycle coalescing engine to double.   Application-specific bearing (80) Thrust bearing (80a) is provided to make the turbine blade cross section (4D) full-blade turbine drive, and it becomes high temperature when returning to the earth at the flight speed such as flight blade (38b) and flight tail (38c). High-temperature mercury (1d) pipes, which are made lighter to higher in pressure with carbon fiber, etc., are piped on all parts to construct a high-pressure lightweight container. Various energy conservation cycle coalescing engine to double.   Application-specific bearing (80) Thrust bearing (80a) is provided to make the turbine blade cross section (4D) full-blade turbine drive, and it becomes high temperature when returning to the earth at the flight speed such as flight blade (38b) and flight tail (38c). All parts are made of light and high-pressure combustion gas pipes made of carbon fiber, etc., and a high-pressure lightweight container is constructed. Heat recovery and atmospheric pressure, the same speed, and the same amount of heat output are about 166,000 times that of steam drive. Various energy conservation cycle coalescing engines.   Application-specific bearing (80) Thrust bearing (80a) is provided to make the turbine blade cross section (4D) full-blade turbine drive, and it becomes high temperature when returning to the earth at the flight speed such as flight blade (38b) and flight tail (38c). A water (52a) pipe that has been reduced in weight to high pressure with carbon nanotubes, etc. is piped in all parts, and a high-pressure lightweight container is constructed. Heat recovery and atmospheric pressure, the same speed, and the same amount of heat output are approximately 166,000 times that of water vapor drive. Various energy conservation cycle coalescing engines.   Application-specific bearing (80) Thrust bearing (80a) is provided to make the turbine blade cross section (4D) full-blade turbine drive, and it becomes high temperature when returning to the earth at the flight speed such as flight blade (38b) and flight tail (38c). A superheated steam (50) pipe that has been reduced in weight to high pressure with carbon nanotubes, etc., is connected to all the parts, and a high-pressure lightweight container is constructed. Heat recovery and atmospheric pressure, the same speed, and the same amount of heat output are about 1,656,000 driven by steam. Various energy conservation cycle coalescing engine to double.   Application-specific bearing (80) Thrust bearing (80a) is provided to make the turbine blade cross section (4D) full-blade turbine drive, and it becomes high temperature when returning to the earth at the flight speed such as flight blade (38b) and flight tail (38c). High-temperature mercury (1d) pipes that are lightened to high-pressure with carbon nanotubes, etc., are piped on all parts to construct a high-pressure light-weight container. Heat recovery and atmospheric pressure, the same speed, and the same amount of heat output are approximately 1,656,000 driven by steam. Various energy conservation cycle coalescing engine to double.   Application-specific bearing (80) Thrust bearing (80a) is provided to make the turbine blade cross section (4D) full-blade turbine drive, and it becomes high temperature when returning to the earth at the flight speed such as flight blade (38b) and flight tail (38c). Lightening to high pressure with carbon nanotubes, etc., with a combustion gas pipe, and a high-pressure lightweight container. Heat recovery and atmospheric pressure, the same speed and the same amount of heat output are approximately 166,000 times that of water vapor drive, etc. Various energy conservation cycle coalescing engines.   Application-specific bearing (80) Thrust bearing (80a) is provided for turbine blade cross-section (4D) full rotor blade drive, combustion gas (49) is recovered by intake air (28a), and heat pump (1G) Various energy storage cycle coalescing engines that recover heat at a compression of 500 to 1000 degrees, etc., and drive all rotor blade water turbines and output atmospheric pressure at the same speed and the same amount of heat about 166,000 times that of steam drive.   Application-specific bearing (80) Thrust bearing (80a) is provided for turbine blade cross-section (4D) full rotor blade drive, combustion gas (49) is recovered by intake air (28a), and heat pump (1G) Various energy storage cycle coalescing engines that recover heat at a compression of 500 to 1000 degrees, etc., and drive the whole moving blade mercury turbine to produce the same atmospheric pressure at the same speed and the same calorific power output as approximately 166,000 times that of the steam drive.   Application-specific bearing (80) Thrust bearing (80a) is provided for turbine blade cross-section (4D) full rotor blade drive, combustion gas (49) is recovered by intake air (28a), and heat pump (1G) Various energy storage cycle coalescing engines that recover heat at a compression of 500 to 1000 degrees, etc., and drive all rotor blade gas turbines to produce the same atmospheric pressure, same speed, and same calorie output, approximately 166,000 times that of steam drive.   Application-specific bearing (80) Thrust bearing (80a) is provided for turbine blade cross-section (4D) full rotor blade drive, combustion gas (49) is recovered by intake air (28a), and heat pump (1G) Various energy storage cycle coalescing engines that recover heat by compression to 500 to 1000 degrees, etc., and drive the combined engine injection section (79K) and output atmospheric pressure at the same speed and the same amount of heat approximately 166,000 times that of steam driving.   Application-specific bearing (80) Thrust bearing (80a) is provided for turbine blade cross-section (4D) full rotor blade drive, combustion gas (49) is recovered by intake air (28a), and heat pump (1G) Combined with various energy storage cycles to recover heat to 500-1000 degrees of compression, etc. to drive a water jet (79M) all-blade mercury turbine and to produce atmospheric pressure at the same speed and heat output of about 166,000 times that of steam organ.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive the turbine blade cross section (4D) for full rotor blade turbine, and the amount of compressed air (28b) is recovered by intake air (28a) to obtain a heat pump (1G) Various energy storage cycle coalescing engines that recover heat by compression to 500 to 1000 degrees, etc., and drive the combined engine injection section (79K) and output atmospheric pressure at the same speed and the same amount of heat approximately 166,000 times that of steam driving.   Application-specific bearing (80) Thrust bearing (80a) is provided to drive the turbine blade cross section (4D) for full rotor blade turbine, and the amount of compressed air (28b) is recovered by intake air (28a) to obtain a heat pump (1G) Various energy storage cycle coalescing engines that recover heat at a compression of 500 to 1000 degrees, etc., and drive the water jet (79M) and the atmospheric pressure, the same speed, and the same calorie output to about 166,000 times that of the steam drive.   The bearing (80) thrust bearing (80a) for the application is provided for safe operation, and the bearing (80) thrust is applied to the all-blade combustion section (32X) vertical all-blade gas turbine (8A) of the turbine blade cross section (4D). Various energy storage cycle coalescing engines as various ships driven by providing bearings (80a).   The bearing (80) thrust bearing (80a) for the application is provided for safe operation, and the bearing (80) thrust is applied to the all blade combustion part (32Y) vertical all blade gas turbine (8A) of the turbine blade cross section (4D). Various energy storage cycle coalescing engines as various ships driven by providing bearings (80a).   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the combined engine combustion section (31Y) full blade impeller gas turbine (8a) with a turbine blade cross section (4D) has a bearing (80) thrust bearing ( Various energy storage cycle coalescing engines which are 80a) and driven by various ships.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the combined engine combustion section (31X) full-blade propeller gas turbine (8a) of the turbine blade cross section (4D) is equipped with a bearing (80) thrust bearing ( Various energy storage cycle coalescing engines which are 80a) and driven by various ships.   The bearing (80) thrust bearing (80a) for the application is provided for safe operation, and the bearing (80) thrust is applied to the all-blade combustion section (32X) vertical all-blade gas turbine (8A) of the turbine blade cross section (4D). Various energy storage cycle coalescing engines as various ships driven by providing a bearing (80a) cold energy recovery means (3C).   The bearing (80) thrust bearing (80a) for the application is provided for safe operation, and the bearing (80) thrust is applied to the all blade combustion part (32Y) vertical all blade gas turbine (8A) of the turbine blade cross section (4D). Various energy storage cycle coalescing engines as various ships driven by providing a bearing (80a) cold energy recovery means (3C).   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the combined engine combustion section (31Y) full blade impeller gas turbine (8a) with a turbine blade cross section (4D) has a bearing (80) thrust bearing ( 80a) Various energy storage cycle coalescing engines, which are various ships that are provided with a cold heat recovery means (3C) and are driven.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the combined engine combustion section (31X) full-blade propeller gas turbine (8a) of the turbine blade cross section (4D) is equipped with a bearing (80) thrust bearing ( 80a) Various energy storage cycle coalescing engines, which are various ships that are provided with a cold heat recovery means (3C) and are driven.   The bearing (80) thrust bearing (80a) for the application is provided for safe operation, and the bearing (80) thrust is applied to the all-blade combustion section (32X) vertical all-blade gas turbine (8A) of the turbine blade cross section (4D). Various energy storage cycle coalescing engines as various ships which are provided with a bearing (80a) and a cold heat recovery device (103).   The bearing (80) thrust bearing (80a) for the application is provided for safe operation, and the bearing (80) thrust is applied to the all blade combustion part (32Y) vertical all blade gas turbine (8A) of the turbine blade cross section (4D). Various energy storage cycle coalescing engines as various ships which are provided with a bearing (80a) and a cold heat recovery device (103).   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the combined engine combustion section (31X) full-blade propeller gas turbine (8a) of the turbine blade cross section (4D) is equipped with a bearing (80) thrust bearing ( 80a) Various energy storage cycle coalescing engines that are provided with a cold heat recovery device (103) to be driven.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the combined engine combustion section (31Y) full blade impeller gas turbine (8a) with a turbine blade cross section (4D) has a bearing (80) thrust bearing ( 80a) Various energy storage cycle coalescing engines that are provided with a cold heat recovery device (103) to be driven.   The bearing (80) thrust bearing (80a) for the application is provided for safe operation, and the bearing (80) thrust is applied to the all-blade combustion section (32X) vertical all-blade gas turbine (8A) of the turbine blade cross section (4D). Various energy storage cycle coalescing engines as various ships that are provided with a bearing (80a) and a cold energy recovery device (103) (103).   The bearing (80) thrust bearing (80a) for the application is provided for safe operation, and the bearing (80) thrust is applied to the all blade combustion part (32Y) vertical all blade gas turbine (8A) of the turbine blade cross section (4D). Various energy storage cycle coalescing engines as various ships that are provided with a bearing (80a) and a cold energy recovery device (103) (103).   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the combined engine combustion section (31X) full-blade propeller gas turbine (8a) of the turbine blade cross section (4D) is equipped with a bearing (80) thrust bearing ( 80a) Various energy storage cycle coalescing engines which are provided with various cold vessels (103) and (103) to be driven.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the combined engine combustion section (31Y) full blade impeller gas turbine (8a) with a turbine blade cross section (4D) has a bearing (80) thrust bearing ( 80a) Various energy storage cycle coalescing engines which are provided with various cold vessels (103) and (103) to be driven.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided for safe operation, and a combined engine combustion section (31X) full blade impeller gas turbine (8a) with a turbine blade cross section (4D) is around 150 degrees Celsius around 24 to 300 MPa. Various energy storage cycle coalescing engines as various ships driven by combustion gas (49).   A bearing (80) for the application (80a) is provided for safe operation by providing a thrust bearing (80a), and a combined engine combustion section (31Y) full blade impeller gas turbine (8a) with a turbine blade cross section (4D) is around 150 degrees Celsius around 24 to 300 MPa. Various energy storage cycle coalescing engines as various ships driven by combustion gas (49).   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the turbine blade cross section (4D) full blade combustion section (32X) vertical all blade gas turbine (8A) is around 150 degrees Celsius 24 Various energy storage cycle coalescing engines as various ships driven by ~ 300 MPa combustion gas (49).   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the entire blade combustion part (32Y) vertical all blade gas turbine (8A) of the turbine blade cross section (4D) is around 150 degrees Celsius 24 Various energy storage cycle coalescing engines as various ships driven by ~ 300 MPa combustion gas (49).   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the combined engine combustion section (31X) full blade impeller gas turbine (8a) of the turbine blade cross section (4D) is around 200 degrees Celsius around 24 to 300 MPa. Various energy storage cycle coalescing engines as various ships driven by combustion gas (49).   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and a combined engine combustion section (31Y) full blade impeller gas turbine (8a) with a turbine blade cross section (4D) is set to around 200 degrees Celsius around 24 to 300 MPa. Various energy storage cycle coalescing engines as various ships driven by combustion gas (49).   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the entire blade combustion section (32X) vertical all-blade gas turbine (8A) with a turbine blade cross section (4D) is set to around 200 degrees Celsius 24 Various energy storage cycle coalescing engines as various ships driven by ~ 300 MPa combustion gas (49).   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and a turbine blade cross section (4D) full blade combustion section (32Y) vertical all blade gas turbine (8A) is set to around 200 degrees Celsius 24 Various energy storage cycle coalescing engines as various ships driven by ~ 300 MPa combustion gas (49).   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the whole blade combustion part (32X) vertical all blade gas turbine (8A) with a turbine blade cross section (4D) is set to around 300 degrees Celsius 24 Various energy storage cycle coalescing engines as various ships driven by ~ 300 MPa combustion gas (49).   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32Y) vertical all blade gas turbine (8A) is set around 300 degrees Celsius 24 Various energy storage cycle coalescing engines as various ships driven by ~ 300 MPa combustion gas (49).   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and a combined engine combustion section (31X) full blade impeller gas turbine (8a) with a turbine blade cross section (4D) is set to around 300 degrees Celsius around 24 to 300 MPa. Various energy storage cycle coalescing engines as various ships driven by combustion gas (49).   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the combined engine combustion section (31Y) full blade impeller gas turbine (8a) with a turbine blade cross section (4D) is set to around 300 degrees Celsius around 24 to 300 MPa. Various energy storage cycle coalescing engines as various ships driven by combustion gas (49).   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided for safe operation, and the combined engine combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven by a high-pressure turbine below the critical temperature to consume heat. Various energy conservation cycle coalescing engines, which are made to be various ship types that make 1/72 etc.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided for safe operation, and the combined combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven by a high-pressure turbine below the critical temperature to consume heat. Various energy conservation cycle coalescing engines, which are made to be various ship types that make 1/72 etc.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) is driven by high-pressure turbine driving below the critical temperature. Various energy storage cycle coalescing engines with various heats that reduce the amount of heat to approximately 1/72.   Provided bearing (80) for application and thrust bearing (80a) for safe operation. Consists of turbine blade cross section (4D) full blade combustion part (32Y) high temperature mercury (1d) driven by high pressure turbine below critical temperature Various energy storage cycle coalescing engines with various heats that reduce the amount of heat to approximately 1/72.   A bearing (80) suitable for the application (80a) and a thrust bearing (80a) are provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) is driven at a high pressure turbine below 1000 degrees Celsius. Various energy storage cycle coalescing engines with various types of ships that reduce heat consumption to approximately 1/72.   A bearing (80) suitable for the application (80a) and a thrust bearing (80a) are provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32Y) high-temperature mercury (1d) is driven at a high pressure turbine below 1000 degrees Celsius. Various energy storage cycle coalescing engines with various types of ships that reduce heat consumption to approximately 1/72.   Consistent use of bearing (80) Thrust bearing (80a) for safe operation, combined combustion section (31X) high-temperature mercury (1d) of turbine blade cross section (4D) driven by high-pressure turbine at 1000 degrees Celsius or less Various energy storage cycle coalescing engines with various heats that reduce the amount of heat to approximately 1/72.   Consistent application (80) Thrust bearing (80a) is provided for safe operation, and combined combustion section (31Y) high-temperature mercury (1d) of turbine blade cross section (4D) is driven by high-pressure turbine driven at 1000 degrees Celsius or less. Various energy storage cycle coalescing engines with various heats that reduce the amount of heat to approximately 1/72.   Consistent application (80) Thrust bearing (80a) is provided for safe operation, and the combined combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven by high-pressure turbine at 800 degrees Celsius or less for consumption. Various energy storage cycle coalescing engines with various heats that reduce the amount of heat to approximately 1/72.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided for safe operation, and the combined combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven by a high-pressure turbine driven at 800 degrees Celsius or less. Various energy storage cycle coalescing engines with various heats that reduce the amount of heat to approximately 1/72.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) is driven by a high-pressure turbine at 800 degrees Celsius or less. Various energy storage cycle coalescing engines with various types of ships that reduce heat consumption to approximately 1/72.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32Y) high-temperature mercury (1d) is driven by a high-pressure turbine at 800 degrees Celsius or less. Various energy storage cycle coalescing engines with various types of ships that reduce heat consumption to approximately 1/72.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) is driven by a high-pressure turbine at 600 degrees Celsius or less. Various energy storage cycle coalescing engines with various types of ships that reduce heat consumption to approximately 1/72.   A bearing (80) suitable for the application (80a) and a thrust bearing (80a) are provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32Y) high-temperature mercury (1d) is driven by a high-pressure turbine at 600 degrees Celsius or less. Various energy storage cycle coalescing engines with various types of ships that reduce heat consumption to approximately 1/72.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided for safe operation, and the combined engine combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven by a high-pressure turbine driven at 600 degrees Celsius or less. Various energy storage cycle coalescing engines with various heats that reduce the amount of heat to approximately 1/72.   A bearing (80) suitable for the application (80a) is provided for safe operation, and the combined combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven by a high-pressure turbine driven at 600 degrees Celsius or less. Various energy storage cycle coalescing engines with various heats that reduce the amount of heat to approximately 1/72.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the combined engine combustion section (31X) high-temperature water (52b) of the turbine blade cross section (4D) is driven by a high-pressure turbine below the critical temperature to consume heat. Various energy conservation cycle coalescing engines that are made to be various ship types with a 1/539 or the like.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the combined engine combustion section (31Y) high-temperature water (52b) in the turbine blade cross section (4D) is driven by a high-pressure turbine below the critical temperature to consume heat. Various energy conservation cycle coalescing engines that are made to be various ship types with a 1/539 or the like.   A bearing (80) suitable for the application (80a) and a thrust bearing (80a) are provided for safe operation, and the entire blade combustion section (32X) high-temperature water (52b) in the turbine blade cross section (4D) is driven by a high-pressure turbine below the critical temperature and consumed. Various energy storage cycle coalescing engines with various heats of approximately 1/539.   A bearing (80) suitable for the application and a thrust bearing (80a) are provided for safe operation, and the entire blade combustion section (32Y) high-temperature water (52b) on the turbine blade cross section (4D) is driven by a high-pressure turbine below the critical temperature and consumed. Various energy storage cycle coalescing engines with various heats of approximately 1/539.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the entire blade combustion section (32X) high-temperature water (52b) on the turbine blade cross section (4D) is driven by a high-pressure turbine to reduce the amount of heat consumed by approximately 1 / 539 etc. Various energy conservation cycle coalescing engines such as various ships.   The bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the whole blade combustion section (32Y) high temperature water (52b) on the turbine blade cross section (4D) is driven by the high-pressure turbine to reduce the amount of heat consumption to about 1 / 539 etc. Various energy conservation cycle coalescing engines such as various ships.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the combined engine combustion section (31X) high-temperature water (52b) on the turbine blade cross section (4D) is driven by a high-pressure turbine to reduce the heat consumption by approximately 1 / Various energy conservation cycle coalescing engines such as various ships such as 539.   The bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the combined engine combustion section (31Y) high-temperature water (52b) on the turbine blade cross section (4D) is driven by the high-pressure turbine to reduce the amount of heat consumption to approximately 1 / Various energy conservation cycle coalescing engines such as various ships such as 539.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and a high-pressure turbine is driven by a combined engine combustion section (31X) high-temperature water (52b) on the turbine blade cross section (4D) to output the same pressure at atmospheric pressure. Various energy storage cycle coalescing engines with various ship types that are 1700 times the weight of steam and m / sec.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and a high-pressure turbine is driven by the combined engine combustion section (31Y) high-temperature water (52b) on the turbine blade cross section (4D) to output the same pressure at atmospheric pressure. Various energy storage cycle coalescing engines with various ship types that are 1700 times the weight of steam and m / sec.   A bearing (80) thrust bearing (80a) for the application is provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32X) is driven by a high-pressure turbine with high-temperature water (52b) to output atmospheric pressure at the same speed. Various energy storage cycle coalescing engines, which are made of various ships that make 1700 times kg weight m / sec of steam drive.   A bearing (80) thrust bearing (80a) for application is provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32Y) is driven by high-pressure turbine with high-temperature water (52b) to output the same pressure at atmospheric pressure. Various energy storage cycle coalescing engines, which are made of various ships that make 1700 times kg weight m / sec of steam drive.   A bearing (80) suitable for the application (80a) is provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32X) high-temperature turbine is driven by high-temperature mercury (1d) to output atmospheric pressure at the same speed. Various energy storage cycle coalescing engines, which are made to be 23,000 times the weight of steam driven and 2 kg / kg weight m / sec.   Provided bearing (80) thrust bearing (80a) for application and safe operation, high-pressure turbine driven by full blade combustion section (32Y) high temperature mercury (1d) of turbine blade cross section (4D) Various energy storage cycle coalescing engines, which are made to be 23,000 times the weight of steam driven and 2 kg / kg weight m / sec.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the combined engine combustion section (31X) of the turbine blade cross section (4D) is driven by a high-pressure turbine with high-temperature mercury (1d) to output the same pressure at atmospheric pressure. Various energy storage cycle coalescing engines, which are 23,000 times the weight of steam driven and weighs m / sec.   A bearing (80) suitable for the application (80a) and a thrust bearing (80a) are provided for safe operation, and a combined turbine combustion section (31Y) of the turbine blade cross section (4D) is driven by a high-pressure turbine with high-temperature mercury (1d) to output the same pressure at atmospheric pressure. Various energy storage cycle coalescing engines, which are 23,000 times the weight of steam driven and weighs m / sec.   A bearing (80) thrust bearing (80a) for the application is provided for safe operation, and the high-pressure turbine is driven by the combined engine combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D), and the atmospheric pressure, the same speed, and the same amount of heat. Various energy conservation cycle coalescing engines whose output is a facility for supplying heat, electricity and cold, which is approximately 166,000 times the output of steam.   A bearing (80) thrust bearing (80a) for use is provided for safe operation, and a high-pressure turbine is driven by a combined engine combustion section (31Y) high-temperature mercury (1d) in the turbine blade cross section (4D), and the atmospheric pressure, the same speed, and the same amount of heat. Various energy conservation cycle coalescing engines whose output is a facility for supplying heat, electricity and cold, which is approximately 166,000 times the output of steam.   A bearing (80) suitable for the application and a thrust bearing (80a) are provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32X) high-temperature turbine is driven by high-temperature mercury (1d) to maintain the same atmospheric pressure and the same speed. Various energy storage cycle coalescing engines that use heat, electricity, and cold supply facilities that produce a heat output that is approximately 166,000 times that of water vapor drive.   Provided bearing (80) thrust bearing (80a) for application and safe operation, high pressure turbine driven by all blade combustion part (32Y) high temperature mercury (1d) of turbine blade cross section (4D) Various energy storage cycle coalescing engines that use heat, electricity, and cold supply facilities that produce a heat output that is approximately 166,000 times that of water vapor drive.   A bearing (80) suitable for the application and a thrust bearing (80a) are provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32X) high-temperature turbine is driven by high-temperature mercury (1d) to maintain the same atmospheric pressure and the same speed. Various energy storage cycle coalescing engines that make the calorific power about 166,000 times that of steam driven.   Provided bearing (80) thrust bearing (80a) for application and safe operation, high pressure turbine driven by all blade combustion part (32Y) high temperature mercury (1d) of turbine blade cross section (4D) Various energy storage cycle coalescing engines that make the calorific power about 166,000 times that of steam driven.   A bearing (80) thrust bearing (80a) for the application is provided for safe operation, and the high-pressure turbine is driven by the combined engine combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D), and the atmospheric pressure, the same speed, and the same amount of heat. Various energy conservation cycle coalescing engines whose output is about 166,000 times that of steam driven.   A bearing (80) thrust bearing (80a) for use is provided for safe operation, and a high-pressure turbine is driven by a combined engine combustion section (31Y) high-temperature mercury (1d) in the turbine blade cross section (4D), and the atmospheric pressure, the same speed, and the same amount of heat. Various energy conservation cycle coalescing engines whose output is about 166,000 times that of steam driven.   A bearing (80) thrust bearing (80a) for the application is provided for safe operation, and the high-pressure turbine is driven by the combined engine combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D), and the atmospheric pressure, the same speed, and the same amount of heat. Various energy storage cycle coalescing engines whose output is various airplanes whose output is approximately 166,000 times that of water vapor drive.   A bearing (80) thrust bearing (80a) for use is provided for safe operation, and a high-pressure turbine is driven by a combined engine combustion section (31Y) high-temperature mercury (1d) in the turbine blade cross section (4D), and the atmospheric pressure, the same speed, and the same amount of heat. Various energy storage cycle coalescing engines whose output is various airplanes whose output is approximately 166,000 times that of water vapor drive.   A bearing (80) suitable for the application and a thrust bearing (80a) are provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32X) high-temperature turbine is driven by high-temperature mercury (1d) to maintain the same atmospheric pressure and the same speed. Various energy storage cycle coalescing engines that produce various types of airplanes with a calorific power output of about 166,000 times that of steam drive.   Provided bearing (80) thrust bearing (80a) for application and safe operation, high pressure turbine driven by all blade combustion part (32Y) high temperature mercury (1d) of turbine blade cross section (4D) Various energy storage cycle coalescing engines that produce various types of airplanes with a calorific power output of about 166,000 times that of steam drive.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided for safe operation, and the turbine blade cross section (4D) full blade combustion section (32X) is driven by a high-pressure turbine with high-temperature water (52b) to maintain the same atmospheric pressure and speed. Various energy conservation cycle coalescing engines that make various kinds of airplanes whose calorie output is about 910,000 times that of steam drive.   A bearing (80) for thrust application (80a) is provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32Y) is driven by high-pressure turbine with high-temperature water (52b) to maintain the same atmospheric pressure and speed. Various energy conservation cycle coalescing engines that make various kinds of airplanes whose calorie output is about 910,000 times that of steam drive.   A bearing (80) thrust bearing (80a) for use is provided for safe operation, and the high-pressure turbine is driven by the combined engine combustion section (31X) high-temperature water (52b) of the turbine blade cross section (4D), and the atmospheric pressure, the same speed, and the same amount of heat. Various energy storage cycle coalescing engines that produce various airplanes whose output is about 910,000 times that of water vapor drive.   Provided bearing (80) thrust bearing (80a) for application and safe operation, combined engine combustion part (31Y) of turbine blade cross section (4D), high pressure turbine driven by high temperature water (52b), atmospheric pressure, same speed, same heat quantity Various energy storage cycle coalescing engines that produce various airplanes whose output is about 910,000 times that of water vapor drive.   A bearing (80) thrust bearing (80a) for use is provided for safe operation, and the high-pressure turbine is driven by the combined engine combustion section (31X) high-temperature water (52b) of the turbine blade cross section (4D), and the atmospheric pressure, the same speed, and the same amount of heat. Various energy storage cycle coalescing engines whose output is about 910,000 times that of steam driven.   Provided bearing (80) thrust bearing (80a) for application and safe operation, combined engine combustion part (31Y) of turbine blade cross section (4D), high pressure turbine driven by high temperature water (52b), atmospheric pressure, same speed, same heat quantity Various energy storage cycle coalescing engines whose output is about 910,000 times that of steam driven.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided for safe operation, and the turbine blade cross section (4D) full blade combustion section (32X) is driven by a high-pressure turbine with high-temperature water (52b) to maintain the same atmospheric pressure and speed. Various energy storage cycle coalescing engines that make the output of heat about 910,000 times that of water vapor drive.   A bearing (80) for thrust application (80a) is provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32Y) is driven by high-pressure turbine with high-temperature water (52b) to maintain the same atmospheric pressure and speed. Various energy storage cycle coalescing engines that make the output of heat about 910,000 times that of water vapor drive.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided for safe operation, and the turbine blade cross section (4D) full blade combustion section (32X) is driven by a high-pressure turbine with high-temperature water (52b) to maintain the same atmospheric pressure and speed. Various energy storage cycle coalescing engine with heat output of about 910,000 times that of steam drive, etc.   A bearing (80) for thrust application (80a) is provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32Y) is driven by high-pressure turbine with high-temperature water (52b) to maintain the same atmospheric pressure and speed. Various energy storage cycle coalescing engine with heat output of about 910,000 times that of steam drive, etc.   A bearing (80) thrust bearing (80a) for use is provided for safe operation, and the high-pressure turbine is driven by the combined engine combustion section (31X) high-temperature water (52b) of the turbine blade cross section (4D), and the atmospheric pressure, the same speed, and the same amount of heat. Various energy storage cycle coalescing engines whose output is about 910,000 times that of water vapor drive, etc.   Provided bearing (80) thrust bearing (80a) for application and safe operation, combined engine combustion part (31Y) of turbine blade cross section (4D), high pressure turbine driven by high temperature water (52b), atmospheric pressure, same speed, same heat quantity Various energy storage cycle coalescing engines whose output is about 910,000 times that of water vapor drive, etc.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided for safe operation, and the combined engine combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven by a high-pressure turbine below the critical temperature to consume heat. Various energy storage cycle coalescing engines with various heat, electricity, and cold supply facilities with approximately 1/72, atmospheric pressure, same speed and same calorie calculation output of 166,000 times.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided for safe operation, and the combined combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven by a high-pressure turbine below the critical temperature to consume heat. Various energy storage cycle coalescing engines with various heat, electricity, and cold supply facilities with approximately 1/72, atmospheric pressure, same speed and same calorie calculation output of 166,000 times.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) is driven by high-pressure turbine driving below the critical temperature. Various energy storage cycle coalescing engines with a heat supply of approximately 1/72, atmospheric pressure and speed and calorific value output of 1,656,000 times, etc. to provide various heat, electricity and cold supply facilities.   Provided bearing (80) for application and thrust bearing (80a) for safe operation. Consists of turbine blade cross section (4D) full blade combustion part (32Y) high temperature mercury (1d) driven by high pressure turbine below critical temperature Various energy storage cycle coalescing engines with a heat supply of approximately 1/72, atmospheric pressure and speed and calorific value output of 1,656,000 times, etc. to provide various heat, electricity and cold supply facilities.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) is driven by high-pressure turbine driving below the critical temperature. Various energy conservation cycle coalescing engines with various heat vessels with a heat quantity of approximately 1/72, atmospheric pressure, same speed, same calorie calculation output, 166,000 times, etc.   Provided bearing (80) for application and thrust bearing (80a) for safe operation. Consists of turbine blade cross section (4D) full blade combustion part (32Y) high temperature mercury (1d) driven by high pressure turbine below critical temperature Various energy conservation cycle coalescing engines with various heat vessels with a heat quantity of approximately 1/72, atmospheric pressure, same speed, same calorie calculation output, 166,000 times, etc.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided for safe operation, and the combined engine combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven by a high-pressure turbine below the critical temperature to consume heat. Various energy conservation cycle coalescing engines with various 1/72 and atmospheric pressure, same speed, and same calorie calculation outputs of 166,000 times.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided for safe operation, and the combined combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven by a high-pressure turbine below the critical temperature to consume heat. Various energy conservation cycle coalescing engines with various 1/72 and atmospheric pressure, same speed, and same calorie calculation outputs of 166,000 times.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided for safe operation, and the combined engine combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven by a high-pressure turbine below the critical temperature to consume heat. Various energy storage cycle coalescing engines with various air planes with approximately 1/72, atmospheric pressure, same speed, same calorie calculation output 166,000 times.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided for safe operation, and the combined combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven by a high-pressure turbine below the critical temperature to consume heat. Various energy storage cycle coalescing engines with various air planes with approximately 1/72, atmospheric pressure, same speed, same calorie calculation output 166,000 times.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) is driven by high-pressure turbine driving below the critical temperature. Various energy conservation cycle coalescing engines with various heats of approximately 1/72, atmospheric pressure, speed, and calorie calculation output of 166,000 times.   Provided bearing (80) for application and thrust bearing (80a) for safe operation. Consists of turbine blade cross section (4D) full blade combustion part (32Y) high temperature mercury (1d) driven by high pressure turbine below critical temperature Various energy conservation cycle coalescing engines with various heats of approximately 1/72, atmospheric pressure, speed, and calorie calculation output of 166,000 times.   A bearing (80) suitable for the application (80a) and a thrust bearing (80a) are provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) is driven at a high pressure turbine below 1000 degrees Celsius. Various energy conservation cycle coalescing engines with various heat consumptions of approximately 1/72 and atmospheric pressure and speed and calorie calculation output of 166,000 times.   A bearing (80) suitable for the application (80a) and a thrust bearing (80a) are provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32Y) high-temperature mercury (1d) is driven at a high pressure turbine below 1000 degrees Celsius. Various energy conservation cycle coalescing engines with various heat consumptions of approximately 1/72 and atmospheric pressure and speed and calorie calculation output of 166,000 times.   Consistent use of bearing (80) Thrust bearing (80a) for safe operation, combined combustion section (31X) high-temperature mercury (1d) of turbine blade cross section (4D) driven by high-pressure turbine at 1000 degrees Celsius or less Various energy conservation cycle coalescing engines that make the amount of heat about 1/72 and various airplanes with atmospheric pressure, same speed, and same calorie calculation output 166,000 times.   Consistent application (80) Thrust bearing (80a) is provided for safe operation, and combined combustion section (31Y) high-temperature mercury (1d) of turbine blade cross section (4D) is driven by high-pressure turbine driven at 1000 degrees Celsius or less. Various energy conservation cycle coalescing engines that make the amount of heat about 1/72 and various airplanes with atmospheric pressure, same speed, and same calorie calculation output 166,000 times.   Consistent use (80) Thrust bearing (80a) is provided for safe operation. Combined engine combustion section (31X) high-temperature mercury (1d) of turbine blade cross section (4D) is driven by high-pressure turbine driven at 1000 degrees Celsius or less. Various energy conservation cycle coalescing engines that make the amount of heat approximately 1/72, various atmospheric pressures at the same speed and calorie calculation output 166,000 times.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided for safe operation, and the combined combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven by high-pressure turbine at 1000 degrees Celsius or less. Various energy conservation cycle coalescing engines that make the amount of heat approximately 1/72, various atmospheric pressures at the same speed and calorie calculation output 166,000 times.   A bearing (80) suitable for the application (80a) and a thrust bearing (80a) are provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) is driven at a high pressure turbine below 1000 degrees Celsius. Various energy conservation cycle coalescing engines with various heat consumptions of approximately 1/72 and atmospheric pressure, speed, and calorie calculation output of 1,656,000 times.   A bearing (80) suitable for the application (80a) and a thrust bearing (80a) are provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32Y) high-temperature mercury (1d) is driven at a high pressure turbine below 1000 degrees Celsius. Various energy conservation cycle coalescing engines with various heat consumptions of approximately 1/72 and atmospheric pressure, speed, and calorie calculation output of 1,656,000 times.   A bearing (80) suitable for the application (80a) and a thrust bearing (80a) are provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) is driven at a high pressure turbine below 1000 degrees Celsius. Various energy storage cycle coalescing engines that use various heat, electricity, and cold supply facilities such as approximately 1/72 of the consumed heat and the atmospheric pressure and speed and calorie calculation output of 1,656,000 times.   A bearing (80) suitable for the application (80a) and a thrust bearing (80a) are provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32Y) high-temperature mercury (1d) is driven at a high pressure turbine below 1000 degrees Celsius. Various energy storage cycle coalescing engines that use various heat, electricity, and cold supply facilities such as approximately 1/72 of the consumed heat and the atmospheric pressure and speed and calorie calculation output of 1,656,000 times.   Consistent use (80) Thrust bearing (80a) is provided for safe operation. Combined engine combustion section (31X) high-temperature mercury (1d) of turbine blade cross section (4D) is driven by high-pressure turbine driven at 1000 degrees Celsius or less. Various energy storage cycle coalescing engines that use various heat, electricity and cold supply facilities, such as approximately 1/72 of heat and atmospheric pressure at the same speed and heat output of 1,656,000 times.   Consistent application (80) Thrust bearing (80a) is provided for safe operation, and combined combustion section (31Y) high-temperature mercury (1d) of turbine blade cross section (4D) is driven by high-pressure turbine driven at 1000 degrees Celsius or less. Various energy storage cycle coalescing engines that use various heat, electricity and cold supply facilities, such as approximately 1/72 of heat and atmospheric pressure at the same speed and heat output of 1,656,000 times.   Consistent application (80) Thrust bearing (80a) is provided for safe operation, and the combined combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven by high-pressure turbine at 800 degrees Celsius or less for consumption. Various energy storage cycle coalescing engines that use various heat, electricity and cold supply facilities, such as approximately 1/72 of heat and atmospheric pressure at the same speed and heat output of 1,656,000 times.   Consistent application (80) Thrust bearing (80a) is provided for safe operation, and the combined combustion section (31Y) high-temperature mercury (1d) in the turbine blade cross section (4D) is driven by high-pressure turbine at 800 degrees Celsius or less. Various energy storage cycle coalescing engines that use various heat, electricity and cold supply facilities, such as approximately 1/72 of heat and atmospheric pressure at the same speed and heat output of 1,656,000 times.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) is driven by a high-pressure turbine at 800 degrees Celsius or less. Various energy storage cycle coalescing engines that use various heat, electricity, and cold supply facilities such as approximately 1/72 of the consumed heat and the atmospheric pressure and speed and calorie calculation output of 1,656,000 times.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32Y) high-temperature mercury (1d) is driven by a high-pressure turbine at 800 degrees Celsius or less. Various energy storage cycle coalescing engines that use various heat, electricity, and cold supply facilities such as approximately 1/72 of the consumed heat and the atmospheric pressure and speed and calorie calculation output of 1,656,000 times.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) is driven by a high-pressure turbine at 800 degrees Celsius or less. Various energy conservation cycle coalescing engines with various heat consumptions of approximately 1/72 and atmospheric pressure, speed, and calorie calculation output of 1,656,000 times.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32Y) high-temperature mercury (1d) is driven by a high-pressure turbine at 800 degrees Celsius or less. Various energy conservation cycle coalescing engines with various heat consumptions of approximately 1/72 and atmospheric pressure, speed, and calorie calculation output of 1,656,000 times.   Consistent application (80) Thrust bearing (80a) is provided for safe operation, and the combined combustion section (31X) high-temperature mercury (1d) in the turbine blade cross section (4D) is driven by high-pressure turbine at 800 degrees Celsius or less. Various energy conservation cycle coalescing engines that make the amount of heat approximately 1/72, various atmospheric pressures at the same speed and calorie calculation output 166,000 times.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided for safe operation, and the combined combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven by a high-pressure turbine driven at 800 degrees Celsius or less. Various energy conservation cycle coalescing engines that make the amount of heat approximately 1/72, various atmospheric pressures at the same speed and calorie calculation output 166,000 times.   Consistent application (80) Thrust bearing (80a) is provided for safe operation, and the combined combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven by high-pressure turbine at 800 degrees Celsius or less for consumption. Various energy conservation cycle coalescing engines that make the amount of heat about 1/72 and various airplanes with atmospheric pressure, same speed, and same calorie calculation output 166,000 times.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided for safe operation, and the combined combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven by a high-pressure turbine driven at 800 degrees Celsius or less. Various energy conservation cycle coalescing engines that make the amount of heat about 1/72 and various airplanes with atmospheric pressure, same speed, and same calorie calculation output 166,000 times.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) is driven by a high-pressure turbine at 800 degrees Celsius or less. Various energy conservation cycle coalescing engines with various heat consumptions of approximately 1/72 and atmospheric pressure and speed and calorie calculation output of 166,000 times.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32Y) high-temperature mercury (1d) is driven by a high-pressure turbine at 800 degrees Celsius or less. Various energy conservation cycle coalescing engines with various heat consumptions of approximately 1/72 and atmospheric pressure and speed and calorie calculation output of 166,000 times.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) is driven by a high-pressure turbine at 600 degrees Celsius or less. Various energy conservation cycle coalescing engines with various heat consumptions of approximately 1/72 and atmospheric pressure and speed and calorie calculation output of 166,000 times.   A bearing (80) suitable for the application (80a) and a thrust bearing (80a) are provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32Y) high-temperature mercury (1d) is driven by a high-pressure turbine at 600 degrees Celsius or less. Various energy conservation cycle coalescing engines with various heat consumptions of approximately 1/72 and atmospheric pressure and speed and calorie calculation output of 166,000 times.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided for safe operation, and the combined engine combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven by a high-pressure turbine driven at 600 degrees Celsius or less. Various energy conservation cycle coalescing engines that make the amount of heat about 1/72 and various airplanes with atmospheric pressure, same speed, and same calorie calculation output 166,000 times.   A bearing (80) suitable for the application (80a) is provided for safe operation, and the combined combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven by a high-pressure turbine driven at 600 degrees Celsius or less. Various energy conservation cycle coalescing engines that make the amount of heat about 1/72 and various airplanes with atmospheric pressure, same speed, and same calorie calculation output 166,000 times.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided for safe operation, and the combined engine combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven by a high-pressure turbine driven at 600 degrees Celsius or less. Various energy conservation cycle coalescing engines that make the amount of heat approximately 1/72, various atmospheric pressures at the same speed and calorie calculation output 166,000 times.   A bearing (80) suitable for the application (80a) is provided for safe operation, and the combined combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven by a high-pressure turbine driven at 600 degrees Celsius or less. Various energy conservation cycle coalescing engines that make the amount of heat approximately 1/72, various atmospheric pressures at the same speed and calorie calculation output 166,000 times.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) is driven by a high-pressure turbine at 600 degrees Celsius or less. Various energy conservation cycle coalescing engines with various heat consumptions of approximately 1/72 and atmospheric pressure, speed, and calorie calculation output of 1,656,000 times.   A bearing (80) suitable for the application (80a) and a thrust bearing (80a) are provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32Y) high-temperature mercury (1d) is driven by a high-pressure turbine at 600 degrees Celsius or less. Various energy conservation cycle coalescing engines with various heat consumptions of approximately 1/72 and atmospheric pressure, speed, and calorie calculation output of 1,656,000 times.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) is driven by a high-pressure turbine at 600 degrees Celsius or less. Various energy storage cycle coalescing engines that use various heat, electricity, and cold supply facilities such as approximately 1/72 of the consumed heat and the atmospheric pressure and speed and calorie calculation output of 1,656,000 times.   A bearing (80) suitable for the application (80a) and a thrust bearing (80a) are provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32Y) high-temperature mercury (1d) is driven by a high-pressure turbine at 600 degrees Celsius or less. Various energy storage cycle coalescing engines that use various heat, electricity, and cold supply facilities such as approximately 1/72 of the consumed heat and the atmospheric pressure and speed and calorie calculation output of 1,656,000 times.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) are provided for safe operation, and the combined engine combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven by a high-pressure turbine driven at 600 degrees Celsius or less. Various energy storage cycle coalescing engines that use various heat, electricity and cold supply facilities, such as approximately 1/72 of heat and atmospheric pressure at the same speed and heat output of 1,656,000 times.   A bearing (80) suitable for the application (80a) is provided for safe operation, and the combined combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven by a high-pressure turbine driven at 600 degrees Celsius or less. Various energy storage cycle coalescing engines that use various heat, electricity and cold supply facilities, such as approximately 1/72 of heat and atmospheric pressure at the same speed and heat output of 1,656,000 times.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the combined engine combustion section (31X) high-temperature water (52b) of the turbine blade cross section (4D) is driven by a high-pressure turbine below the critical temperature to consume heat. Various energy storage cycle coalescence engines that make various heat, electricity and cold supply facilities such as approximately 1/539, atmospheric pressure, same speed, same calorie calculation output 910,000 times.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the combined engine combustion section (31Y) high-temperature water (52b) in the turbine blade cross section (4D) is driven by a high-pressure turbine below the critical temperature to consume heat. Various energy storage cycle coalescence engines that make various heat, electricity and cold supply facilities such as approximately 1/539, atmospheric pressure, same speed, same calorie calculation output 910,000 times.   A bearing (80) suitable for the application (80a) and a thrust bearing (80a) are provided for safe operation, and the entire blade combustion section (32X) high-temperature water (52b) in the turbine blade cross section (4D) is driven by a high-pressure turbine below the critical temperature and consumed. Various energy storage cycle coalescing engines that use various heat, electricity and cold supply facilities such as heat output of approximately 1/539 and atmospheric pressure at the same speed and heat output of 910,000 times.   A bearing (80) suitable for the application and a thrust bearing (80a) are provided for safe operation, and the entire blade combustion section (32Y) high-temperature water (52b) on the turbine blade cross section (4D) is driven by a high-pressure turbine below the critical temperature and consumed. Various energy storage cycle coalescing engines that use various heat, electricity and cold supply facilities such as heat output of approximately 1/539 and atmospheric pressure at the same speed and heat output of 910,000 times.   A bearing (80) suitable for the application (80a) and a thrust bearing (80a) are provided for safe operation, and the entire blade combustion section (32X) high-temperature water (52b) in the turbine blade cross section (4D) is driven by a high-pressure turbine below the critical temperature and consumed. Various energy conservation cycle coalescing engines that make the amount of heat about 1/539 and various ships with atmospheric pressure at the same speed and calorie calculation output 910,000 times.   A bearing (80) suitable for the application and a thrust bearing (80a) are provided for safe operation, and the entire blade combustion section (32Y) high-temperature water (52b) on the turbine blade cross section (4D) is driven by a high-pressure turbine below the critical temperature and consumed. Various energy conservation cycle coalescing engines that make the amount of heat about 1/539 and various ships with atmospheric pressure at the same speed and calorie calculation output 910,000 times.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the combined engine combustion section (31X) high-temperature water (52b) of the turbine blade cross section (4D) is driven by a high-pressure turbine below the critical temperature to consume heat. Various energy conservation cycle coalescing engines that make various ships of about 1/539, atmospheric pressure, same speed, same calorie calculation output 910,000 times.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the combined engine combustion section (31Y) high-temperature water (52b) in the turbine blade cross section (4D) is driven by a high-pressure turbine below the critical temperature to consume heat. Various energy conservation cycle coalescing engines that make various ships of about 1/539, atmospheric pressure, same speed, same calorie calculation output 910,000 times.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the combined engine combustion section (31X) high-temperature water (52b) of the turbine blade cross section (4D) is driven by a high-pressure turbine below the critical temperature to consume heat. Various energy conservation cycle coalescing engines that make the aircraft approximately 1/539, atmospheric pressure, same speed, same calorie calculation output 910,000 times.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the combined engine combustion section (31Y) high-temperature water (52b) in the turbine blade cross section (4D) is driven by a high-pressure turbine below the critical temperature to consume heat. Various energy conservation cycle coalescing engines that make the aircraft approximately 1/539, atmospheric pressure, same speed, same calorie calculation output 910,000 times.   A bearing (80) suitable for the application (80a) and a thrust bearing (80a) are provided for safe operation, and the entire blade combustion section (32X) high-temperature water (52b) in the turbine blade cross section (4D) is driven by a high-pressure turbine below the critical temperature and consumed. Various energy storage cycle coalescing engines that make various kinds of airplanes with a calorific value of approximately 1/539 and atmospheric pressure, same speed, and same calorie output 910,000 times.   A bearing (80) suitable for the application and a thrust bearing (80a) are provided for safe operation, and the entire blade combustion section (32Y) high-temperature water (52b) on the turbine blade cross section (4D) is driven by a high-pressure turbine below the critical temperature and consumed. Various energy storage cycle coalescing engines that make various kinds of airplanes with a calorific value of approximately 1/539 and atmospheric pressure, same speed, and same calorie output 910,000 times.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the entire blade combustion section (32X) high-temperature water (52b) on the turbine blade cross section (4D) is driven by a high-pressure turbine to reduce the amount of heat consumed by approximately 1 / 539 and various energy conservation cycle coalescing engines to make various airplanes such as atmospheric pressure, same speed, same calorie calculation output 910,000 times.   The bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the whole blade combustion section (32Y) high temperature water (52b) on the turbine blade cross section (4D) is driven by the high-pressure turbine to reduce the amount of heat consumption to about 1 / 539 and various energy conservation cycle coalescing engines to make various airplanes such as atmospheric pressure, same speed, same calorie calculation output 910,000 times.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the combined engine combustion section (31X) high-temperature water (52b) on the turbine blade cross section (4D) is driven by a high-pressure turbine to reduce the heat consumption by approximately 1 / Various energy storage cycle coalescing engines such as 539 and various airplanes such as atmospheric pressure, same speed, same calorie calculation output 910,000 times.   The bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the combined engine combustion section (31Y) high-temperature water (52b) on the turbine blade cross section (4D) is driven by the high-pressure turbine to reduce the amount of heat consumption to approximately 1 / Various energy storage cycle coalescing engines such as 539 and various airplanes such as atmospheric pressure, same speed, same calorie calculation output 910,000 times.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the combined engine combustion section (31X) high-temperature water (52b) on the turbine blade cross section (4D) is driven by a high-pressure turbine to reduce the heat consumption by approximately 1 / 539 and various energy conservation cycle coalescing engines for various ships such as atmospheric pressure, same speed, same calorie calculation output 910,000 times.   The bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the combined engine combustion section (31Y) high-temperature water (52b) on the turbine blade cross section (4D) is driven by the high-pressure turbine to reduce the amount of heat consumption to approximately 1 / 539 and various energy conservation cycle coalescing engines for various ships such as atmospheric pressure, same speed, same calorie calculation output 910,000 times.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the entire blade combustion section (32X) high-temperature water (52b) on the turbine blade cross section (4D) is driven by a high-pressure turbine to reduce the amount of heat consumed by approximately 1 / 539 and various energy storage cycle coalescing engines to make various ships such as atmospheric pressure, same speed, same calorie calculation output 910,000 times.   The bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the whole blade combustion section (32Y) high temperature water (52b) on the turbine blade cross section (4D) is driven by the high-pressure turbine to reduce the amount of heat consumption to about 1 / 539 and various energy storage cycle coalescing engines to make various ships such as atmospheric pressure, same speed, same calorie calculation output 910,000 times.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the entire blade combustion section (32X) high-temperature water (52b) on the turbine blade cross section (4D) is driven by a high-pressure turbine to reduce the amount of heat consumed by approximately 1 / 539 and various energy storage cycle coalescence engine to make various heat, electricity and cold supply facilities such as atmospheric pressure, same speed, same calorie calculation output 910,000 times.   The bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the whole blade combustion section (32Y) high temperature water (52b) on the turbine blade cross section (4D) is driven by the high-pressure turbine to reduce the amount of heat consumption to about 1 / 539 and various energy storage cycle coalescence engine to make various heat, electricity and cold supply facilities such as atmospheric pressure, same speed, same calorie calculation output 910,000 times.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the combined engine combustion section (31X) high-temperature water (52b) on the turbine blade cross section (4D) is driven by a high-pressure turbine to reduce the heat consumption by approximately 1 / 539 and various energy conservation cycle coalescence engines that use various heat, electricity, and cold supply facilities such as atmospheric pressure, same speed, and same calorie calculation output 910,000 times.   The bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the combined engine combustion section (31Y) high-temperature water (52b) on the turbine blade cross section (4D) is driven by the high-pressure turbine to reduce the amount of heat consumption to approximately 1 / 539 and various energy conservation cycle coalescence engines that use various heat, electricity, and cold supply facilities such as atmospheric pressure, same speed, and same calorie calculation output 910,000 times.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and a high-pressure turbine is driven by a combined engine combustion section (31X) high-temperature water (52b) on the turbine blade cross section (4D) to output the same pressure at atmospheric pressure. Various energy storage cycle coalescing engines that provide various heat, electricity, and cold supply facilities with additional gravity acceleration in vacuum, such as steam-driven 1700 times kg weight m / sec and atmospheric pressure, same speed, and same calorie calculation output 910,000 times.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and a high-pressure turbine is driven by the combined engine combustion section (31Y) high-temperature water (52b) on the turbine blade cross section (4D) to output the same pressure at atmospheric pressure. Various energy storage cycle coalescing engines that provide various heat, electricity, and cold supply facilities with additional gravity acceleration in vacuum, such as steam-driven 1700 times kg weight m / sec and atmospheric pressure, same speed, and same calorie calculation output 910,000 times.   A bearing (80) thrust bearing (80a) for the application is provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32X) is driven by a high-pressure turbine with high-temperature water (52b) to output atmospheric pressure at the same speed. Various energy storage cycle coalescence engines that make various heat, electricity and cold supply equipment with gravity acceleration added in vacuum to steam driven 1700 times kg weight m / second, atmospheric pressure same speed same heat quantity calculation output 910,000 times, etc. .   A bearing (80) thrust bearing (80a) for application is provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32Y) is driven by high-pressure turbine with high-temperature water (52b) to output the same pressure at atmospheric pressure. Various energy storage cycle coalescence engines that make various heat, electricity and cold supply equipment with gravity acceleration added in vacuum to steam driven 1700 times kg weight m / second, atmospheric pressure same speed same heat quantity calculation output 910,000 times, etc. .   A bearing (80) thrust bearing (80a) for the application is provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32X) is driven by a high-pressure turbine with high-temperature water (52b) to output atmospheric pressure at the same speed. Various energy storage cycle coalescing engines that make the steam-driven 1700 times kg weight m / second, atmospheric pressure, the same speed and the same calorie output, 910,000 times the atmospheric pressure, etc.   A bearing (80) thrust bearing (80a) for application is provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32Y) is driven by high-pressure turbine with high-temperature water (52b) to output the same pressure at atmospheric pressure. Various energy storage cycle coalescing engines that make the steam-driven 1700 times kg weight m / second, atmospheric pressure, the same speed and the same calorie output, 910,000 times the atmospheric pressure, etc.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and a high-pressure turbine is driven by a combined engine combustion section (31X) high-temperature water (52b) on the turbine blade cross section (4D) to output the same pressure at atmospheric pressure. Various energy storage cycle coalescing engines to make various ships with gravity acceleration added in vacuum to steam driven 1700 times kg weight m / second, atmospheric pressure same speed same heat quantity calculation output 910,000 times, etc.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and a high-pressure turbine is driven by the combined engine combustion section (31Y) high-temperature water (52b) on the turbine blade cross section (4D) to output the same pressure at atmospheric pressure. Various energy storage cycle coalescing engines to make various ships with gravity acceleration added in vacuum to steam driven 1700 times kg weight m / second, atmospheric pressure same speed same heat quantity calculation output 910,000 times, etc.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and a high-pressure turbine is driven by a combined engine combustion section (31X) high-temperature water (52b) on the turbine blade cross section (4D) to output the same pressure at atmospheric pressure. Various energy storage cycle coalescing engines that make various airplanes with gravity acceleration added in vacuum to steam driven 1700 times kg weight m / second, atmospheric pressure same speed same heat quantity calculation output 910,000 times.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and a high-pressure turbine is driven by the combined engine combustion section (31Y) high-temperature water (52b) on the turbine blade cross section (4D) to output the same pressure at atmospheric pressure. Various energy storage cycle coalescing engines that make various airplanes with gravity acceleration added in vacuum to steam driven 1700 times kg weight m / second, atmospheric pressure same speed same heat quantity calculation output 910,000 times.   A bearing (80) thrust bearing (80a) for the application is provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32X) is driven by a high-pressure turbine with high-temperature water (52b) to output atmospheric pressure at the same speed. Various energy conservation cycle coalescing engines that make various airplanes with gravity acceleration added in vacuum to steam driven 1700 times kg weight m / second, atmospheric pressure same speed same heat quantity calculation output 910,000 times, etc.   A bearing (80) thrust bearing (80a) for application is provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32Y) is driven by high-pressure turbine with high-temperature water (52b) to output the same pressure at atmospheric pressure. Various energy conservation cycle coalescing engines that make various airplanes with gravity acceleration added in vacuum to steam driven 1700 times kg weight m / second, atmospheric pressure same speed same heat quantity calculation output 910,000 times, etc.   A bearing (80) suitable for the application (80a) is provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32X) high-temperature turbine is driven by high-temperature mercury (1d) to output atmospheric pressure at the same speed. Various energy storage cycle coalescing engines that make the various types of airplanes with gravity acceleration added in vacuum to 23,000 times kg weight m / second of steam driven and atmospheric pressure same speed same heat quantity calculation output 166,000 times.   Provided bearing (80) thrust bearing (80a) for application and safe operation, high-pressure turbine driven by full blade combustion section (32Y) high temperature mercury (1d) of turbine blade cross section (4D) Various energy storage cycle coalescing engines that make the various types of airplanes with gravity acceleration added in vacuum to 23,000 times kg weight m / second of steam driven and atmospheric pressure same speed same heat quantity calculation output 166,000 times.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the combined engine combustion section (31X) of the turbine blade cross section (4D) is driven by a high-pressure turbine with high-temperature mercury (1d) to output the same pressure at atmospheric pressure. Various energy storage cycle coalescing engines to make various airplanes with gravity acceleration added in vacuum to steam driven 23,000 times kg weight m / second, atmospheric pressure, same speed and same calorie calculation output 166,000 times.   A bearing (80) suitable for the application (80a) and a thrust bearing (80a) are provided for safe operation, and a combined turbine combustion section (31Y) of the turbine blade cross section (4D) is driven by a high-pressure turbine with high-temperature mercury (1d) to output the same pressure at atmospheric pressure. Various energy storage cycle coalescing engines to make various airplanes with gravity acceleration added in vacuum to steam driven 23,000 times kg weight m / second, atmospheric pressure, same speed and same calorie calculation output 166,000 times.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the combined engine combustion section (31X) of the turbine blade cross section (4D) is driven by a high-pressure turbine with high-temperature mercury (1d) to output the same pressure at atmospheric pressure. Various energy storage cycle coalescing engines to make various ships with additional gravity acceleration in a vacuum, such as steam driven 23,000 times kg weight m / second, atmospheric pressure same speed and same calorie calculation output 166,000 times.   A bearing (80) suitable for the application (80a) and a thrust bearing (80a) are provided for safe operation, and a combined turbine combustion section (31Y) of the turbine blade cross section (4D) is driven by a high-pressure turbine with high-temperature mercury (1d) to output the same pressure at atmospheric pressure. Various energy storage cycle coalescing engines to make various ships with additional gravity acceleration in a vacuum, such as steam driven 23,000 times kg weight m / second, atmospheric pressure same speed and same calorie calculation output 166,000 times.   A bearing (80) suitable for the application (80a) is provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32X) high-temperature turbine is driven by high-temperature mercury (1d) to output atmospheric pressure at the same speed. Various energy conservation cycle coalescing engines that make the steam-driven 23,000 times kg weight m / second, atmospheric pressure, same speed, same calorie calculation output, 166,000 times, etc., in a variety of ships with gravity acceleration added in vacuum.   Provided bearing (80) thrust bearing (80a) for application and safe operation, high-pressure turbine driven by full blade combustion section (32Y) high temperature mercury (1d) of turbine blade cross section (4D) Various energy conservation cycle coalescing engines that make the steam-driven 23,000 times kg weight m / second, atmospheric pressure, same speed, same calorie calculation output, 166,000 times, etc., in a variety of ships with gravity acceleration added in vacuum.   A bearing (80) suitable for the application (80a) is provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32X) high-temperature turbine is driven by high-temperature mercury (1d) to output atmospheric pressure at the same speed. Various types of equipment for supplying heat, electricity and cold with additional gravity acceleration in vacuum to steam driven 23,000 times kg weight m / second, atmospheric pressure, same speed, same calorific value calculation output 166,000 times, etc. Energy conservation cycle coalescence engine.   Provided bearing (80) thrust bearing (80a) for application and safe operation, high-pressure turbine driven by full blade combustion section (32Y) high temperature mercury (1d) of turbine blade cross section (4D) Various types of equipment for supplying heat, electricity and cold with additional gravity acceleration in vacuum to steam driven 23,000 times kg weight m / second, atmospheric pressure, same speed, same calorific value calculation output 166,000 times, etc. Energy conservation cycle coalescence engine.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the combined engine combustion section (31X) of the turbine blade cross section (4D) is driven by a high-pressure turbine with high-temperature mercury (1d) to output the same pressure at atmospheric pressure. Various energy to be used to supply various heat, electricity and cold in vacuum with additional gravity acceleration in steam driven 23,000 times kg weight m / second, atmospheric pressure, same speed, same calorie calculation output 166,000 times, etc. Conservation cycle coalescence organization.   A bearing (80) suitable for the application (80a) and a thrust bearing (80a) are provided for safe operation, and a combined turbine combustion section (31Y) of the turbine blade cross section (4D) is driven by a high-pressure turbine with high-temperature mercury (1d) to output the same pressure at atmospheric pressure. Various energy to be used to supply various heat, electricity and cold in vacuum with additional gravity acceleration in steam driven 23,000 times kg weight m / second, atmospheric pressure, same speed, same calorie calculation output 166,000 times, etc. Conservation cycle coalescence organization.   Application-specific bearings (80) Thrust bearings (80a) are provided for safe operation, and the combined combustion section (31X) high-temperature mercury (1d) on the turbine blade cross section (4D) is vertically below the gravity acceleration added in the vacuum. Combined engine with various energy conservation cycles to increase the output of high-pressure turbine and atmospheric pressure at the same speed and calorific value by 1,66,000 times by acceleration.   Application-specific bearings (80) Thrust bearings (80a) are provided for safe operation, and the combined combustion unit (31Y) high-temperature mercury (1d) in the turbine blade cross section (4D) is injected vertically below the gravitational acceleration in a vacuum. Combined engine with various energy conservation cycles to increase the output of high-pressure turbine and atmospheric pressure at the same speed and calorific value by 1,66,000 times by acceleration.   A bearing (80) for thrust application (80a) is provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) is sprayed vertically downward in the vacuum to increase the gravitational acceleration. Various energy conservation cycle coalescing engines that increase high-pressure turbine drive and atmospheric pressure, same speed, and same calorie calculation output by 166,000 times with the added acceleration.   Application-specific bearing (80) Thrust bearing (80a) is provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32Y) high-temperature mercury (1d) is sprayed vertically downward in the vacuum Various energy conservation cycle coalescing engines that increase high-pressure turbine drive and atmospheric pressure, same speed, and same calorie calculation output by 166,000 times with the added acceleration.   A bearing (80) for thrust application (80a) is provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) is sprayed vertically downward in the vacuum to increase the gravitational acceleration. Combined with various types of energy storage cycle engines that use high-speed turbine drive and atmospheric pressure, same speed, and same calorific value calculation output 166,000 times as much as the added heat, electricity, and cold supply facilities.   Application-specific bearing (80) Thrust bearing (80a) is provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32Y) high-temperature mercury (1d) is sprayed vertically downward in the vacuum Combined with various types of energy storage cycle engines that use high-speed turbine drive and atmospheric pressure, same speed, and same calorific value calculation output 166,000 times as much as the added heat, electricity, and cold supply facilities.   Application-specific bearings (80) Thrust bearings (80a) are provided for safe operation, and the combined combustion section (31X) high-temperature mercury (1d) on the turbine blade cross section (4D) is vertically below the gravity acceleration added in the vacuum. Accelerated high-pressure turbine drive and atmospheric pressure, same speed, same calorific value calculation output 166,000 times various energy storage cycle coalescing engine to make various heat, electricity and cold supply facilities.   Application-specific bearings (80) Thrust bearings (80a) are provided for safe operation, and the combined combustion unit (31Y) high-temperature mercury (1d) in the turbine blade cross section (4D) is injected vertically below the gravitational acceleration in a vacuum. Accelerated high-pressure turbine drive and atmospheric pressure, same speed, same calorific value calculation output 166,000 times various energy storage cycle coalescing engine to make various heat, electricity and cold supply facilities.   Application-specific bearings (80) Thrust bearings (80a) are provided for safe operation, and the combined combustion section (31X) high-temperature mercury (1d) on the turbine blade cross section (4D) is vertically below the gravity acceleration added in the vacuum. Combined with various energy storage cycle engines that make high-speed turbine drive and atmospheric pressure, same speed, same calorie calculation output 166,000 times as large as various kinds of ships.   Application-specific bearings (80) Thrust bearings (80a) are provided for safe operation, and the combined combustion unit (31Y) high-temperature mercury (1d) in the turbine blade cross section (4D) is injected vertically below the gravitational acceleration in a vacuum. Combined with various energy storage cycle engines that make high-speed turbine drive and atmospheric pressure, same speed, same calorie calculation output 166,000 times as large as various kinds of ships.   A bearing (80) for thrust application (80a) is provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) is sprayed vertically downward in the vacuum to increase the gravitational acceleration. Various energy conservation cycle coalescing engines that make high-speed turbine drive and atmospheric pressure same speed same heat quantity calculation output 166,000 times more various ships with added acceleration.   Application-specific bearing (80) Thrust bearing (80a) is provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32Y) high-temperature mercury (1d) is sprayed vertically downward in the vacuum Various energy conservation cycle coalescing engines that make high-speed turbine drive and atmospheric pressure same speed same heat quantity calculation output 166,000 times more various ships with added acceleration.   A bearing (80) for thrust application (80a) is provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) is sprayed vertically downward in the vacuum to increase the gravitational acceleration. Combined engine with various energy conservation cycles to make high-speed turbine drive and atmospheric pressure same speed same heat quantity calculation output 166,000 times various airplanes with added acceleration.   Application-specific bearing (80) Thrust bearing (80a) is provided for safe operation, and the turbine blade cross section (4D) full blade combustion part (32Y) high-temperature mercury (1d) is sprayed vertically downward in the vacuum Combined engine with various energy conservation cycles to make high-speed turbine drive and atmospheric pressure same speed same heat quantity calculation output 166,000 times various airplanes with added acceleration.   Application-specific bearings (80) Thrust bearings (80a) are provided for safe operation, and the combined combustion section (31X) high-temperature mercury (1d) on the turbine blade cross section (4D) is vertically below the gravity acceleration added in the vacuum. Combined with various energy conservation cycle engines that make high-speed turbine drive and atmospheric pressure same speed and same calorific value calculation output 166,000 times various airplanes.   Application-specific bearings (80) Thrust bearings (80a) are provided for safe operation, and the combined combustion unit (31Y) high-temperature mercury (1d) in the turbine blade cross section (4D) is injected vertically below the gravitational acceleration in a vacuum. Combined with various energy conservation cycle engines that make high-speed turbine drive and atmospheric pressure same speed and same calorific value calculation output 166,000 times various airplanes.   Application-specific bearings (80) Thrust bearings (80a) are provided for safe operation, and the combined acceleration of the turbine blade cross section (4D) combustion part (31X) high temperature water (52b) is added vertically under gravity in the jet vacuum Accelerated high-pressure turbine drive and atmospheric pressure, same speed, same calorie calculation output, 910,000 times various energy conservation cycle coalescing engines to make various airplanes.   Application-specific bearing (80) Thrust bearing (80a) is provided for safe operation. Gravity acceleration is added in the vacuum by jetting the combined engine combustion part (31Y) hot water (52b) vertically on the turbine blade cross section (4D) Accelerated high-pressure turbine drive and atmospheric pressure, same speed, same calorie calculation output, 910,000 times various energy conservation cycle coalescing engines to make various airplanes.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation. Gravity acceleration is measured in a vacuum by jetting the whole blade combustion section (32X) hot water (52b) vertically on the turbine blade cross section (4D). Combined engine with various energy storage cycles to make high-speed turbine drive and atmospheric pressure, same speed, same calorie calculation output 910,000 times various airplanes with added acceleration.   A bearing (80) suitable for the application (80a) is provided for safe operation, and the entire blade combustion section (32Y) high-temperature water (52b) in the turbine blade cross section (4D) is sprayed vertically downward in the vacuum to increase the gravitational acceleration. Combined engine with various energy storage cycles to make high-speed turbine drive and atmospheric pressure, same speed, same calorie calculation output 910,000 times various airplanes with added acceleration.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation. Gravity acceleration is measured in a vacuum by jetting the whole blade combustion section (32X) hot water (52b) vertically on the turbine blade cross section (4D). Combined engine with various energy conservation cycles to make high-speed turbine drive and atmospheric pressure same speed same heat quantity calculation output 910,000 times various ships with added acceleration.   A bearing (80) suitable for the application (80a) is provided for safe operation, and the entire blade combustion section (32Y) high-temperature water (52b) in the turbine blade cross section (4D) is sprayed vertically downward in the vacuum to increase the gravitational acceleration. Combined engine with various energy conservation cycles to make high-speed turbine drive and atmospheric pressure same speed same heat quantity calculation output 910,000 times various ships with added acceleration.   Application-specific bearings (80) Thrust bearings (80a) are provided for safe operation, and the combined acceleration of the turbine blade cross section (4D) combustion part (31X) high temperature water (52b) is added vertically under gravity in the jet vacuum Accelerated high-pressure turbine drive and atmospheric pressure, same speed, same calorie calculation output, 910,000 times various energy conservation cycle coalescing engines.   Application-specific bearing (80) Thrust bearing (80a) is provided for safe operation. Gravity acceleration is added in the vacuum by jetting the combined engine combustion part (31Y) hot water (52b) vertically on the turbine blade cross section (4D) Accelerated high-pressure turbine drive and atmospheric pressure, same speed, same calorie calculation output, 910,000 times various energy conservation cycle coalescing engines.   Application-specific bearings (80) Thrust bearings (80a) are provided for safe operation, and the combined acceleration of the turbine blade cross section (4D) combustion part (31X) high temperature water (52b) is added vertically under gravity in the jet vacuum Accelerated high-pressure turbine drive and atmospheric pressure, same speed, same calorie calculation output 910,000 times various energy conservation cycle coalescence engine to make various heat, electricity and cold supply facilities.   Application-specific bearing (80) Thrust bearing (80a) is provided for safe operation. Gravity acceleration is added in the vacuum by jetting the combined engine combustion part (31Y) hot water (52b) vertically on the turbine blade cross section (4D) Accelerated high-pressure turbine drive and atmospheric pressure, same speed, same calorie calculation output 910,000 times various energy conservation cycle coalescence engine to make various heat, electricity and cold supply facilities.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation. Gravity acceleration is measured in a vacuum by jetting the whole blade combustion section (32X) hot water (52b) vertically on the turbine blade cross section (4D). Combined engine with various energy storage cycles to make high-pressure turbine drive and atmospheric pressure same speed and same calorie calculation output 910,000 times with various additional heat, electricity and cold supply facilities.   A bearing (80) suitable for the application (80a) is provided for safe operation, and the entire blade combustion section (32Y) high-temperature water (52b) in the turbine blade cross section (4D) is sprayed vertically downward in the vacuum to increase the gravitational acceleration. Combined engine with various energy storage cycles to make high-pressure turbine drive and atmospheric pressure same speed and same calorie calculation output 910,000 times with various additional heat, electricity and cold supply facilities.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation. Gravity acceleration is measured in a vacuum by jetting the whole blade combustion section (32X) hot water (52b) vertically on the turbine blade cross section (4D). Various energy storage cycle coalescing engines that increase the output of 910,000 times high pressure turbine drive and atmospheric pressure, same speed, and same calorific value with added acceleration.   A bearing (80) suitable for the application (80a) is provided for safe operation, and the entire blade combustion section (32Y) high-temperature water (52b) in the turbine blade cross section (4D) is sprayed vertically downward in the vacuum to increase the gravitational acceleration. Various energy storage cycle coalescing engines that increase the output of 910,000 times high pressure turbine drive and atmospheric pressure, same speed, and same calorific value with added acceleration.   Application-specific bearings (80) Thrust bearings (80a) are provided for safe operation, and the combined acceleration of the turbine blade cross section (4D) combustion part (31X) high temperature water (52b) is added vertically under gravity in the jet vacuum Combined with various energy storage cycle engines that increase the output of high-pressure turbine drive and atmospheric pressure, same speed, and same calorific value by 910,000 times.   Application-specific bearing (80) Thrust bearing (80a) is provided for safe operation. Gravity acceleration is added in the vacuum by jetting the combined engine combustion part (31Y) hot water (52b) vertically on the turbine blade cross section (4D) Combined with various energy storage cycle engines that increase the output of high-pressure turbine drive and atmospheric pressure, same speed, and same calorific value by 910,000 times.   A bearing (80) suitable for the application (80a) is provided for safe operation, and the combined combustion section (31X) of the turbine blade cross section (4D) is heated by the high-temperature mercury (1d) exhaust heat to compress the heat. Combined engine with various energy conservation cycles to increase the theoretical best heat pump (1G) and atmospheric pressure, same speed, same calorie calculation output to 166,000 times.   A bearing (80) suitable for the application (80a) is provided for safe operation, and a combined engine combustion part (31Y) high-temperature mercury (1d) in the turbine blade cross section (4D) heats the intake air by the amount of exhaust heat to recover compression heat Combined engine with various energy conservation cycles to increase the theoretical best heat pump (1G) and atmospheric pressure, same speed, same calorie calculation output to 166,000 times.   A bearing (80) suitable for the application (80a) and a thrust bearing (80a) are provided for safe operation, and the whole blade combustion part (32X) high-temperature mercury (1d) in the turbine blade cross section (4D) is heated by the intake heat to compress the heat. Recovery theory best heat pump (1G) and various energy storage cycle coalescing engines that increase the atmospheric pressure, the same speed, and the same calorie calculation output by 166,000 times.   A bearing (80) thrust bearing (80a) for use is provided for safe operation, and the entire blade combustion section (32Y) high-temperature mercury (1d) in the turbine blade cross section (4D) heats the intake air by the amount of exhaust heat to compress heat Recovery theory best heat pump (1G) and various energy storage cycle coalescing engines that increase the atmospheric pressure, the same speed, and the same calorie calculation output by 166,000 times.   The bearing (80) and thrust bearing (80a) for use are provided for safe operation, and the intake air is heated by the exhaust heat quantity near 230 degrees of all blade combustion section (32X) high temperature mercury (1d) in the turbine blade cross section (4D). Compressed heat recovery theory best heat pump (1G) and various energy storage cycle coalescing engine that makes atmospheric pressure same speed same heat quantity calculation output 166,000 times.   The bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the intake air is heated by the exhaust heat quantity in the vicinity of 230 degrees of all blade combustion part (32Y) high temperature mercury (1d) in the turbine blade cross section (4D). Compressed heat recovery theory best heat pump (1G) and various energy storage cycle coalescing engine that makes atmospheric pressure same speed same heat quantity calculation output 166,000 times.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the intake air is heated by an exhaust heat amount near 230 degrees of the combined engine combustion section (31X) high temperature mercury (1d) of the turbine blade cross section (4D). Compression heat recovery theory Best heat pump (1G) and various energy storage cycle coalescing engine that makes atmospheric pressure same speed same heat quantity calculation output 166,000 times.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the intake air is heated by the exhaust heat quantity near 230 degrees of the combined engine combustion part (31Y) high temperature mercury (1d) of the turbine blade cross section (4D). Compression heat recovery theory Best heat pump (1G) and various energy storage cycle coalescing engine that makes atmospheric pressure same speed same heat quantity calculation output 166,000 times.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the intake air is heated by an exhaust heat amount near 230 degrees of the combined engine combustion section (31X) high temperature mercury (1d) of the turbine blade cross section (4D). Compression heat recovery theory best heat pump (1G), atmospheric pressure, same speed, same calorie calculation output, 166,000 times, various energy storage cycle coalescing engine for various heat, electricity and cold supply facilities.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the intake air is heated by the exhaust heat quantity near 230 degrees of the combined engine combustion part (31Y) high temperature mercury (1d) of the turbine blade cross section (4D). Compression heat recovery theory best heat pump (1G), atmospheric pressure, same speed, same calorie calculation output, 166,000 times, various energy storage cycle coalescing engine for various heat, electricity and cold supply facilities.   The bearing (80) and thrust bearing (80a) for use are provided for safe operation, and the intake air is heated by the exhaust heat quantity near 230 degrees of all blade combustion section (32X) high temperature mercury (1d) in the turbine blade cross section (4D). Compression heat recovery theory best heat pump (1G), atmospheric pressure, same speed, same calorie calculation output, 166,000 times, various energy storage cycle coalescing engine to supply various heat, electricity and cold.   The bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the intake air is heated by the exhaust heat quantity in the vicinity of 230 degrees of all blade combustion part (32Y) high temperature mercury (1d) in the turbine blade cross section (4D). Compression heat recovery theory best heat pump (1G), atmospheric pressure, same speed, same calorie calculation output, 166,000 times, various energy storage cycle coalescing engine to supply various heat, electricity and cold.   The bearing (80) and thrust bearing (80a) for use are provided for safe operation, and the intake air is heated by the exhaust heat quantity near 230 degrees of all blade combustion section (32X) high temperature mercury (1d) in the turbine blade cross section (4D). Compressed heat recovery theory Best heat pump (1G) and Atmospheric pressure, same speed, same calorie calculation output, 166,000 times various energy conservation cycle coalescing engines for various ships.   The bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the intake air is heated by the exhaust heat quantity in the vicinity of 230 degrees of all blade combustion part (32Y) high temperature mercury (1d) in the turbine blade cross section (4D). Compressed heat recovery theory Best heat pump (1G) and Atmospheric pressure, same speed, same calorie calculation output, 166,000 times various energy conservation cycle coalescing engines for various ships.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the intake air is heated by an exhaust heat amount near 230 degrees of the combined engine combustion section (31X) high temperature mercury (1d) of the turbine blade cross section (4D). Compression heat recovery theory Best heat pump (1G) and various energy storage cycle coalescing engines to make various ships 166,000 times the atmospheric pressure same speed same heat quantity calculation output.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the intake air is heated by the exhaust heat quantity near 230 degrees of the combined engine combustion part (31Y) high temperature mercury (1d) of the turbine blade cross section (4D). Compression heat recovery theory Best heat pump (1G) and various energy storage cycle coalescing engines to make various ships 166,000 times the atmospheric pressure same speed same heat quantity calculation output.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the intake air is heated by an exhaust heat amount near 230 degrees of the combined engine combustion section (31X) high temperature mercury (1d) of the turbine blade cross section (4D). Compressed heat recovery theory Best heat pump (1G) and atmospheric pressure, same speed, same calorie calculation output, 1656,000 times, various types of energy storage cycle coalescing engines.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the intake air is heated by the exhaust heat quantity near 230 degrees of the combined engine combustion part (31Y) high temperature mercury (1d) of the turbine blade cross section (4D). Compressed heat recovery theory Best heat pump (1G) and atmospheric pressure, same speed, same calorie calculation output, 1656,000 times, various types of energy storage cycle coalescing engines.   The bearing (80) and thrust bearing (80a) for use are provided for safe operation, and the intake air is heated by the exhaust heat quantity near 230 degrees of all blade combustion section (32X) high temperature mercury (1d) in the turbine blade cross section (4D). Compression heat recovery theory The best heat pump (1G) and various energy storage cycle coalescing engines that make various airplanes with the same atmospheric pressure and speed and calorie output 16656,000 times.   The bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and the intake air is heated by the exhaust heat quantity in the vicinity of 230 degrees of all blade combustion part (32Y) high temperature mercury (1d) in the turbine blade cross section (4D). Compression heat recovery theory The best heat pump (1G) and various energy storage cycle coalescing engines that make various airplanes with the same atmospheric pressure and speed and calorie output 16656,000 times.   A bearing (80) suitable for the application (80a) is provided for safe operation, and the combined combustion section (31X) of the turbine blade cross section (4D) is heated by the high-temperature mercury (1d) exhaust heat to compress the heat. Theoretical best heat pump (1G) and the atmospheric pressure, the same speed, the same calorific value calculation output, 166,000 times the various energy storage cycle coalescing engine to supply various heat, electricity and cold.   A bearing (80) suitable for the application (80a) is provided for safe operation, and a combined engine combustion part (31Y) high-temperature mercury (1d) in the turbine blade cross section (4D) heats the intake air by the amount of exhaust heat to recover compression heat Theoretical best heat pump (1G) and the atmospheric pressure, the same speed, the same calorific value calculation output, 166,000 times the various energy storage cycle coalescing engine to supply various heat, electricity and cold.   A bearing (80) suitable for the application (80a) and a thrust bearing (80a) are provided for safe operation, and the whole blade combustion part (32X) high-temperature mercury (1d) in the turbine blade cross section (4D) is heated by the intake heat to compress the heat. Recovery theory best heat pump (1G), atmospheric pressure, same speed, same calorie calculation output, 166,000 times, various energy storage cycle coalescing engine to supply various heat, electricity and cold.   A bearing (80) thrust bearing (80a) for use is provided for safe operation, and the entire blade combustion section (32Y) high-temperature mercury (1d) in the turbine blade cross section (4D) heats the intake air by the amount of exhaust heat to compress heat Recovery theory best heat pump (1G), atmospheric pressure, same speed, same calorie calculation output, 166,000 times, various energy storage cycle coalescing engine to supply various heat, electricity and cold.   A bearing (80) suitable for the application (80a) and a thrust bearing (80a) are provided for safe operation, and the whole blade combustion part (32X) high-temperature mercury (1d) in the turbine blade cross section (4D) is heated by the intake heat to compress the heat. Recovery theory best heat pump (1G) and atmospheric pressure, same speed, same calorific value calculation output 166,000 times various energy conservation cycle coalescing engines for various ships.   A bearing (80) thrust bearing (80a) for use is provided for safe operation, and the entire blade combustion section (32Y) high-temperature mercury (1d) in the turbine blade cross section (4D) heats the intake air by the amount of exhaust heat to compress heat Recovery theory best heat pump (1G) and atmospheric pressure, same speed, same calorific value calculation output 166,000 times various energy conservation cycle coalescing engines for various ships.   A bearing (80) suitable for the application (80a) is provided for safe operation, and the combined combustion section (31X) of the turbine blade cross section (4D) is heated by the high-temperature mercury (1d) exhaust heat to compress the heat. Theoretical best heat pump (1G) and various energy storage cycle coalescing engines that make various ships 166,000 times the atmospheric pressure, the same speed, and the same calorie calculation output.   A bearing (80) suitable for the application (80a) is provided for safe operation, and a combined engine combustion part (31Y) high-temperature mercury (1d) in the turbine blade cross section (4D) heats the intake air by the amount of exhaust heat to recover compression heat Theoretical best heat pump (1G) and various energy storage cycle coalescing engines that make various ships 166,000 times the atmospheric pressure, the same speed, and the same calorie calculation output.   A bearing (80) suitable for the application (80a) is provided for safe operation, and the combined combustion section (31X) of the turbine blade cross section (4D) is heated by the high-temperature mercury (1d) exhaust heat to compress the heat. Theoretical best heat pump (1G) and the atmospheric pressure, the same speed, the same calorie calculation output, 166,000 times the various energy conservation cycle coalescing engines that make various airplanes.   A bearing (80) suitable for the application (80a) is provided for safe operation, and a combined engine combustion part (31Y) high-temperature mercury (1d) in the turbine blade cross section (4D) heats the intake air by the amount of exhaust heat to recover compression heat Theoretical best heat pump (1G) and the atmospheric pressure, the same speed, the same calorie calculation output, 166,000 times the various energy conservation cycle coalescing engines that make various airplanes.   A bearing (80) suitable for the application (80a) and a thrust bearing (80a) are provided for safe operation, and the whole blade combustion part (32X) high-temperature mercury (1d) in the turbine blade cross section (4D) is heated by the intake heat to compress the heat. Recovery theory best heat pump (1G), atmospheric pressure, same speed, same calorie calculation output, 166,000 times more various energy storage cycle coalescing engine to make various airplanes.   A bearing (80) thrust bearing (80a) for use is provided for safe operation, and the entire blade combustion section (32Y) high-temperature mercury (1d) in the turbine blade cross section (4D) heats the intake air by the amount of exhaust heat to compress heat Recovery theory best heat pump (1G), atmospheric pressure, same speed, same calorie calculation output, 166,000 times more various energy storage cycle coalescing engine to make various airplanes.   A bearing (80) for thrust application (80a) is provided for safe operation, and a cold heat recovery means (3C) is provided for the turbine blade (8c) of the entire blade of the turbine blade cross section (4D) to recover the cold heat. Combined with various energy storage cycle engines that output 166,000 times the atmospheric pressure and speed and calorific value.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and a cooling / heat recovery means (3C) is provided on the turbine blade (8c) of the turbine blade cross section (4D) of the turbine blade cross section (4D) for heating and Combined engine with various energy storage cycles to increase the atmospheric pressure, velocity, and calorie calculation output by 166,000 times.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and a cold heat recovery means (3C) is provided on the turbine blade (8c) of the whole rotor blade gas turbine of the turbine blade cross section (4D) to provide alcohol (1C ) Various energy storage cycle coalescing engines that collect cold heat and output atmospheric pressure at the same speed and calorific value by 166,000 times.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and a cold heat recovery means (3C) is provided on the turbine blade (8c) of the whole rotor blade gas turbine of the turbine blade cross section (4D) to provide alcohol (1C ) Various energy storage cycle coalescing engines that increase heating and atmospheric pressure at the same speed and heat output by 166,000 times.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and a cold heat recovery means (3C) is provided on the turbine blade (8c) of the whole rotor blade gas turbine of the turbine blade cross section (4D) to provide alcohol (1C ) Various energy conservation cycle coalescing engines that increase the recovery output and the atmospheric pressure, the same speed, and the same calorie calculation output by 166,000 times.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and a cold heat recovery means (3C) is provided on the turbine blade (8c) of the whole rotor blade gas turbine of the turbine blade cross section (4D) to provide alcohol (1C ) Etc. Various energy storage cycle coalescing engines that increase the heating output, etc., and increase the atmospheric pressure, the same speed, and the same calorie calculation output by 166,000 times.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and a cold heat recovery means (3C) is provided on the turbine blade (8c) of the whole rotor blade gas turbine of the turbine blade cross section (4D) to provide alcohol (1C ) Collecting cold heat, etc. Various energy storage cycle coalescing engines that prevent sticking of dry ice, moisture, etc. and increase the atmospheric pressure, the same speed, and the same calorie calculation output by 166,000 times.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and a cold heat recovery means (3C) is provided on the turbine blade (8c) of the whole rotor blade gas turbine of the turbine blade cross section (4D) to provide alcohol (1C ), Etc. Various energy storage cycle coalescence engines that prevent the adhesion of heated dry ice, moisture, etc. and increase the atmospheric pressure, the same speed, and the same calorie calculation output by 166,000 times.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and a heating high temperature means (3B) is provided on the turbine blade (8c) of the turbine blade cross section (4D) of the turbine blade cross section (4D) to Combined engine with various energy storage cycles to increase the atmospheric pressure, velocity, and calorie calculation output by 166,000 times.   A bearing (80) thrust bearing (80a) corresponding to the application is provided for safe operation, and a water repellent action (3A) is provided on the turbine blade (8c) of the turbine blade cross section (4D) of the turbine blade cross section (4D). Various energy storage cycle coalescing engines that increase the atmospheric pressure, the same speed, and the same calorie calculation output by 166,000 times.   Application-specific bearing (80) Thrust bearing (80a) is provided for safe operation, and heating high temperature means (3B) is provided on the turbine blade (8c) of the turbine blade cross section (4D) of the turbine blade cross section (4D). Various energy storage cycle coalescing engine that makes rolling contact rotation output and atmospheric pressure same speed same heat same calorie calculation output 166,000 times.   Provided bearing (80) for application and thrust bearing (80a) for safe operation and water repellent action by providing water repellent action (3A) to turbine blade (8c) of turbine blade cross section (4D) Various energy storage cycle coalescing engine that makes rolling contact rotation output and atmospheric pressure same speed same heat same calorie calculation output 166,000 times.   A bearing (80) thrust bearing (80a) for use is provided for safe operation, and the exhaust blade saturation temperature of the turbine blade cross section (4D) near the exhaust saturation temperature of 30 degrees is reduced by cooling (52e) or at the same pressure at the same atmospheric pressure. Various energy storage cycle coalescing engine with calorific value calculation output of 166,000 times.   A bearing (80) thrust bearing (80a) for the application is provided to ensure safe operation, and the exhaust blade saturation temperature of the turbine blade cross section (4D) near the exhaust saturation temperature of 30 degrees is cooled (52e) to prevent seawater temperature rise. Combined with various energy storage cycle engines that output 166,000 times the atmospheric pressure and speed and calorific value.   Use of bearing (80) thrust bearing (80a) for application and safe operation, recover and store alcohol cold heat (52e) in all blade gas turbine with turbine blade cross section (4D) Various energy conservation cycle coalescing engines that increase the calculation output by 166,000 times.   The bearings (80) and thrust bearings (80a) for use are provided for safe operation, and the compressed air cold heat (52e) is recovered and stored in an all blade gas turbine with a turbine blade cross section (4D). Various energy conservation cycle coalescing engines that increase calorie calculation output by 166,000 times.   Use bearing (80) Thrust bearing (80a) for safe operation, and collect and store ice-cooled heat (52e) in all blade gas turbine with turbine blade cross section (4D) for use and atmospheric pressure at the same speed and heat Various energy conservation cycle coalescing engines that increase the calculation output by 166,000 times.   Various types of bearings (80) and thrust bearings (80a) suitable for applications are used for safe operation, and cold heat (52e) is recovered and stored in all rotor blade gas turbines with a turbine blade cross section (4D) and used as various refrigeration equipment. Energy conservation cycle coalescence engine.   The bearings (80) and thrust bearings (80a) for use are provided for safe operation, and cold heat (52e) is recovered and stored in a full blade gas turbine with a turbine blade cross section (4D) for use as various refrigeration equipment. Combined engine with various energy storage cycles to increase the atmospheric pressure, velocity, and calorie calculation output by 166,000 times.   A bearing (80) and a thrust bearing (80a) corresponding to the application are provided for safe operation, and cold heat (52e) is recovered and stored in an all blade gas turbine with a turbine blade cross section (4D) for use as various cooling equipment. Combined engine with various energy storage cycles to increase the atmospheric pressure, velocity, and calorie calculation output by 166,000 times.   The bearings (80) and thrust bearings (80a) suitable for the application are provided for safe operation, and the cold blade (52e) is recovered and stored in a turbine blade cross section (4D) full blade gas turbine for use as various cooling equipment. Combined engine with various energy storage cycles to increase the atmospheric pressure, velocity, and calorie calculation output by 166,000 times.   The bearings (80) and thrust bearings (80a) for use are provided for safe operation, and cold heat (52e) is recovered and stored in a full blade gas turbine with a turbine blade cross section (4D) for use as various ice making equipment. Combined engine with various energy storage cycles to increase the atmospheric pressure, velocity, and calorie calculation output by 166,000 times.   Use bearings (80) and thrust bearings (80a) for application to ensure safe operation, collect and store cold heat (52e) in a turbine blade cross section (4D) full blade gas turbine, and use as various compressed air cold piping buildings Combined with various energy storage cycle engines that output 166,000 times the atmospheric pressure and speed and calorific value.   Provided bearing (80) thrust bearing (80a) for application and safe operation, supply of all turbine blade gas turbine exhaust of turbine blade cross section (4D) as combustion gas dissolved water (52g) such as CO2 to the seabed, etc. Various energy storage cycle coalescing engine with the same speed and calorific value calculation output of 166,000 times.   A bearing (80) thrust bearing (80a) for use is provided for safe operation, and all rotor blade gas turbine exhaust with a turbine blade cross section (4D) is supplied to the seabed as combustion gas dissolved water (52 g) such as CO2 Various energy conservation cycle coalescing engines that increase the output of 165,000 times the growth and atmospheric pressure and speed and calorific value.   A bearing (80) thrust bearing (80a) for use is provided for safe operation, and all rotor blade gas turbine exhaust with a turbine blade cross section (4D) is supplied to the seabed as combustion gas dissolved water (52g) such as CO2 Various energy storage cycle coalescing engines that increase the output and the atmospheric pressure, the same speed, and the same calorie calculation output 166,000 times.   Providing bearings for use (80) Thrust bearings (80a) for safe operation, supplying all rotor blade gas turbine exhaust with turbine blade cross section (4D) as combustion gas dissolved water (52g) such as CO2 to the sea floor etc. Various energy conservation cycle coalescing engines that increase the number of planktons to multiply and calculate the atmospheric pressure at the same speed and calorific value by 166,000 times.   A dedicated bearing (80) thrust bearing (80a) is provided for safe operation, and dedicated to the rotational output of the turbine blade cross section (4E), the excess heat is recovered and stored at various temperatures (52d) of 300 degrees or less for use and large Combined engine with various energy storage cycles to increase the atmospheric pressure, velocity, and calorie calculation output by 166,000 times.   Provided bearings (80) for application and thrust bearings (80a) for safe operation, and dedicated to rotating output of turbine blade cross section (4E), recovering and storing surplus heat with various temperatures (52d) of 300 degrees or less, and various heating facilities Various energy storage cycle coalescing engines that can be used as equipment and have an output of 166,000 times the atmospheric pressure, speed, and calorific value.   A bearing (80) and thrust bearing (80a) corresponding to the application are provided for safe operation, and for the rotational output of the turbine blade cross section (4E), the excess heat is recovered and stored at various temperatures (52d) of 300 degrees or less, and various cooking facilities Various energy storage cycle coalescing engines that can be used as equipment and have an output of 166,000 times the atmospheric pressure, speed, and calorific value.   A bearing (80) suitable for the application and a thrust bearing (80a) are provided for safe operation, and for the rotational output of the turbine blade cross section (4E), the excess heat is recovered and stored at various temperatures (52d) of 300 degrees or less, and various hot water facilities Various energy storage cycle coalescing engines that can be used as equipment and have an output of 166,000 times the atmospheric pressure, speed, and calorific value.   A bearing (80) and thrust bearing (80a) corresponding to the application are provided for safe operation, and for the rotational output of the turbine blade cross section (4E), the excess heat is recovered and stored at various temperatures (52d) of 300 degrees or less, and various dishwashers Various energy storage cycle coalescing engines that can be used as a kind or output at an atmospheric pressure and speed and calorie calculation output of 166,000 times.   A bearing (80) and a thrust bearing (80a) corresponding to the application are provided for safe operation, and for the rotation output of the turbine blade cross section (4E), the excess heat is recovered and stored at various temperatures (52d) of 300 degrees or less, and various washing drying Various energy conservation cycle coalescing engines that can be used as machinery and have an output of 166,000 times the atmospheric pressure, speed, and calorific value.   A bearing (80) and thrust bearing (80a) for use are provided for safe operation, and for the rotational output of the turbine blade cross section (4E), the excess heat is recovered and stored at various temperatures (52d) of 300 degrees or less, and various water temperatures Various energy storage cycle coalescing engines that are used as piping buildings and have an atmospheric pressure, same speed, and same calorie calculation output of 166,000 times.   A bearing (80) thrust bearing (80a) for use is provided for safe operation, and for the rotational output of the turbine blade cross section (4E), excess heat is recovered and stored at various temperatures (52d) of 300 degrees or less, and various types of seawater, etc. Various energy conservation cycle coalescing engines that use water as distilled water and increase the atmospheric pressure, speed, and calorie calculation output by 166,000 times.   A bearing (80) thrust bearing (80a) for use is provided for safe operation, and for the rotational output of the turbine blade cross section (4E), excess heat is recovered and stored at various temperatures (52d) of 300 degrees or less, and various types of seawater, etc. Various energy storage cycle coalescing engines that use water as distilled water or salt, and that output atmospheric pressure at the same speed and calorific value by 166,000 times.   The turbine blade cross section (4D) application-compatible bearing (80) thrust bearing (80a) is provided for safe operation, the compressed air heat (28b) is recovered by the intake air (28a), and the heat is compressed by the heat pump (1G). Various energy storage cycle coalescing engine that makes recovery and atmospheric pressure same speed same heat quantity calculation output 166,000 times.   The turbine blade cross section (4D) application-compatible bearing (80) thrust bearing (80a) is provided for safe operation, and the mercury exhaust heat quantity (5A) + compressed air heat quantity (28b) is recovered by the intake air (28a) Various energy storage cycle coalescing engines that use a pump (1G) to recover compression heat and output atmospheric pressure at the same speed and calorific value by 166,000 times.   A bearing (80) thrust bearing (80a) corresponding to the application of the turbine blade cross section (4D) is provided for safe operation, the amount of compressed air heat (28b) is recovered by intake air (28a), and compressed by a heat pump (1G) 500 Various energy storage cycle coalescing engines that make heat recovery and atmospheric pressure same speed same heat quantity calculation output 166,000 times as ~ 1000 degrees.   The turbine blade cross section (4D) application-compatible bearing (80) thrust bearing (80a) is provided for safe operation, and the mercury exhaust heat quantity (5A) + compressed air heat quantity (28b) is recovered by the intake air (28a) Various energy storage cycle coalescing engines that make heat recovery and atmospheric pressure same speed same heat quantity calculation output 166,000 times by pump (1G) compression 500-1000 degrees.   A bearing (80) thrust bearing (80a) corresponding to the application of the turbine blade cross section (4D) is provided for safe operation, the amount of compressed air heat (28b) is recovered by intake air (28a), and compressed by a heat pump (1G) 500 Various energy conservation cycle coalescing engines that recover heat by ˜1000 degrees, etc. to drive all rotor blade water turbines and output atmospheric pressure at the same speed and calorific value by 166,000 times.   A bearing (80) thrust bearing (80a) corresponding to the application of the turbine blade cross section (4D) is provided for safe operation, the amount of compressed air heat (28b) is recovered by intake air (28a), and compressed by a heat pump (1G) 500 Various energy storage cycle coalescing engines that recover heat by ˜1000 degrees, etc. to drive all moving blade mercury turbines and output atmospheric pressure at the same speed and calorific value by 166,000 times.   A bearing (80) thrust bearing (80a) corresponding to the application of the turbine blade cross section (4D) is provided for safe operation, the amount of compressed air heat (28b) is recovered by intake air (28a), and compressed by a heat pump (1G) 500 Various energy storage cycle coalescing engines that recover heat by ˜1000 degrees, etc. to drive all rotor blade gas turbines and output atmospheric pressure at the same speed and calorific value by 166,000 times.   A turbine blade cross section (4D) application-compatible bearing (80) Thrust bearing (80a) is provided for safe operation, such as the flying wing (38b) and flying tail (38c), all the parts that become hot at the time of return to the earth at the flying speed Combined with various energy storage cycles that make water (52a) pipes made lighter and higher in pressure with carbon fiber, etc., and make high-pressure lightweight containers 166.5 times heat recovery and atmospheric pressure, same speed, same calorie calculation output organ.   A turbine blade cross section (4D) application-compatible bearing (80) Thrust bearing (80a) is provided for safe operation, such as the flying wing (38b) and flying tail (38c), all the parts that become hot at the time of return to the earth at the flying speed Various energy storage cycles that make the high-pressure light weight container 16500 times the heat recovery and atmospheric pressure, same speed, and same calorific value output by piping the superheated steam (50) pipe that has been reduced in weight to high pressure with carbon fiber, etc. Combined organization.   A turbine blade cross section (4D) application-compatible bearing (80) Thrust bearing (80a) is provided for safe operation, such as the flying wing (38b) and flying tail (38c), all the parts that become hot at the time of return to the earth at the flying speed Various energy storage cycles that make a high-pressure light weight container 166.5 times as much as constituent heat recovery and atmospheric pressure, same speed, and same calorific value by piping a high-temperature mercury (1d) pipe that has been reduced in weight to high pressure with carbon fiber, etc. Combined organization.   A turbine blade cross section (4D) application-compatible bearing (80) Thrust bearing (80a) is provided for safe operation, such as the flying wing (38b) and flying tail (38c), all the parts that become hot at the time of return to the earth at the flying speed Various energy storage cycle coalescing engines that make combustion gas pipes made lighter and higher in pressure with carbon fiber, etc., and make the high-pressure and light-weight container 166.5 times the heat recovery and atmospheric pressure, same-speed, and same-heat calculation output.   A turbine blade cross section (4D) application-compatible bearing (80) Thrust bearing (80a) is provided for safe operation, such as the flying wing (38b) and flying tail (38c), all the parts that become hot at the time of return to the earth at the flying speed Combined with various energy storage cycles that make water (52a) pipes made lighter and higher in pressure with carbon nanotubes, etc., and make high-pressure lightweight containers 166.5 times heat recovery and atmospheric pressure, same speed, same calorie calculation output organ.   A turbine blade cross section (4D) application-compatible bearing (80) Thrust bearing (80a) is provided for safe operation, such as the flying wing (38b) and flying tail (38c), all the parts that become hot at the time of return to the earth at the flying speed , Various energy storage cycles that make a high-pressure light weight container 16500 times more heat recovery and atmospheric pressure, same speed, and same calorific value calculation by piping a superheated steam (50) pipe that has been reduced in weight to high pressure with carbon nanotubes, etc. Combined organization.   A turbine blade cross section (4D) application-compatible bearing (80) Thrust bearing (80a) is provided for safe operation, such as the flying wing (38b) and flying tail (38c), all the parts that become hot at the time of return to the earth at the flying speed , Various energy storage cycles that make high-pressure and light weight containers composed of heat-reduced and atmospheric pressure, same-velocity, same-heat-calculation output 166,000 times by piping high-temperature mercury (1d) tubes that have been reduced in weight to high pressure with carbon nanotubes, etc. Combined organization.   The turbine blade cross section (4D) application-compatible bearing (80) thrust bearing (80a) is provided for safe operation, and all the parts such as the flying wing (38b) and the flying tail (38c) that become hot when returning to the earth at the flight speed 0 In addition, various energy storage cycle coalescence engines that make combustion gas pipes lightened with carbon nanotubes, etc., piping a high-pressure light-weight container, and make up the heat recovery and atmospheric pressure, same-speed, and same-heat-calculation output 166,000 times .   The turbine blade cross section (4D) application-compatible bearing (80) thrust bearing (80a) is provided for safe operation, the combustion gas (49) is recovered by the intake air (28a), and is compressed by the heat pump (1G). Various energy conservation cycle coalescing engines that recover heat by ˜1000 degrees, etc. to drive all rotor blade water turbines and output atmospheric pressure at the same speed and calorific value by 166,000 times.   The turbine blade cross section (4D) application-compatible bearing (80) thrust bearing (80a) is provided for safe operation, the combustion gas (49) is recovered by the intake air (28a), and is compressed by the heat pump (1G). Various energy storage cycle coalescing engines that recover heat by ˜1000 degrees, etc. to drive all moving blade mercury turbines and output atmospheric pressure at the same speed and calorific value by 166,000 times.   The turbine blade cross section (4D) application-compatible bearing (80) thrust bearing (80a) is provided for safe operation, the combustion gas (49) is recovered by the intake air (28a), and is compressed by the heat pump (1G). Various energy storage cycle coalescing engines that recover heat by ˜1000 degrees, etc. to drive all rotor blade gas turbines and output atmospheric pressure at the same speed and calorific value by 166,000 times.   The turbine blade cross section (4D) application-compatible bearing (80) thrust bearing (80a) is provided for safe operation, the combustion gas (49) is recovered by the intake air (28a), and is compressed by the heat pump (1G). Various energy storage cycle coalescing engines that recover heat by ˜1000 degrees, etc. to drive the coalesced engine injection part (79K) and output the atmospheric pressure, the same speed, and the same calorific value by 166,000 times.   The turbine blade cross section (4D) application-compatible bearing (80) thrust bearing (80a) is provided for safe operation, the combustion gas (49) is recovered by the intake air (28a), and is compressed by the heat pump (1G). Various energy conservation cycle coalescing engines that recover heat by ˜1000 degrees, etc. to drive the water jet (79M) all-blade mercury turbine and output the atmospheric pressure at the same speed and the same calorific value.   A bearing (80) thrust bearing (80a) corresponding to the application of the turbine blade cross section (4D) is provided for safe operation, the amount of compressed air heat (28b) is recovered by intake air (28a), and compressed by a heat pump (1G) 500 Various energy storage cycle coalescing engines that recover heat by ˜1000 degrees, etc. to drive the coalesced engine injection part (79K) and output the atmospheric pressure, the same speed, and the same calorific value by 166,000 times.   A bearing (80) thrust bearing (80a) corresponding to the application of the turbine blade cross section (4D) is provided for safe operation, the amount of compressed air heat (28b) is recovered by intake air (28a), and compressed by a heat pump (1G) 500 Various energy conservation cycle coalescing engines that recover heat by ˜1000 degrees, etc. to drive the water jet (79M) and calculate the atmospheric pressure, the same speed, and the same calorific value.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, providing a full blade combustion section (32X) vertical all blade gas turbine (8A) with a turbine blade cross section (4D) Various energy storage cycle coalescence engine to drive.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), a turbine blade cross section (4D) full blade combustion part (32Y) vertical all blade gas turbine (8A) is provided. Various energy storage cycle coalescence engine to drive.   Aiming at a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) corresponding to the application, a combined turbine combustion section (31Y) full blade impeller gas turbine (8a) with a turbine blade cross section (4D) is provided and driven Various energy conservation cycle coalescence engine.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a) and driving by providing a combined engine combustion section (31X) full blade impeller gas turbine (8a) with a turbine blade cross section (4D) Various energy conservation cycle coalescence engine.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) suitable for applications, recovering cold heat to the turbine blade cross section (4D) all blade combustion section (32X) vertical all blade gas turbine (8A) Various energy storage cycle coalescing engines that are driven by means (3C).   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, recovering cold heat to the all blade combustion part (32Y) vertical all blade gas turbine (8A) of the turbine blade cross section (4D) Various energy storage cycle coalescing engines that are driven by means (3C).   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) corresponding to the application, a cold heat recovery means (8a) is connected to the combined engine combustion section (31Y) full blade impeller gas turbine (8a) of the turbine blade cross section (4D). 3C) Various energy storage cycle coalescing engines that are driven and provided.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, and a cold heat recovery means (8a) in the combined engine combustion section (31X) full blade impeller gas turbine (8a) of the turbine blade cross section (4D) 3C) Various energy storage cycle coalescing engines that are driven and provided.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) suitable for applications, recovering cold heat to the turbine blade cross section (4D) all blade combustion section (32X) vertical all blade gas turbine (8A) Various energy storage cycle coalescing engines that are driven by providing a vessel (103).   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, recovering cold heat to the all blade combustion part (32Y) vertical all blade gas turbine (8A) of the turbine blade cross section (4D) Various energy storage cycle coalescing engines that are driven by providing a vessel (103).   Aiming for up to 1.65 million times power with a bearing (80) thrust bearing (80a) for application, bearing (80) to the combined engine combustion section (31X) full blade impeller gas turbine (8a) of the turbine blade cross section (4D) Various energy storage cycle coalescing engines that are driven by a thrust bearing (80a) and a cold energy recovery unit (103).   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, a cold heat recovery device (8a) with a combined engine combustion section (31Y) full blade impeller gas turbine (8a) with a turbine blade cross section (4D) 103) Various energy storage cycle coalescing engines that are driven and provided.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) suitable for applications, recovering cold heat to the turbine blade cross section (4D) all blade combustion section (32X) vertical all blade gas turbine (8A) Various energy storage cycle coalescing engines that are driven by the devices (103) and (103).   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, recovering cold heat to the all blade combustion part (32Y) vertical all blade gas turbine (8A) of the turbine blade cross section (4D) Various energy storage cycle coalescing engines that are driven by the devices (103) and (103).   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, a cold heat recovery unit (8a) is connected to the combined engine combustion section (31X) full blade impeller gas turbine (8a) of the turbine blade cross section (4D). 103) Various energy storage cycle coalescing engines driven by providing (103).   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, a cold heat recovery device (8a) with a combined engine combustion section (31Y) full blade impeller gas turbine (8a) with a turbine blade cross section (4D) 103) Various energy storage cycle coalescing engines driven by providing (103).   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, and a combined turbine combustion section (31X) full blade impeller gas turbine (8a) with a turbine blade cross section (4D) around 150 degrees Celsius Various energy storage cycle coalescence engine driven by 24-300 MPa combustion gas (49).   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), the combined engine combustion section (31Y) full blade impeller gas turbine (8a) with a turbine blade cross section (4D) is around 150 degrees Celsius Various energy storage cycle coalescence engine driven by 24-300 MPa combustion gas (49).   Aiming for up to 1.65 million times work with a bearing (80) thrust bearing (80a) for the application, and a full blade combustion section (32X) vertical all blade gas turbine (8A) with a turbine blade cross section (4D) 150 degrees Celsius Various energy storage cycle coalescing engines driven by 24-300 MPa combustion gas (49).   Aiming for up to 1.65 million times work with a bearing (80) thrust bearing (80a) for the application, a turbine blade cross section (4D) full blade combustion section (32Y) vertical all blade gas turbine (8A) 150 ° C Various energy storage cycle coalescing engines driven by 24-300 MPa combustion gas (49).   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, the combined engine combustion section (31X) full blade impeller gas turbine (8a) with a turbine blade cross section (4D) is around 200 degrees Celsius. Various energy storage cycle coalescence engine driven by 24-300 MPa combustion gas (49).   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, a combined turbine combustion section (31Y) full blade impeller gas turbine (8a) with a turbine blade cross section (4D) around 200 degrees Celsius Various energy storage cycle coalescence engine driven by 24-300 MPa combustion gas (49).   Aiming for a maximum of 1.65 million times work with a bearing (80) thrust bearing (80a) for the application, a turbine blade cross section (4D) full blade combustion section (32X) vertical all blade gas turbine (8A) 200 degrees Celsius Various energy storage cycle coalescing engines driven by 24-300 MPa combustion gas (49).   Aiming for a maximum of 1.65 million times work with a bearing (80) thrust bearing (80a) for the application, a turbine blade cross section (4D) all blade combustion part (32Y) vertical all blade gas turbine (8A) 200 degrees Celsius Various energy storage cycle coalescing engines driven by 24-300 MPa combustion gas (49).   Aiming at a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, a turbine blade cross section (4D) full blade combustion part (32X) vertical all blade gas turbine (8A) 300 degrees Celsius Various energy storage cycle coalescing engines driven by 24-300 MPa combustion gas (49).   Aiming at a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) suitable for applications, a turbine blade cross section (4D) full blade combustion part (32Y) vertical all blade gas turbine (8A) 300 degrees Celsius Various energy storage cycle coalescing engines driven by 24-300 MPa combustion gas (49).   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, a combined turbine combustion section (31X) full blade impeller gas turbine (8a) with a turbine blade cross section (4D) around 300 degrees Celsius Various energy storage cycle coalescence engine driven by 24-300 MPa combustion gas (49).   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, a combined turbine combustion section (31Y) full blade impeller gas turbine (8a) with a turbine blade cross section (4D) around 300 degrees Celsius Various energy storage cycle coalescence engine driven by 24-300 MPa combustion gas (49).   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), the combined engine combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven by a high-pressure turbine below the critical temperature. Various energy storage cycle coalescing engines that reduce heat consumption to approximately 1/72.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, a high-pressure turbine drive is performed with the combined combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) below the critical temperature. Various energy storage cycle coalescing engines that reduce heat consumption to approximately 1/72.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) suitable for applications, high-pressure turbine drive of the turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) below the critical temperature Various energy storage cycle coalescing engines that reduce the amount of heat consumed to approximately 1/72.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) suitable for applications, high-pressure turbine drive of turbine blade cross section (4D) full blade combustion part (32Y) high temperature mercury (1d) below critical temperature Various energy storage cycle coalescing engines that reduce the amount of heat consumed to approximately 1/72.   A high-pressure turbine with an application-ready bearing (80) thrust bearing (80a), aiming for a maximum work rate of 1.65 million times, turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) below 1000 degrees Celsius Various energy storage cycle coalescing engines that drive to reduce heat consumption to approximately 1/72.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) aiming for a maximum work of 1.65 million times, a turbine blade cross section (4D) full blade combustion part (32Y) high-temperature mercury (1d) high pressure turbine below 1000 degrees Celsius Various energy storage cycle coalescing engines that drive to reduce heat consumption to approximately 1/72.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), high-pressure turbine drive with a combined combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D) at 1000 degrees Celsius or less Various energy storage cycle coalescing engines that reduce the amount of heat consumed to approximately 1/72.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), high-pressure turbine drive with a combined combustion section (31Y) high-temperature mercury (1d) in the turbine blade cross section (4D) at 1000 degrees Celsius or less Various energy storage cycle coalescing engines that reduce the amount of heat consumed to approximately 1/72.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, a high-pressure turbine drive with a combined engine combustion section (31X) high-temperature mercury (1d) in the turbine blade cross section (4D) at 800 degrees Celsius or less Various energy storage cycle coalescing engines that reduce the amount of heat consumed to approximately 1/72.   The bearing (80) thrust bearing (80a) for the application aims at a maximum work of 1.65 million times, and the combined combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven at a high pressure turbine below 800 degrees Celsius. Various energy storage cycle coalescing engines that reduce the amount of heat consumed to approximately 1/72.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for use, a high-pressure turbine with a turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) at 800 degrees Celsius or less Various energy storage cycle coalescing engines that drive to reduce heat consumption to approximately 1/72.   A high-pressure turbine with an application-ready bearing (80) thrust bearing (80a) with a maximum of 1.65 million times power and a turbine blade cross section (4D) full blade combustion part (32Y) high-temperature mercury (1d) at 800 degrees Celsius or less Various energy storage cycle coalescing engines that drive to reduce heat consumption to approximately 1/72.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, a high-pressure turbine with a turbine blade cross section (4D) full blade combustion part (32X) high temperature mercury (1d) at 600 degrees Celsius or less Various energy storage cycle coalescing engines that drive to reduce heat consumption to approximately 1/72.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for use, a high-pressure turbine with a turbine blade cross section (4D) full blade combustion part (32Y) high-temperature mercury (1d) below 600 degrees Celsius Various energy storage cycle coalescing engines that drive to reduce heat consumption to approximately 1/72.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, a high-pressure turbine drive with a combined engine combustion section (31X) high-temperature mercury (1d) in the turbine blade cross section (4D) at 600 degrees Celsius or less Various energy storage cycle coalescing engines that reduce the amount of heat consumed to approximately 1/72.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), a high-pressure turbine drive with a combined combustion section (31Y) high-temperature mercury (1d) of a turbine blade cross section (4D) at 600 degrees Celsius or less Various energy storage cycle coalescing engines that reduce the amount of heat consumed to approximately 1/72.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, a high-pressure turbine is driven at a temperature below the critical temperature for the combined engine combustion section (31X) high-temperature water (52b) of the turbine blade cross section (4D). Various energy storage cycle coalescing engines that reduce heat consumption to approximately 1/539.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, a high-pressure turbine is driven at a critical temperature or lower with the combined engine combustion section (31Y) high-temperature water (52b) on the turbine blade cross section (4D). Various energy storage cycle coalescing engines that reduce heat consumption to approximately 1/539.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, high-pressure turbine drive of the turbine blade cross section (4D) full blade combustion part (32X) high temperature water (52b) below the critical temperature Various energy storage cycle coalescence engines that reduce the amount of heat consumed to approximately 1/539.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, high-pressure turbine drive of the turbine blade cross section (4D) full blade combustion part (32Y) high temperature water (52b) below the critical temperature Various energy storage cycle coalescence engines that reduce the amount of heat consumed to approximately 1/539.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, and a high-pressure turbine drive with high-temperature turbine (32X) high-temperature water (52b) in the turbine blade cross section (4D). Various energy conservation cycle coalescing engines that reduce the energy to approximately 1/539.   Aiming for a maximum work of 1.65 million times with application-specific bearing (80) thrust bearing (80a) and driving high-pressure turbine with turbine blade cross section (4D) full blade combustion part (32Y) high temperature water (52b) Various energy conservation cycle coalescing engines that reduce the energy to approximately 1/539.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for use, and driving a high-pressure turbine with a combined engine combustion section (31X) high-temperature water (52b) on the turbine blade cross section (4D) to reduce the amount of heat consumed Various energy conservation cycle coalescing engines that make it approximately 1/539.   Aiming for a maximum work of 1.65 million times with the bearing (80) thrust bearing (80a) for the application, and driving the high-pressure turbine with the combined engine combustion section (31Y) high-temperature water (52b) of the turbine blade cross section (4D) to reduce the heat consumption. Various energy conservation cycle coalescing engines that make it approximately 1/539.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), driving the high-pressure turbine with the combined engine combustion section (31X) hot water (52b) on the turbine blade cross section (4D) Various energy storage cycle coalescing engines with a speed output of 1700 times the weight of steam driven by m / s.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), driving the high-pressure turbine with the combined engine combustion section (31Y) high-temperature water (52b) of the turbine blade cross section (4D) Various energy storage cycle coalescing engines with a speed output of 1700 times the weight of steam driven by m / s.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for application, and a high-pressure turbine driven by high-pressure turbine (32X) high-temperature water (52b) in the turbine blade cross section (4D) Various energy storage cycle coalescing engine that makes the same speed output 1700 times kg weight m / sec of steam drive.   Aiming for a maximum work of 1.65 million times with application-specific bearing (80) thrust bearing (80a), high-pressure turbine driven with turbine blade cross section (4D) full blade combustion part (32Y) high temperature water (52b) and atmospheric pressure Various energy storage cycle coalescing engine that makes the same speed output 1700 times kg weight m / sec of steam drive.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, and driving the high-pressure turbine with the turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) Various energy storage cycle coalescing engines with the same speed output, 23,000 times the weight of steam driven by kg weight m / sec.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for application, and a high-pressure turbine driven by a high-pressure mercury (1d) turbine blade combustion section (32D) turbine blade cross section (4D) Various energy storage cycle coalescing engines with the same speed output, 23,000 times the weight of steam driven by kg weight m / sec.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), driving the high-pressure turbine with a combined engine combustion section (31X) high-temperature mercury (1d) on the turbine blade cross section (4D) Various energy storage cycle coalescing engines with a speed output of 23,000 times the weight per kg of steam driven m / sec.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), driving the high-pressure turbine with a combined engine combustion section (31Y) high-temperature mercury (1d) on the turbine blade cross section (4D) Various energy storage cycle coalescing engines with a speed output of 23,000 times the weight per kg of steam driven m / sec.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), driving the high-pressure turbine with a combined engine combustion section (31X) high-temperature mercury (1d) on the turbine blade cross section (4D) Various energy storage cycle coalescing engines with a speed output of 23,000 times the weight of steam-driven heat, electricity and cold.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), driving the high-pressure turbine with a combined engine combustion section (31Y) high-temperature mercury (1d) on the turbine blade cross section (4D) Various energy storage cycle coalescing engines with a speed output of 23,000 times the weight of steam-driven heat, electricity and cold.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, and driving the high-pressure turbine with the turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) Various energy storage cycle coalescing engines that use the same speed output as 23,000 times the weight of steam-driven heat, electricity, and cold supply facilities.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for application, and a high-pressure turbine driven by a high-pressure mercury (1d) turbine blade combustion section (32D) turbine blade cross section (4D) Various energy storage cycle coalescing engines that use the same speed output as 23,000 times the weight of steam-driven heat, electricity, and cold supply facilities.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, and driving the high-pressure turbine with the turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) Various energy conservation cycle coalescing engines with the same speed output and various ships equipped with steam-driven 23,000 times kg weight m / sec.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for application, and a high-pressure turbine driven by a high-pressure mercury (1d) turbine blade combustion section (32D) turbine blade cross section (4D) Various energy conservation cycle coalescing engines with the same speed output and various ships equipped with steam-driven 23,000 times kg weight m / sec.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), driving the high-pressure turbine with a combined engine combustion section (31X) high-temperature mercury (1d) on the turbine blade cross section (4D) Various energy storage cycle coalescing engines that make the speed output a variety of ships equipped with steam-driven 23,000 times kg weight m / sec.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), driving the high-pressure turbine with a combined engine combustion section (31Y) high-temperature mercury (1d) on the turbine blade cross section (4D) Various energy storage cycle coalescing engines that make the speed output a variety of ships equipped with steam-driven 23,000 times kg weight m / sec.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), driving the high-pressure turbine with a combined engine combustion section (31X) high-temperature mercury (1d) on the turbine blade cross section (4D) Various energy storage cycle coalescing engines that make the speed output 23000 times the weight of steam driven aircraft / kg / m.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), driving the high-pressure turbine with a combined engine combustion section (31Y) high-temperature mercury (1d) on the turbine blade cross section (4D) Various energy storage cycle coalescing engines that make the speed output 23000 times the weight of steam driven aircraft / kg / m.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, and driving the high-pressure turbine with the turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) Various energy storage cycle coalescing engines with the same speed output and various airplanes equipped with steam-driven 23,000 times kg weight m / sec.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for application, and a high-pressure turbine driven by a high-pressure mercury (1d) turbine blade combustion section (32D) turbine blade cross section (4D) Various energy storage cycle coalescing engines with the same speed output and various airplanes equipped with steam-driven 23,000 times kg weight m / sec.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for application, and a high-pressure turbine driven by high-pressure turbine (32X) high-temperature water (52b) in the turbine blade cross section (4D) Various energy conservation cycle coalescing engines that make various airplanes equipped with the same speed output 1700 times kg weight m / sec of steam drive.   Aiming for a maximum work of 1.65 million times with application-specific bearing (80) thrust bearing (80a), high-pressure turbine driven with turbine blade cross section (4D) full blade combustion part (32Y) high temperature water (52b) and atmospheric pressure Various energy conservation cycle coalescing engines that make various airplanes equipped with the same speed output 1700 times kg weight m / sec of steam drive.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), driving the high-pressure turbine with the combined engine combustion section (31X) hot water (52b) on the turbine blade cross section (4D) Various energy storage cycle coalescing engines that use various airplanes with a speed output of 1,700 times the weight of steam driven m / s.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), driving the high-pressure turbine with the combined engine combustion section (31Y) high-temperature water (52b) of the turbine blade cross section (4D) Various energy storage cycle coalescing engines that use various airplanes with a speed output of 1,700 times the weight of steam driven m / s.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), driving the high-pressure turbine with the combined engine combustion section (31X) hot water (52b) on the turbine blade cross section (4D) Various energy storage cycle coalescing engines that make various speeds with a steam output of 1700 times kg weight m / sec.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), driving the high-pressure turbine with the combined engine combustion section (31Y) high-temperature water (52b) of the turbine blade cross section (4D) Various energy storage cycle coalescing engines that make various speeds with a steam output of 1700 times kg weight m / sec.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for application, and a high-pressure turbine driven by high-pressure turbine (32X) high-temperature water (52b) in the turbine blade cross section (4D) Various energy storage cycle coalescing engines that make the same speed output to various ships equipped with 1700 times the weight of steam driven m / s.   Aiming for a maximum work of 1.65 million times with application-specific bearing (80) thrust bearing (80a), high-pressure turbine driven with turbine blade cross section (4D) full blade combustion part (32Y) high temperature water (52b) and atmospheric pressure Various energy storage cycle coalescing engines that make the same speed output to various ships equipped with 1700 times the weight of steam driven m / s.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for application, and a high-pressure turbine driven by high-pressure turbine (32X) high-temperature water (52b) in the turbine blade cross section (4D) Various energy storage cycle coalescing engines that use the same speed output as the supply equipment for various heat, electricity, and cold at 1,700 times the weight of steam driven m / sec.   Aiming for a maximum work of 1.65 million times with application-specific bearing (80) thrust bearing (80a), high-pressure turbine driven with turbine blade cross section (4D) full blade combustion part (32Y) high temperature water (52b) and atmospheric pressure Various energy storage cycle coalescing engines that use the same speed output as the supply equipment for various heat, electricity, and cold at 1,700 times the weight of steam driven m / sec.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), driving the high-pressure turbine with the combined engine combustion section (31X) hot water (52b) on the turbine blade cross section (4D) Various energy storage cycle coalescing engines with speed output of 1,700 times the weight of steam driven m / sec.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), driving the high-pressure turbine with the combined engine combustion section (31Y) high-temperature water (52b) of the turbine blade cross section (4D) Various energy storage cycle coalescing engines with speed output of 1,700 times the weight of steam driven m / sec.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), the combined engine combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven by a high-pressure turbine below the critical temperature. Various energy storage cycle coalescence engines with a heat consumption of approximately 1/72, etc., and a facility for supplying various types of heat, electricity and cold.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, a high-pressure turbine drive is performed with the combined combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) below the critical temperature. Various energy storage cycle coalescence engines with a heat consumption of approximately 1/72, etc., and a facility for supplying various types of heat, electricity and cold.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) suitable for applications, high-pressure turbine drive of the turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) below the critical temperature Various energy storage cycle coalescing engines with a heat consumption of approximately 1/72, etc. to provide various heat, electricity and cold supply facilities.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) suitable for applications, high-pressure turbine drive of turbine blade cross section (4D) full blade combustion part (32Y) high temperature mercury (1d) below critical temperature Various energy storage cycle coalescing engines with a heat consumption of approximately 1/72, etc. to provide various heat, electricity and cold supply facilities.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) suitable for applications, high-pressure turbine drive of the turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) below the critical temperature Various energy storage cycle coalescing engines with various heat consumptions of about 1/72 etc. to make various ships.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) suitable for applications, high-pressure turbine drive of turbine blade cross section (4D) full blade combustion part (32Y) high temperature mercury (1d) below critical temperature Various energy storage cycle coalescing engines with various heat consumptions of about 1/72 etc. to make various ships.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), the combined engine combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven by a high-pressure turbine below the critical temperature. Various energy storage cycle coalescing engines that reduce the amount of heat consumed to approximately 1/72 etc. to make various ships.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, a high-pressure turbine drive is performed with the combined combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) below the critical temperature. Various energy storage cycle coalescing engines that reduce the amount of heat consumed to approximately 1/72 etc. to make various ships.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), the combined engine combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven by a high-pressure turbine below the critical temperature. Various energy storage cycle coalescing engines that reduce the amount of heat consumed to approximately 1/72 etc. to make various aircraft.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, a high-pressure turbine drive is performed with the combined combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) below the critical temperature. Various energy storage cycle coalescing engines that reduce the amount of heat consumed to approximately 1/72 etc. to make various aircraft.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) suitable for applications, high-pressure turbine drive of the turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) below the critical temperature Various energy storage cycle coalescing engines that reduce the amount of heat consumed to approximately 1/72 and make various aircraft.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) suitable for applications, high-pressure turbine drive of turbine blade cross section (4D) full blade combustion part (32Y) high temperature mercury (1d) below critical temperature Various energy storage cycle coalescing engines that reduce the amount of heat consumed to approximately 1/72 and make various aircraft.   A high-pressure turbine with an application-ready bearing (80) thrust bearing (80a), aiming for a maximum work rate of 1.65 million times, turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) below 1000 degrees Celsius Various energy storage cycle coalescing engines that drive to make various types of airplanes that consume approximately 1/72 of heat.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) aiming for a maximum work of 1.65 million times, a turbine blade cross section (4D) full blade combustion part (32Y) high-temperature mercury (1d) high pressure turbine below 1000 degrees Celsius Various energy storage cycle coalescing engines that drive to make various types of airplanes that consume approximately 1/72 of heat.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), high-pressure turbine drive with a combined combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D) at 1000 degrees Celsius or less Various energy storage cycle coalescing engines that make various types of airplanes that consume approximately 1/72 of heat.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), a high-pressure turbine drive with a combined combustion section (31Y) high-temperature mercury (1d) in the turbine blade cross section (4D) at 1000 degrees Celsius or less Various energy storage cycle coalescing engines that make various types of airplanes that consume approximately 1/72 of heat.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), a high-pressure turbine drive with a combined combustion section (31X) high-temperature mercury (1d) in the turbine blade cross section (4D) at 1000 degrees Celsius or less Various energy storage cycle coalescing engines that reduce the amount of heat consumed to about 1/72.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), a high-pressure turbine drive with a combined combustion section (31Y) high-temperature mercury (1d) in the turbine blade cross section (4D) at 1000 degrees Celsius or less Various energy storage cycle coalescing engines that reduce the amount of heat consumed to about 1/72.   A high-pressure turbine with an application-ready bearing (80) thrust bearing (80a), aiming for a maximum work rate of 1.65 million times, turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) below 1000 degrees Celsius Various energy storage cycle coalescing engines that drive to make various types of ships with approximately 1/72 of heat consumption.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) aiming for a maximum work of 1.65 million times, a turbine blade cross section (4D) full blade combustion part (32Y) high-temperature mercury (1d) high pressure turbine below 1000 degrees Celsius Various energy storage cycle coalescing engines that drive to make various types of ships with approximately 1/72 of heat consumption.   A high-pressure turbine with an application-ready bearing (80) thrust bearing (80a), aiming for a maximum work rate of 1.65 million times, turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) below 1000 degrees Celsius Various energy storage cycle coalescing engines that are driven to produce various heat, electricity and cold supply facilities that consume approximately 1/72 of heat.   A bearing (80) suitable for applications (80a) and a thrust bearing (80a) aiming for a maximum work of 1.65 million times, a turbine blade cross section (4D) full blade combustion part (32Y) high-temperature mercury (1d) high pressure turbine below 1000 degrees Celsius Various energy storage cycle coalescing engines that are driven to produce various heat, electricity and cold supply facilities that consume approximately 1/72 of heat.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), high-pressure turbine drive with a combined combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D) at 1000 degrees Celsius or less Various energy storage cycle coalescing engines that use various heat, electricity, and cold supply facilities that consume approximately 1/72 of heat.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), high-pressure turbine drive with a combined combustion section (31Y) high-temperature mercury (1d) in the turbine blade cross section (4D) at 1000 degrees Celsius or less Various energy storage cycle coalescing engines that use various heat, electricity, and cold supply facilities that consume approximately 1/72 of heat.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, a high-pressure turbine drive with a combined engine combustion section (31X) high-temperature mercury (1d) in the turbine blade cross section (4D) at 800 degrees Celsius or less Various energy storage cycle coalescing engines that use various heat, electricity, and cold supply facilities that consume approximately 1/72 of heat.   The bearing (80) thrust bearing (80a) for the application aims at a maximum work of 1.65 million times, and the combined combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven at a high pressure turbine below 800 degrees Celsius. Various energy storage cycle coalescing engines that use various heat, electricity, and cold supply facilities that consume approximately 1/72 of heat.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for use, a high-pressure turbine with a turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) at 800 degrees Celsius or less Various energy storage cycle coalescing engines that are driven to produce various heat, electricity and cold supply facilities that consume approximately 1/72 of heat.   A high-pressure turbine with an application-ready bearing (80) thrust bearing (80a) with a maximum of 1.65 million times power and a turbine blade cross section (4D) full blade combustion part (32Y) high-temperature mercury (1d) at 800 degrees Celsius or less Various energy storage cycle coalescing engines that are driven to produce various heat, electricity and cold supply facilities that consume approximately 1/72 of heat.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for use, a high-pressure turbine with a turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) at 800 degrees Celsius or less Various energy storage cycle coalescing engines that drive to make various types of ships with approximately 1/72 of heat consumption.   A high-pressure turbine with an application-ready bearing (80) thrust bearing (80a) with a maximum of 1.65 million times power and a turbine blade cross section (4D) full blade combustion part (32Y) high-temperature mercury (1d) at 800 degrees Celsius or less Various energy storage cycle coalescing engines that drive to make various types of ships with approximately 1/72 of heat consumption.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, a high-pressure turbine drive with a combined engine combustion section (31X) high-temperature mercury (1d) in the turbine blade cross section (4D) at 800 degrees Celsius or less Various energy storage cycle coalescing engines that reduce the amount of heat consumed to about 1/72.   The bearing (80) thrust bearing (80a) for the application aims at a maximum work of 1.65 million times, and the combined combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven at a high pressure turbine below 800 degrees Celsius. Various energy storage cycle coalescing engines that reduce the amount of heat consumed to about 1/72.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), a high-pressure turbine drive with a combined combustion section (31X) high-temperature mercury (1d) of a turbine blade cross section (4D) at 800 degrees Celsius or less Various energy storage cycle coalescing engines that make various types of airplanes that consume approximately 1/72 of heat.   The bearing (80) thrust bearing (80a) for the application aims at a maximum work of 1.65 million times, and the combined combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) is driven at a high pressure turbine below 800 degrees Celsius. Various energy storage cycle coalescing engines that make various types of airplanes that consume approximately 1/72 of heat.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for use, a high-pressure turbine with a turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) at 800 degrees Celsius or less Various energy storage cycle coalescing engines that drive to make various types of airplanes that consume approximately 1/72 of heat.   A high-pressure turbine with an application-ready bearing (80) thrust bearing (80a) with a maximum of 1.65 million times power and a turbine blade cross section (4D) full blade combustion part (32Y) high-temperature mercury (1d) at 800 degrees Celsius or less Various energy storage cycle coalescing engines that drive to make various types of airplanes that consume approximately 1/72 of heat.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, a high-pressure turbine with a turbine blade cross section (4D) full blade combustion part (32X) high temperature mercury (1d) at 600 degrees Celsius or less Various energy storage cycle coalescing engines that drive to make various types of airplanes that consume approximately 1/72 of heat.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for use, a high-pressure turbine with a turbine blade cross section (4D) full blade combustion part (32Y) high-temperature mercury (1d) below 600 degrees Celsius Various energy storage cycle coalescing engines that drive to make various types of airplanes that consume approximately 1/72 of heat.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, a high-pressure turbine drive with a combined engine combustion section (31X) high-temperature mercury (1d) in the turbine blade cross section (4D) at 600 degrees Celsius or less Various energy storage cycle coalescing engines that make various types of airplanes that consume approximately 1/72 of heat.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), a high-pressure turbine drive with a combined combustion section (31Y) high-temperature mercury (1d) of a turbine blade cross section (4D) at 600 degrees Celsius or less Various energy storage cycle coalescing engines that make various types of airplanes that consume approximately 1/72 of heat.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, a high-pressure turbine drive with a combined engine combustion section (31X) high-temperature mercury (1d) in the turbine blade cross section (4D) at 600 degrees Celsius or less Various energy storage cycle coalescing engines that reduce the amount of heat consumed to about 1/72.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), a high-pressure turbine drive with a combined combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) at 600 degrees Celsius or less Various energy storage cycle coalescing engines that reduce the amount of heat consumed to about 1/72.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, a high-pressure turbine with a turbine blade cross section (4D) full blade combustion part (32X) high temperature mercury (1d) at 600 degrees Celsius or less Various energy storage cycle coalescing engines that drive to make various types of ships with approximately 1/72 of heat consumption.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for use, a high-pressure turbine with a turbine blade cross section (4D) full blade combustion part (32Y) high-temperature mercury (1d) below 600 degrees Celsius Various energy storage cycle coalescing engines that drive to make various types of ships with approximately 1/72 of heat consumption.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, a high-pressure turbine with a turbine blade cross section (4D) full blade combustion part (32X) high temperature mercury (1d) at 600 degrees Celsius or less Various energy storage cycle coalescing engines that are driven to produce various heat, electricity and cold supply facilities that consume approximately 1/72 of heat.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for use, a high-pressure turbine with a turbine blade cross section (4D) full blade combustion part (32Y) high-temperature mercury (1d) below 600 degrees Celsius Various energy storage cycle coalescing engines that are driven to produce various heat, electricity and cold supply facilities that consume approximately 1/72 of heat.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, a high-pressure turbine drive with a combined engine combustion section (31X) high-temperature mercury (1d) in the turbine blade cross section (4D) at 600 degrees Celsius or less Various energy storage cycle coalescing engines that use various heat, electricity, and cold supply facilities that consume approximately 1/72 of heat.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), a high-pressure turbine drive with a combined combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) at 600 degrees Celsius or less Various energy storage cycle coalescing engines that use various heat, electricity, and cold supply facilities that consume approximately 1/72 of heat.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, a high-pressure turbine is driven at a temperature below the critical temperature for the combined engine combustion section (31X) high-temperature water (52b) of the turbine blade cross section (4D). Various energy storage cycle coalescing engines that use various heat, electricity, and cold supply facilities such as approximately 1/539.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, a high-pressure turbine is driven at a critical temperature or lower with the combined engine combustion section (31Y) high-temperature water (52b) on the turbine blade cross section (4D). Various energy storage cycle coalescing engines that use various heat, electricity, and cold supply facilities such as approximately 1/539.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, high-pressure turbine drive of the turbine blade cross section (4D) full blade combustion part (32X) high temperature water (52b) below the critical temperature Various energy storage cycle coalescing engines that use various heat, electricity, and cold supply facilities, such as approximately 1/539, for the amount of heat consumed.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, high-pressure turbine drive of the turbine blade cross section (4D) full blade combustion part (32Y) high temperature water (52b) below the critical temperature Various energy storage cycle coalescing engines that use various heat, electricity, and cold supply facilities, such as approximately 1/539, for the amount of heat consumed.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, high-pressure turbine drive of the turbine blade cross section (4D) full blade combustion part (32X) high temperature water (52b) below the critical temperature Various energy storage cycle coalescing engines that make the amount of heat consumed approximately 1/539.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, high-pressure turbine drive of the turbine blade cross section (4D) full blade combustion part (32Y) high temperature water (52b) below the critical temperature Various energy storage cycle coalescing engines that make the amount of heat consumed approximately 1/539.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, a high-pressure turbine is driven at a temperature below the critical temperature for the combined engine combustion section (31X) high-temperature water (52b) of the turbine blade cross section (4D). Various energy storage cycle coalescing engines that make various types of ships that consume approximately 1/539 of heat.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, a high-pressure turbine is driven at a critical temperature or lower with the combined engine combustion section (31Y) high-temperature water (52b) on the turbine blade cross section (4D). Various energy storage cycle coalescing engines that make various types of ships that consume approximately 1/539 of heat.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, a high-pressure turbine is driven at a temperature below the critical temperature for the combined engine combustion section (31X) high-temperature water (52b) of the turbine blade cross section (4D). Various energy storage cycle coalescing engines that make various types of airplanes that consume approximately 1/539 of heat.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, a high-pressure turbine drive is performed with the combined engine combustion section (31Y) high-temperature water (52b) on the turbine blade cross section (4D) below the critical temperature. Various energy storage cycle coalescing engines that make various types of airplanes that consume approximately 1/539 of heat.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, high-pressure turbine drive of the turbine blade cross section (4D) full blade combustion part (32X) high temperature water (52b) below the critical temperature Various energy storage cycle coalescing engines that make various types of airplanes that consume approximately 1/539 of heat.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, high-pressure turbine drive of the turbine blade cross section (4D) full blade combustion part (32Y) high temperature water (52b) below the critical temperature Various energy storage cycle coalescing engines that make various types of airplanes that consume approximately 1/539 of heat.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, and a high-pressure turbine drive with high-temperature turbine (32X) high-temperature water (52b) in the turbine blade cross section (4D). Various energy conservation cycle coalescing engines that make various airplanes such as 1/539.   Aiming for a maximum work of 1.65 million times with application-specific bearing (80) thrust bearing (80a) and driving high-pressure turbine with turbine blade cross section (4D) full blade combustion part (32Y) high temperature water (52b) Various energy conservation cycle coalescing engines that make various airplanes such as 1/539.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for use, and driving a high-pressure turbine with a combined engine combustion section (31X) high-temperature water (52b) on the turbine blade cross section (4D) to reduce the amount of heat consumed Various energy conservation cycle coalescing engines that make various airplanes such as about 1/539.   Aiming for a maximum work of 1.65 million times with the bearing (80) thrust bearing (80a) for the application, and driving the high-pressure turbine with the combined engine combustion section (31Y) high-temperature water (52b) of the turbine blade cross section (4D) to reduce the heat consumption. Various energy conservation cycle coalescing engines that make various airplanes such as about 1/539.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for use, and driving a high-pressure turbine with a combined engine combustion section (31X) high-temperature water (52b) on the turbine blade cross section (4D) to reduce the amount of heat consumed Various energy conservation cycle coalescing engines for various ships such as approximately 1/539.   Aiming for a maximum work of 1.65 million times with the bearing (80) thrust bearing (80a) for the application, and driving the high-pressure turbine with the combined engine combustion section (31Y) high-temperature water (52b) of the turbine blade cross section (4D) to reduce the heat consumption. Various energy conservation cycle coalescing engines for various ships such as approximately 1/539.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, and a high-pressure turbine drive with high-temperature turbine (32X) high-temperature water (52b) in the turbine blade cross section (4D). Various energy conservation cycle coalescing engines that make various ship types such as approximately 1/539.   Aiming for a maximum work of 1.65 million times with application-specific bearing (80) thrust bearing (80a) and driving high-pressure turbine with turbine blade cross section (4D) full blade combustion part (32Y) high temperature water (52b) Various energy conservation cycle coalescing engines that make various ship types such as approximately 1/539.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, and a high-pressure turbine drive with high-temperature turbine (32X) high-temperature water (52b) in the turbine blade cross section (4D). Various energy storage cycle coalescence engines that make various heat, electricity, and cold supply facilities of approximately 1/539.   Aiming for a maximum work of 1.65 million times with application-specific bearing (80) thrust bearing (80a) and driving high-pressure turbine with turbine blade cross section (4D) full blade combustion part (32Y) high temperature water (52b) Various energy storage cycle coalescence engines that make various heat, electricity, and cold supply facilities of approximately 1/539.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for use, and driving a high-pressure turbine with a combined engine combustion section (31X) high-temperature water (52b) on the turbine blade cross section (4D) to reduce the amount of heat consumed Various energy storage cycle coalescing engines that provide various heat, electricity, and cold supply facilities such as approximately 1/539.   Aiming for a maximum work of 1.65 million times with the bearing (80) thrust bearing (80a) for the application, and driving the high-pressure turbine with the combined engine combustion section (31Y) high-temperature water (52b) of the turbine blade cross section (4D) to reduce the heat consumption. Various energy storage cycle coalescing engines that provide various heat, electricity, and cold supply facilities such as approximately 1/539.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), driving the high-pressure turbine with the combined engine combustion section (31X) hot water (52b) on the turbine blade cross section (4D) Various energy storage cycle coalescence engine that makes the speed output 1700 times kg weight m / second of steam drive, etc. in vacuum, and adds various gravitational acceleration to various heat, electricity and cold supply facilities.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), driving the high-pressure turbine with the combined engine combustion section (31Y) high-temperature water (52b) of the turbine blade cross section (4D) Various energy storage cycle coalescence engine that makes the speed output 1700 times kg weight m / second of steam drive, etc. in vacuum, and adds various gravitational acceleration to various heat, electricity and cold supply facilities.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for application, and a high-pressure turbine driven by high-pressure turbine (32X) high-temperature water (52b) in the turbine blade cross section (4D) Various energy storage cycle coalescing engines that use the same speed output as a steam-driven 1700 times kg weight m / second, etc. in vacuum, and supply facilities for various heat, electricity and cold in addition to gravitational acceleration.   Aiming for a maximum work of 1.65 million times with application-specific bearing (80) thrust bearing (80a), high-pressure turbine driven with turbine blade cross section (4D) full blade combustion part (32Y) high temperature water (52b) and atmospheric pressure Various energy storage cycle coalescing engines that use the same speed output as a steam-driven 1700 times kg weight m / second, etc. in vacuum, and supply facilities for various heat, electricity and cold in addition to gravitational acceleration.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for application, and a high-pressure turbine driven by high-pressure turbine (32X) high-temperature water (52b) in the turbine blade cross section (4D) Various energy storage cycle coalescing engines that make the same speed output 1700 times kg weight m / sec of steam drive and various ships with gravity acceleration added in vacuum.   Aiming for a maximum work of 1.65 million times with application-specific bearing (80) thrust bearing (80a), high-pressure turbine driven with turbine blade cross section (4D) full blade combustion part (32Y) high temperature water (52b) and atmospheric pressure Various energy storage cycle coalescing engines that make the same speed output 1700 times kg weight m / sec of steam drive and various ships with gravity acceleration added in vacuum.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), driving the high-pressure turbine with the combined engine combustion section (31X) hot water (52b) on the turbine blade cross section (4D) Various energy conservation cycle coalescing engines that make the speed output 1700 times the weight of steam driven m / sec.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), driving the high-pressure turbine with the combined engine combustion section (31Y) high-temperature water (52b) of the turbine blade cross section (4D) Various energy conservation cycle coalescing engines that make the speed output 1700 times the weight of steam driven m / sec.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), driving the high-pressure turbine with the combined engine combustion section (31X) hot water (52b) on the turbine blade cross section (4D) Various energy storage cycle coalescing engines that make the speed output 1700 times the weight of steam driven, m / sec.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), driving the high-pressure turbine with the combined engine combustion section (31Y) high-temperature water (52b) of the turbine blade cross section (4D) Various energy storage cycle coalescing engines that make the speed output 1700 times the weight of steam driven, m / sec.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for application, and a high-pressure turbine driven by high-pressure turbine (32X) high-temperature water (52b) in the turbine blade cross section (4D) Various energy conservation cycle coalescing engine that makes the same speed output 1700 times kg weight of steam driven m / second, etc., and various airplanes with gravity acceleration added in vacuum.   Aiming for a maximum work of 1.65 million times with application-specific bearing (80) thrust bearing (80a), high-pressure turbine driven with turbine blade cross section (4D) full blade combustion part (32Y) high temperature water (52b) and atmospheric pressure Various energy conservation cycle coalescing engine that makes the same speed output 1700 times kg weight of steam driven m / second, etc., and various airplanes with gravity acceleration added in vacuum.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, and driving the high-pressure turbine with the turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) Various energy storage cycle coalescing engine that makes the same speed output 23000 times kg weight m / sec of water vapor drive and other airplanes with gravity acceleration added in vacuum.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for application, and a high-pressure turbine driven by a high-pressure mercury (1d) turbine blade combustion section (32D) turbine blade cross section (4D) Various energy storage cycle coalescing engine that makes the same speed output 23000 times kg weight m / sec of water vapor drive and other airplanes with gravity acceleration added in vacuum.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), driving the high-pressure turbine with a combined engine combustion section (31X) high-temperature mercury (1d) on the turbine blade cross section (4D) Various energy storage cycle coalescing engines that make the speed output 23,000 times the weight of water vapor driven kg weight m / second, etc., in various airplanes with gravity acceleration added in vacuum.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), driving the high-pressure turbine with a combined engine combustion section (31Y) high-temperature mercury (1d) on the turbine blade cross section (4D) Various energy storage cycle coalescing engines that make the speed output 23,000 times the weight of water vapor driven kg weight m / second, etc., in various airplanes with gravity acceleration added in vacuum.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), driving the high-pressure turbine with a combined engine combustion section (31X) high-temperature mercury (1d) on the turbine blade cross section (4D) Various energy conservation cycle coalescing engines that make the speed output 23,000 times the weight of water vapor driven kg weight m / sec.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), driving the high-pressure turbine with a combined engine combustion section (31Y) high-temperature mercury (1d) on the turbine blade cross section (4D) Various energy conservation cycle coalescing engines that make the speed output 23,000 times the weight of water vapor driven kg weight m / sec.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, and driving the high-pressure turbine with the turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) Various energy storage cycle coalescing engines that make the same speed output 23,000 times the weight of steam driven kg weight m / sec.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for application, and a high-pressure turbine driven by a high-pressure mercury (1d) turbine blade combustion section (32D) turbine blade cross section (4D) Various energy storage cycle coalescing engines that make the same speed output 23,000 times the weight of steam driven kg weight m / sec.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), driving the high-pressure turbine with a turbine blade cross section (4D) full blade combustion section (32X) high-temperature mercury (1d) and atmospheric pressure Various energy storage cycle coalescing engines that use the same speed output as a steam-driven 23,000 times kg weight m / second, etc. to supply various heat, electricity and cold supply facilities with additional gravity acceleration in vacuum.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for application, and a high-pressure turbine driven by a high-pressure mercury (1d) turbine blade combustion section (32D) turbine blade cross section (4D) Various energy storage cycle coalescing engines that use the same speed output as a steam-driven 23,000 times kg weight m / second, etc. to supply various heat, electricity and cold supply facilities with additional gravity acceleration in vacuum.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, driving the high-pressure turbine with the combined engine combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D) Various energy storage cycle coalescing engines that make the speed output 23,000 times the weight of water vapor driven kg weight m / second, etc., and supply various types of heat, electricity, and cold in a vacuum.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, driving the high-pressure turbine with the combined engine combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D) Various energy storage cycle coalescing engines that make the speed output 23,000 times the weight of water vapor driven kg weight m / second, etc., and supply various types of heat, electricity, and cold in a vacuum.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, and the combined combustion part (31X) high-temperature mercury (1d) of the turbine blade cross section (4D) gravity vertically in the jet vacuum Various energy storage cycle coalescing engines that drive high-pressure turbines with acceleration with added acceleration.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, and the combined combustion part (31Y) high-temperature mercury (1d) of the turbine blade cross-section (4D) gravity vertically in the jet vacuum Various energy storage cycle coalescing engines that drive high-pressure turbines with acceleration with added acceleration.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) vertically injected in vacuum Various energy storage cycle coalescing engines that drive high-pressure turbines with acceleration with added gravitational acceleration.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, the turbine blade cross section (4D) full rotor blade combustion part (32Y) high-temperature mercury (1d) vertically in a jet vacuum Various energy storage cycle coalescing engines that drive high-pressure turbines with acceleration with added gravitational acceleration.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) vertically injected in vacuum Combined with various energy storage cycle engines that use high-pressure turbine-driven various heat, electricity, and cold supply facilities with acceleration by adding gravitational acceleration.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, the turbine blade cross section (4D) full rotor blade combustion part (32Y) high-temperature mercury (1d) vertically in a jet vacuum Combined with various energy storage cycle engines that use high-pressure turbine-driven various heat, electricity, and cold supply facilities with acceleration by adding gravitational acceleration.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, and the combined combustion part (31X) high-temperature mercury (1d) of the turbine blade cross section (4D) gravity vertically in the jet vacuum Various energy storage cycle coalescing engines that use high-pressure turbine-driven various heat, electricity and cold supply facilities by adding acceleration.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, and the combined combustion part (31Y) high-temperature mercury (1d) of the turbine blade cross-section (4D) gravity vertically in the jet vacuum Various energy storage cycle coalescing engines that use high-pressure turbine-driven various heat, electricity and cold supply facilities by adding acceleration.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, and the combined combustion part (31X) high-temperature mercury (1d) of the turbine blade cross section (4D) gravity vertically in the jet vacuum Various energy storage cycle coalescing engines that make various vessels driven by high pressure turbines with acceleration added.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, and the combined combustion part (31Y) high-temperature mercury (1d) of the turbine blade cross-section (4D) gravity vertically in the jet vacuum Various energy storage cycle coalescing engines that make various vessels driven by high pressure turbines with acceleration added.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) vertically injected in vacuum Various energy storage cycle coalescing engines that make various vessels driven by high-pressure turbines with acceleration with added gravitational acceleration.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, the turbine blade cross section (4D) full rotor blade combustion part (32Y) high-temperature mercury (1d) vertically in a jet vacuum Various energy storage cycle coalescing engines that make various vessels driven by high-pressure turbines with acceleration with added gravitational acceleration.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), turbine blade cross section (4D) full blade combustion part (32X) high-temperature mercury (1d) vertically injected in vacuum Various energy storage cycle coalescing engines that make various airplanes driven by high-pressure turbines with acceleration by adding gravitational acceleration.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, the turbine blade cross section (4D) full rotor blade combustion part (32Y) high-temperature mercury (1d) vertically in a jet vacuum Various energy storage cycle coalescing engines that make various airplanes driven by high-pressure turbines with acceleration by adding gravitational acceleration.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, and the combined combustion part (31X) high-temperature mercury (1d) of the turbine blade cross section (4D) gravity vertically in the jet vacuum Various energy storage cycle coalescing engines that make various airplanes driven by high pressure turbines with acceleration added.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, and the combined combustion part (31Y) high-temperature mercury (1d) of the turbine blade cross-section (4D) gravity vertically in the jet vacuum Various energy storage cycle coalescing engines that make various airplanes driven by high pressure turbines with acceleration added.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, and the combined engine combustion section (31X) high-temperature water (52b) of the turbine blade cross section (4D) gravity vertically in the jet vacuum Various energy storage cycle coalescing engines that make various airplanes driven by high pressure turbines with acceleration added.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, and the combined engine combustion section (31Y) high-temperature water (52b) of the turbine blade cross section (4D) gravity down in the jet vacuum Various energy storage cycle coalescing engines that make various airplanes driven by high pressure turbines with acceleration added.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, injecting the whole blade combustion part (32X) high-temperature water (52b) in the turbine blade cross section (4D) vertically in the injection vacuum Various energy storage cycle coalescing engines that make various airplanes driven by high-pressure turbines with acceleration by adding gravitational acceleration.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, all blade combustion section (32Y) high-temperature water (52b) of turbine blade cross section (4D) is injected vertically downward in a vacuum. Various energy storage cycle coalescing engines that make various airplanes driven by high-pressure turbines with acceleration by adding gravitational acceleration.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, injecting the whole blade combustion part (32X) high-temperature water (52b) in the turbine blade cross section (4D) vertically in the injection vacuum Various energy storage cycle coalescing engines that make various vessels driven by high-pressure turbines with acceleration with added gravitational acceleration.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, all blade combustion section (32Y) high-temperature water (52b) of turbine blade cross section (4D) is injected vertically downward in a vacuum. Various energy storage cycle coalescing engines that make various vessels driven by high-pressure turbines with acceleration with added gravitational acceleration.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, and the combined engine combustion section (31X) high-temperature water (52b) of the turbine blade cross section (4D) gravity vertically in the jet vacuum Various energy storage cycle coalescing engines that make various vessels driven by high pressure turbines with acceleration added.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, and the combined engine combustion section (31Y) high-temperature water (52b) of the turbine blade cross section (4D) gravity down in the jet vacuum Various energy storage cycle coalescing engines that make various vessels driven by high pressure turbines with acceleration added.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, and the combined engine combustion section (31X) high-temperature water (52b) of the turbine blade cross section (4D) gravity vertically in the jet vacuum Various energy storage cycle coalescing engines that use high-pressure turbine-driven various heat, electricity and cold supply facilities by adding acceleration.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, and the combined engine combustion section (31Y) high-temperature water (52b) of the turbine blade cross section (4D) gravity down in the jet vacuum Various energy storage cycle coalescing engines that use high-pressure turbine-driven various heat, electricity and cold supply facilities by adding acceleration.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, injecting the whole blade combustion part (32X) high-temperature water (52b) in the turbine blade cross section (4D) vertically in the injection vacuum Combined with various energy storage cycle engines that use high-pressure turbine-driven various heat, electricity, and cold supply facilities with acceleration by adding gravitational acceleration.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, all blade combustion section (32Y) high-temperature water (52b) of turbine blade cross section (4D) is injected vertically downward in a vacuum. Combined with various energy storage cycle engines that use high-pressure turbine-driven various heat, electricity, and cold supply facilities with acceleration by adding gravitational acceleration.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, injecting the whole blade combustion part (32X) high-temperature water (52b) in the turbine blade cross section (4D) vertically in the injection vacuum Various energy storage cycle coalescing engines that drive high-pressure turbines with acceleration with added gravitational acceleration.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, all blade combustion section (32Y) high-temperature water (52b) of turbine blade cross section (4D) is injected vertically downward in a vacuum. Various energy storage cycle coalescing engines that drive high-pressure turbines with acceleration with added gravitational acceleration.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, and the combined engine combustion section (31X) high-temperature water (52b) of the turbine blade cross section (4D) gravity vertically in the jet vacuum Various energy storage cycle coalescing engines that drive high-pressure turbines with acceleration with added acceleration.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, and the combined engine combustion section (31Y) high-temperature water (52b) of the turbine blade cross section (4D) gravity down in the jet vacuum Various energy storage cycle coalescing engines that drive high-pressure turbines with acceleration with added acceleration.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, the intake air is heated by the combined engine combustion part (31X) high-temperature mercury (1d) exhaust heat quantity of the turbine blade cross section (4D) Compressed heat recovery theory Combined engine with various energy storage cycles to make the best heat pump (1G).   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, the intake air is heated by the combined engine combustion section (31Y) high-temperature mercury (1d) exhaust heat quantity of the turbine blade cross section (4D) Compressed heat recovery theory Combined engine with various energy storage cycles to make the best heat pump (1G).   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, the intake air is heated by the whole blade combustion part (32X) high-temperature mercury (1d) exhaust heat quantity of the turbine blade cross section (4D) Compressed heat recovery theory Combined engine with various energy storage cycles to make the best heat pump (1G).   Aiming at a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, the intake air is heated by the total blade combustion part (32Y) high-temperature mercury (1d) exhaust heat of the turbine blade cross section (4D) Compressed heat recovery theory Combined engine with various energy storage cycles to make the best heat pump (1G).   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, intake air by exhaust heat quantity near 230 degrees of all blade combustion part (32X) high temperature mercury (1d) turbine blade cross section (4D) Various energy storage cycle coalescence engine that heats the heat to the compression heat recovery theory best heat pump (1G).   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, intake air by exhaust heat quantity near 230 degrees of all blade combustion part (32Y) high temperature mercury (1d) turbine blade cross section (4D) Various energy storage cycle coalescence engine that heats the heat to the compression heat recovery theory best heat pump (1G).   Aiming at a maximum work of 1.65 million times with the bearing (80) thrust bearing (80a) for the application, the combined engine combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D), and the intake heat by the exhaust heat quantity near 230 degrees Various energy storage cycle coalescing engines that heat to produce the best heat pump (1G) for compression heat recovery theory.   The bearing (80) thrust bearing (80a) for the application aims at a maximum work of 1.65 million times, and the intake air is absorbed by the exhaust heat quantity near 230 degrees of the combined engine combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D). Various energy storage cycle coalescing engines that heat to produce the best heat pump (1G) for compression heat recovery theory.   Aiming at a maximum work of 1.65 million times with the bearing (80) thrust bearing (80a) for the application, the combined engine combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D), and the intake heat by the exhaust heat quantity near 230 degrees Compression heat recovery theory best heat pump (1G) Combined engine with various energy storage cycles to supply various types of heat, electricity and cold.   The bearing (80) thrust bearing (80a) for the application aims at a maximum work of 1.65 million times, and the intake air is absorbed by the exhaust heat quantity near 230 degrees of the combined engine combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D). Compression heat recovery theory best heat pump (1G) Combined engine with various energy storage cycles to supply various types of heat, electricity and cold.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, intake air by exhaust heat quantity near 230 degrees of all blade combustion part (32X) high temperature mercury (1d) turbine blade cross section (4D) Compressed heat recovery theory best heat pump (1G) to make various heat, electricity and cold supply facilities, etc.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, intake air by exhaust heat quantity near 230 degrees of all blade combustion part (32Y) high temperature mercury (1d) turbine blade cross section (4D) Compressed heat recovery theory best heat pump (1G) to make various heat, electricity and cold supply facilities, etc.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, intake air by exhaust heat quantity near 230 degrees of all blade combustion part (32X) high temperature mercury (1d) turbine blade cross section (4D) Compressed heat recovery theory best heat pump (1G) various energy storage cycle coalescing engine to heat.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, intake air by exhaust heat quantity near 230 degrees of all blade combustion part (32Y) high temperature mercury (1d) turbine blade cross section (4D) Compressed heat recovery theory best heat pump (1G) various energy storage cycle coalescing engine to heat.   Aiming at a maximum work of 1.65 million times with the bearing (80) thrust bearing (80a) for the application, the combined engine combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D), and the intake heat by the exhaust heat quantity near 230 degrees Compression energy recovery theory best heat pump (1G) various energy storage cycle coalescing engines that are heated to various ships.   The bearing (80) thrust bearing (80a) for the application aims at a maximum work of 1.65 million times, and the intake air is absorbed by the exhaust heat quantity near 230 degrees of the combined engine combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D). Compression energy recovery theory best heat pump (1G) various energy storage cycle coalescing engines that are heated to various ships.   Aiming at a maximum work of 1.65 million times with the bearing (80) thrust bearing (80a) for the application, the combined engine combustion section (31X) high-temperature mercury (1d) of the turbine blade cross section (4D), and the intake heat by the exhaust heat quantity near 230 degrees Compression energy recovery theory best heat pump (1G) Various energy storage cycle coalescing engines that are heated to various airplanes.   The bearing (80) thrust bearing (80a) for the application aims at a maximum work of 1.65 million times, and the intake air is absorbed by the exhaust heat quantity near 230 degrees of the combined engine combustion section (31Y) high-temperature mercury (1d) of the turbine blade cross section (4D). Compression energy recovery theory best heat pump (1G) Various energy storage cycle coalescing engines that are heated to various airplanes.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, intake air by exhaust heat quantity near 230 degrees of all blade combustion part (32X) high temperature mercury (1d) turbine blade cross section (4D) Compressed heat recovery theory best heat pump (1G) various energy storage cycle coalescing engine by heating the air.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, intake air by exhaust heat quantity near 230 degrees of all blade combustion part (32Y) high temperature mercury (1d) turbine blade cross section (4D) Compressed heat recovery theory best heat pump (1G) various energy storage cycle coalescing engine by heating the air.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, the intake air is heated by the combined engine combustion part (31X) high-temperature mercury (1d) exhaust heat quantity of the turbine blade cross section (4D) Compression heat recovery theory Best heat pump (1G) Various energy storage cycle coalescing engine for various heat, electricity and cold supply facilities.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, the intake air is heated by the combined engine combustion section (31Y) high-temperature mercury (1d) exhaust heat quantity of the turbine blade cross section (4D) Compression heat recovery theory Best heat pump (1G) Various energy storage cycle coalescing engine for various heat, electricity and cold supply facilities.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, the intake air is heated by the whole blade combustion part (32X) high-temperature mercury (1d) exhaust heat quantity of the turbine blade cross section (4D) Compressed heat recovery theory Best heat pump (1G) Various energy storage cycle coalescing engine for various heat, electricity and cold supply facilities.   Aiming at a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, the intake air is heated by the total blade combustion part (32Y) high-temperature mercury (1d) exhaust heat of the turbine blade cross section (4D) Compressed heat recovery theory Best heat pump (1G) Various energy storage cycle coalescing engine for various heat, electricity and cold supply facilities.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, the intake air is heated by the whole blade combustion part (32X) high-temperature mercury (1d) exhaust heat quantity of the turbine blade cross section (4D) Compressed heat recovery theory Best heat pump (1G) Various energy storage cycle coalescing engines for various ships.   Aiming at a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, the intake air is heated by the total blade combustion part (32Y) high-temperature mercury (1d) exhaust heat of the turbine blade cross section (4D) Compressed heat recovery theory Best heat pump (1G) Various energy storage cycle coalescing engines for various ships.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, the intake air is heated by the combined engine combustion part (31X) high-temperature mercury (1d) exhaust heat quantity of the turbine blade cross section (4D) Compression heat recovery theory Best heat pump (1G) Various energy storage cycle coalescing engines for various ships.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, the intake air is heated by the combined engine combustion section (31Y) high-temperature mercury (1d) exhaust heat quantity of the turbine blade cross section (4D) Compression heat recovery theory Best heat pump (1G) Various energy storage cycle coalescing engines for various ships.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, the intake air is heated by the combined engine combustion part (31X) high-temperature mercury (1d) exhaust heat quantity of the turbine blade cross section (4D) Compressed heat recovery theory Best heat pump (1G) Various energy storage cycle coalescing engines for various airplanes.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, the intake air is heated by the combined engine combustion section (31Y) high-temperature mercury (1d) exhaust heat quantity of the turbine blade cross section (4D) Compressed heat recovery theory Best heat pump (1G) Various energy storage cycle coalescing engines for various airplanes.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, the intake air is heated by the whole blade combustion part (32X) high-temperature mercury (1d) exhaust heat quantity of the turbine blade cross section (4D) Compressed heat recovery theory Best heat pump (1G) Various energy storage cycle coalescing engines for various airplanes.   Aiming at a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, the intake air is heated by the total blade combustion part (32Y) high-temperature mercury (1d) exhaust heat of the turbine blade cross section (4D) Compressed heat recovery theory Best heat pump (1G) Various energy storage cycle coalescing engines for various airplanes.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for use, and providing a cold heat recovery means (3C) on the turbine blade (8c) of the turbine blade cross section (4D) of the turbine blade cross section (4D) Various energy storage cycle coalescence engine that collects cold energy.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for use, and providing a cold heat recovery means (3C) on the turbine blade (8c) of the turbine blade cross section (4D) of the turbine blade cross section (4D) Various energy storage cycle coalescence engine to heat.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for use, and providing a cold heat recovery means (3C) on the turbine blade (8c) of the turbine blade cross section (4D) of the turbine blade cross section (4D) Various energy storage cycle coalescence engine that recovers cold energy with alcohol (1C) or the like.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for use, and providing a cold heat recovery means (3C) on the turbine blade (8c) of the turbine blade cross section (4D) of the turbine blade cross section (4D) Various energy storage cycle coalescence engine heated with alcohol (1C) or the like.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for use, and providing a cold heat recovery means (3C) on the turbine blade (8c) of the turbine blade cross section (4D) of the turbine blade cross section (4D) Various energy storage cycle coalescing engine that collects and outputs cold energy with alcohol (1C).   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for use, and providing a cold heat recovery means (3C) on the turbine blade (8c) of the turbine blade cross section (4D) of the turbine blade cross section (4D) Various energy storage cycle coalescing engines that increase heating output with alcohol (1C) or the like.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for use, and providing a cold heat recovery means (3C) on the turbine blade (8c) of the turbine blade cross section (4D) of the turbine blade cross section (4D) Collecting cold energy with alcohol (1C), etc. Various energy storage cycle coalescence engines that prevent sticking of dry ice and moisture.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for use, and providing a cold heat recovery means (3C) on the turbine blade (8c) of the turbine blade cross section (4D) of the turbine blade cross section (4D) Various energy storage cycle coalescence engines that prevent the adhesion of heated dry ice and moisture with alcohol (1C).   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for application, and providing a heating high temperature means (3B) on the turbine blade (8c) of the turbine blade cross section (4D) of the turbine blade cross section (4D) Various energy storage cycle coalescence engine to heat.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), providing water repellent action (3A) on the turbine blade (8c) of the turbine blade cross section (4D) Water repellent energy conservation cycle coalescence engine.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for application, and providing a heating high temperature means (3B) on the turbine blade (8c) of the turbine blade cross section (4D) of the turbine blade cross section (4D) Various energy storage cycle coalescing engines that produce rolling contact rotation output by a heated vaporization film.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), providing water repellent action (3A) on the turbine blade (8c) of the turbine blade cross section (4D) Various energy storage cycle coalescing engine that produces rolling contact rotation output by water repellent action.   Aiming at a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for various applications, various types of turbine blade cross-section (4D) with all rotor blade water turbines with an exhaust saturation temperature of around 30 degrees as cold (52e) cooling Energy conservation cycle coalescence engine.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for the application, seawater temperature with cooling (52e) cooling near the exhaust saturation temperature of all rotor blade water turbines with a turbine blade cross section (4D) Various energy conservation cycle coalescence engine that prevents the climb.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for various applications, and recovering and storing alcohol cold heat (52e) in an all-blade gas turbine with a turbine blade cross section (4D) Cycle coalescence engine.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for various applications, and various energy used by recovering and storing compressed air cold heat (52e) in a turbine blade cross section (4D) full blade gas turbine Conservation cycle coalescence organization.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), and recovering and storing ice-cold heat (52e) in a turbine blade cross-section (4D) full blade gas turbine for various energy conservation Cycle coalescence engine.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for application, and collecting and storing cold heat (52e) with a turbine blade cross section (4D) full blade gas turbine as various refrigeration equipment Various energy conservation cycle coalescence engines used.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for use, and collecting and storing cold heat (52e) with a turbine blade cross section (4D) full blade gas turbine as various refrigeration equipment Various energy conservation cycle coalescence engines used.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for use, and collecting and storing cold heat (52e) with a turbine blade cross-section (4D) full blade gas turbine as various cooling equipment Various energy conservation cycle coalescence engines used.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for application, and collecting and storing cold heat (52e) in a turbine blade cross section (4D) full blade gas turbine as various cooling equipment Various energy conservation cycle coalescence engines used.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for application, and collecting and storing cold heat (52e) with a turbine blade cross section (4D) full blade gas turbine as various ice making equipment Various energy conservation cycle coalescence engines used.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for various applications, and collecting and storing cold heat (52e) with all blade gas turbines with a turbine blade cross section (4D). Various energy conservation cycle coalescence engine used as a kind.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), supplying all rotor blade gas turbine exhaust with a turbine blade cross section (4D) as combustion gas dissolved water (52 g) such as CO2 to the seabed Various energy conservation cycle coalescing engines.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), supplying all rotor blade gas turbine exhaust with a turbine blade cross section (4D) as combustion gas dissolved water (52 g) such as CO2 to the seabed Various energy conservation cycle coalescing engines that grow seaweeds.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), supplying all rotor blade gas turbine exhaust with a turbine blade cross section (4D) as combustion gas dissolved water (52 g) such as CO2 to the seabed Various energy conservation cycle coalescence organizations that grow algae.   Aiming for a maximum work of 1.65 million times with an application-compatible bearing (80) thrust bearing (80a), supplying all rotor blade gas turbine exhaust with a turbine blade cross section (4D) as combustion gas dissolved water (52 g) such as CO2 to the seabed Various energy conservation cycle coalescence organizations that grow phytoplanktons.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for use, and recovering and storing excess heat at various temperatures (52d) of 300 degrees or less for exclusive use of the rotational output of the turbine blade cross section (4E) Various energy conservation cycle coalescence engines used.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for use, and recovering and storing excess heat at various temperatures (52d) of 300 degrees or less for exclusive use of the rotational output of the turbine blade cross section (4E) Various energy storage cycle coalescence engine used as various heating equipment.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for use, and recovering and storing excess heat at various temperatures (52d) of 300 degrees or less for exclusive use of the rotational output of the turbine blade cross section (4E) Various energy conservation cycle coalescence engine used as various cooking equipment.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for use, and recovering and storing excess heat at various temperatures (52d) of 300 degrees or less for exclusive use of the rotational output of the turbine blade cross section (4E) Various energy conservation cycle coalescence engine used as various hot water equipment.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for use, and recovering and storing excess heat at various temperatures (52d) of 300 degrees or less for exclusive use of the rotational output of the turbine blade cross section (4E) Various energy conservation cycle coalescence engine used as various dishwashers.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for use, and recovering and storing excess heat at various temperatures (52d) of 300 degrees or less for exclusive use of the rotational output of the turbine blade cross section (4E) Various energy storage cycle coalescence engine used as various washing dryers.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for use, and recovering and storing excess heat at various temperatures (52d) of 300 degrees or less for exclusive use of the rotational output of the turbine blade cross section (4E) Various energy conservation cycle coalescence engine used as various water temperature and heat piping buildings.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for use, and recovering and storing excess heat at various temperatures (52d) of 300 degrees or less for exclusive use of the rotational output of the turbine blade cross section (4E) Various energy conservation cycle coalescence engine that uses various water such as seawater as distilled water.   Aiming for a maximum work of 1.65 million times with a bearing (80) thrust bearing (80a) for use, and recovering and storing excess heat at various temperatures (52d) of 300 degrees or less for exclusive use of the rotational output of the turbine blade cross section (4E) Various energy conservation cycle coalescence engine that uses various water such as seawater as distilled water and salt.   Turbine blade cross section (4D) application-compatible bearing (80) Thrust bearing (80a) aiming for a maximum of 1.65 million times power, recovering compressed air heat (28b) with intake air (28a) and heat pump (1G) Various energy storage cycle coalescing engines that recover compression heat.   Turbine blade cross section (4D) application-compatible bearing (80) Thrust bearing (80a) aiming for a maximum of 1.65 million times power and recovering mercury exhaust heat (5A) + compressed air heat (28b) by intake air (28a) Various energy storage cycle coalescence engines that recover compression heat with a heat pump (1G).   Turbine blade cross section (4D) application-compatible bearing (80) Thrust bearing (80a) aiming for a maximum of 1.65 million times power, recovering compressed air heat (28b) with intake air (28a) and heat pump (1G) Various energy storage cycle coalescing engine that recovers heat as 500 to 1000 degrees compression.   Turbine blade cross section (4D) application-compatible bearing (80) Thrust bearing (80a) aiming for a maximum of 1.65 million times power and recovering mercury exhaust heat (5A) + compressed air heat (28b) by intake air (28a) Various energy storage cycle coalescence engines that recover heat with a heat pump (1G) as compressed at 500 to 1000 degrees.   Turbine blade cross section (4D) application-compatible bearing (80) Thrust bearing (80a) aiming for a maximum of 1.65 million times power, recovering compressed air heat (28b) with intake air (28a) and heat pump (1G) Various energy storage cycle coalescence engine that recovers heat to 500-1000 degrees of compression and drives all rotor blade water turbine.   Turbine blade cross section (4D) application-compatible bearing (80) Thrust bearing (80a) aiming for a maximum of 1.65 million times power, recovering compressed air heat (28b) with intake air (28a) and heat pump (1G) Various energy storage cycle coalescing engines that recover heat at a compression of 500 to 1000 degrees, etc., and drive all moving blade mercury turbines.   Turbine blade cross section (4D) application-compatible bearing (80) Thrust bearing (80a) aiming for a maximum of 1.65 million times power, recovering compressed air heat (28b) with intake air (28a) and heat pump (1G) Various energy storage cycle coalescing engines that drive all rotor blade gas turbines by recovering heat at a compression of 500 to 1000 degrees, etc.   Turbine blade cross section (4D) application-compatible bearing (80) Thrust bearing (80a) aiming for a maximum of 1.65 million times power, and becomes high temperature when returning to the earth at flight speeds such as flight wing (38b) and flight tail (38c) Various energy storage cycle coalescing engines in which water (52a) pipes reduced in weight to high pressure with carbon fiber or the like are piped in all parts, and a high-pressure light-weight container is constituted to recover heat.   Turbine blade cross section (4D) application-compatible bearing (80) Thrust bearing (80a) aiming for a maximum of 1.65 million times power, and becomes high temperature when returning to the earth at flight speeds such as flight wing (38b) and flight tail (38c) Various energy storage cycle coalescing engines in which superheated steam (50) pipes are reduced in weight to high pressure with carbon fiber or the like, and the high-pressure light-weight container is configured to recover heat.   Turbine blade cross section (4D) application-compatible bearing (80) Thrust bearing (80a) aiming for a maximum of 1.65 million times power, and becomes high temperature when returning to the earth at flight speeds such as flight wing (38b) and flight tail (38c) Various energy storage cycle coalescing engines in which high-temperature and light-weight containers are constructed and heat-recovered by piping high-temperature mercury (1d) pipes that are lightened to high-pressure with carbon fiber or the like in all parts.   Turbine blade cross section (4D) application-compatible bearing (80) Thrust bearing (80a) aiming for a maximum of 1.65 million times power, and becomes high temperature when returning to the earth at flight speeds such as flight wing (38b) and flight tail (38c) Various energy storage cycle coalescing engines that recover the heat of a high-pressure lightweight container by piping a combustion gas pipe that has been reduced in weight to high pressure with carbon fiber or the like in all parts.   Turbine blade cross section (4D) application-compatible bearing (80) Thrust bearing (80a) aiming for a maximum of 1.65 million times power, and becomes high temperature when returning to the earth at flight speeds such as flight wing (38b) and flight tail (38c) Various energy storage cycle coalescing engines in which water (52a) pipes reduced in weight to high pressure with carbon nanotubes or the like are piped in all parts, and the high-pressure and light-weight container is configured to recover heat.   Turbine blade cross section (4D) application-compatible bearing (80) Thrust bearing (80a) aiming for a maximum of 1.65 million times power, and becomes high temperature when returning to the earth at flight speeds such as flight wing (38b) and flight tail (38c) Various energy storage cycle coalescing engines in which the superheated steam (50) pipe, which has been reduced in weight to high pressure with carbon nanotubes or the like, is piped in all parts, and the high-pressure lightweight container is configured to recover heat.   Turbine blade cross section (4D) application-compatible bearing (80) Thrust bearing (80a) aiming for a maximum of 1.65 million times power, and becomes high temperature when returning to the earth at flight speeds such as flight wing (38b) and flight tail (38c) Various energy storage cycle coalescing engines in which high-temperature and lightweight containers are constructed and heat-recovered by piping high-temperature mercury (1d) pipes that are lightened to high-pressure with carbon nanotubes or the like in all parts.   Turbine blade cross section (4D) application-compatible bearing (80) Thrust bearing (80a) aiming for a maximum of 1.65 million times power, and becomes high temperature when returning to the earth at flight speeds such as flight wing (38b) and flight tail (38c) Various energy storage cycle coalescing engines in which the combustion gas pipes are reduced in weight to high pressure with carbon nanotubes or the like, and the high-pressure lightweight container is configured to recover heat.   Turbine blade cross section (4D) application-compatible bearing (80) Thrust bearing (80a) aiming for a maximum of 1.65 million times power and recovering combustion gas (49) heat quantity with intake air (28a) and heat pump (1G) Various energy storage cycle coalescence engine that recovers heat to 500-1000 degrees of compression and drives all rotor blade water turbine.   Turbine blade cross section (4D) application-compatible bearing (80) Thrust bearing (80a) aiming for a maximum of 1.65 million times power and recovering combustion gas (49) heat quantity with intake air (28a) and heat pump (1G) Various energy storage cycle coalescing engines that recover heat at a compression of 500 to 1000 degrees, etc., and drive all moving blade mercury turbines.   Turbine blade cross section (4D) application-compatible bearing (80) Thrust bearing (80a) aiming for a maximum of 1.65 million times power and recovering combustion gas (49) heat quantity with intake air (28a) and heat pump (1G) Various energy storage cycle coalescing engines that drive all rotor blade gas turbines by recovering heat at a compression of 500 to 1000 degrees, etc.   Turbine blade cross section (4D) application-compatible bearing (80) Thrust bearing (80a) aiming for a maximum of 1.65 million times power and recovering combustion gas (49) heat quantity with intake air (28a) and heat pump (1G) Various energy storage cycle coalescing engines that recover the heat at a compression of 500 to 1000 degrees or the like and drive the coalescing engine injection unit (79K).   Turbine blade cross section (4D) application-compatible bearing (80) Thrust bearing (80a) aiming for a maximum of 1.65 million times power and recovering combustion gas (49) heat quantity with intake air (28a) and heat pump (1G) Various energy storage cycle coalescing engines that drive the waterjet (79M) all-blade mercury turbine by recovering heat as 500 to 1000 degrees of compression.   Turbine blade cross section (4D) application-compatible bearing (80) Thrust bearing (80a) aiming for a maximum of 1.65 million times power, recovering compressed air heat (28b) with intake air (28a) and heat pump (1G) Various energy storage cycle coalescing engines that recover the heat at a compression of 500 to 1000 degrees or the like and drive the coalescing engine injection unit (79K).   Turbine blade cross section (4D) application-compatible bearing (80) Thrust bearing (80a) aiming for a maximum of 1.65 million times power, recovering compressed air heat (28b) with intake air (28a) and heat pump (1G) Various energy storage cycle coalescing engine that recovers heat at 500-1000 degrees of compression and drives water jet (79M).   Various energy storage cycles aiming at 1650,000 times the work rate + 910,000 times the work rate + all the blades work rate with the bearing (80) thrust bearing (80a) for the whole blade combustion part (32X) of the turbine blade cross section (4D) Combined organization.   Various energy storage cycles aiming at 1650,000 times the work rate + 910,000 times the work rate + all the blades work rate with the bearing (80) thrust bearing (80a) of the turbine blade cross section (4D) for all blade combustion part (32Y) applications Combined organization.   Combined engine combustion section (31X) of turbine blade cross section (4D) (80) Thrust bearing (80a) with various energy conservation cycle coalescence aiming at 1650,000 times power + 910,000 times power + total blade power organ.   Combined combustion section (31Y) of turbine blade cross section (4D) for bearing (80) Thrust bearing (80a) Combined with various energy conservation cycles aiming at 1650,000 times power + 910,000 times power + total blade power organ.   Various energy storage cycle coalescing engines aiming for 910,000 times higher work rate + total moving blade work rate with bearing (80) thrust bearing (80a) for all blade combustion part (32X) application of turbine blade cross section (4D).   Various energy storage cycle coalescing engines aiming for 910,000 times higher work rate + total moving blade work rate with bearing (80) thrust bearing (80a) for all blade combustion part (32Y) application of turbine blade cross section (4D).   Various energy storage cycle coalescing engines aiming for 910,000 times power + total rotor blade power with a bearing (80) thrust bearing (80a) compatible with the combined engine combustion section (31X) of the turbine blade cross section (4D).   Various energy storage cycle coalescing engines aiming for 910,000 times power + total blade power with bearings (80) thrust bearings (80a) compatible with combined engine combustion section (31Y) of turbine blade cross section (4D).   Various energy storage cycle coalescence engines aiming at the full blade efficiency with bearings (80) thrust bearings (80a) for all blade combustion section (32X) applications with turbine blade cross section (4D).   Various energy storage cycle coalescence engines aiming at the full blade efficiency with the bearing (80) thrust bearing (80a) for the all blade combustion part (32Y) application of the turbine blade cross section (4D).   Various energy storage cycle coalescence engines aiming at the full blade efficiency with a bearing (80) thrust bearing (80a) compatible with the combined engine combustion section (31X) of the turbine blade cross section (4D).   Various energy storage cycle coalescing engines aiming at full blade power with bearings (80) thrust bearings (80a) for combined engine combustion section (31Y) of turbine blade cross section (4D).   Various energy storage cycle coalescing engines aiming for 910,000 times higher work in bearings (80) thrust bearings (80a) for all rotor blade combustion section (32X) applications with turbine blade cross section (4D).   Various energy storage cycle coalescing engines aiming for 910,000 times higher work with bearings (80) thrust bearings (80a) for all rotor blade combustion section (32Y) applications of turbine blade cross section (4D).   Various energy storage cycle coalescing engines aiming for 910,000 times higher work in bearings (80) thrust bearings (80a) for combined engine combustion section (31X) of turbine blade cross section (4D).   Various energy storage cycle coalescing engines aiming for 910,000 times higher power with a bearing (80) thrust bearing (80a) compatible with a combined engine combustion section (31Y) of a turbine blade cross section (4D).   Various energy storage cycle coalescence engines aiming at a work rate of 1,650,000 times with a bearing (80) thrust bearing (80a) for all rotor blade combustion section (32X) applications of turbine blade cross section (4D).   Various energy storage cycle coalescing engines aiming at a work rate of 1,650,000 times with a bearing (80) thrust bearing (80a) compatible with all rotor blade combustion sections (32Y) in the turbine blade cross section (4D).   Various energy storage cycle coalescing engines aiming at a work of 1.65 million times with a bearing (80) thrust bearing (80a) compatible with a combined engine combustion section (31X) of a turbine blade cross section (4D).   Various energy storage cycle coalescing engines aiming at a work of 1.65 million times with a bearing (80) thrust bearing (80a) compatible with the combined engine combustion section (31Y) of the turbine blade cross section (4D).   Various energy storage cycle coalescence engines aiming at 1.65 million times power + 910,000 times power + total power blade power with bearing (80) thrust bearing (80a) for turbine blade cross section (4D) application.   Various energy storage cycle coalescence engines aiming at 910,000 times the work rate + total power blade work rate with bearing (80) thrust bearing (80a) for turbine blade cross section (4D) application.   Various energy storage cycle coalescing engines aiming at full blade efficiency with a bearing (80) thrust bearing (80a) for turbine blade cross section (4D) application.   Various energy storage cycle coalescing engines aiming for 910,000 times higher work with bearing (80) thrust bearing (80a) for turbine blade cross section (4D) application.   Various energy storage cycle coalescing engines aiming at 1.65 million times power with a bearing (80) thrust bearing (80a) for turbine blade cross section (4D) application.   Various energy conservation cycle coalescing engines provided with a bearing (80) thrust bearing (80a) aiming at 910,000 times the power of the turbine blade cross section (4D) and used as an opposed series full blade impeller water turbine (8b).   Various energy conservation cycle coalescence engines provided in two stages as opposed series full blade impeller water turbine (8b) provided with bearing (80) thrust bearing (80a) aiming at 910,000 times work rate of turbine blade cross section (4D).   Various energy conservation cycle coalescence engines equipped with a bearing (80) thrust bearing (80a) aiming at 910,000 times power of the turbine blade cross section (4D) and provided in three stages as an opposed series full blade impeller water turbine (8b).   Various energy conservation cycle coalescence engines equipped with a bearing (80) thrust bearing (80a) aiming at 910,000 times power of the turbine blade cross section (4D) and provided in four stages as an opposed series full blade impeller water turbine (8b).   Various energy conservation cycle coalescence engines equipped with a bearing (80) thrust bearing (80a) aiming at 910,000 times power of the turbine blade cross section (4D) and provided in five stages as an opposed series full blade impeller water turbine (8b).   Various energy storage cycle coalescing engines equipped with a bearing (80) thrust bearing (80a) aiming at 910,000 times the power of the turbine blade cross section (4D) and provided in six stages as an opposed series full blade impeller water turbine (8b).   Various energy conservation cycle coalescence engines equipped with a bearing (80) thrust bearing (80a) aiming at 910,000 times power of the turbine blade cross section (4D) and equipped in 7 stages as an opposed series full blade impeller water turbine (8b).   Various energy conservation cycle coalescing engines equipped with a bearing (80) thrust bearing (80a) aiming for a 910,000-fold work rate of the turbine blade cross section (4D) and equipped in eight stages as an opposed series full blade impeller water turbine (8b).   Various energy conservation cycle coalescence engines equipped with a bearing (80) thrust bearing (80a) aiming at 910,000 times power of the turbine blade cross section (4D) and equipped in 9 stages as an opposed series full blade impeller water turbine (8b).   Various energy conservation cycle coalescence engines equipped with a bearing (80) thrust bearing (80a) aiming at 910,000 times power of the turbine blade cross section (4D) and provided in 10 stages as an opposed series full blade impeller water turbine (8b).   Various energy conservation cycle coalescence engines equipped with 11 stages as opposed series full blade impeller water turbine (8b) with bearing (80) thrust bearing (80a) aiming at 910,000 times power of turbine blade cross section (4D).   Various energy storage cycle coalescence engines equipped with 12 stages as opposed series full blade impeller water turbine (8b) provided with bearing (80) thrust bearing (80a) aiming at 910,000 times power of turbine blade cross section (4D).   Various energy storage cycle coalescing engines provided with a bearing (80) thrust bearing (80a) aiming at a 1.65 million times power of the turbine blade cross section (4D) and used as an opposed series full blade impeller mercury turbine (8E).   Various energy storage cycle coalescing engines equipped with a bearing (80) thrust bearing (80a) aiming at 1.65 million times work of the turbine blade cross section (4D) and equipped in two stages as an opposed series full blade impeller mercury turbine (8E).   Various energy storage cycle coalescing engines equipped with a bearing (80) thrust bearing (80a) aiming at 1.65 million times power of the turbine blade cross section (4D) and equipped in three stages as an opposed series full blade impeller mercury turbine (8E).   Various energy storage cycle coalescing engines equipped with a bearing (80) thrust bearing (80a) aiming at 1.65 million times power of the turbine blade cross section (4D) and equipped in four stages as an opposed series full blade impeller mercury turbine (8E).   Various energy storage cycle coalescing engines equipped with a bearing (80) thrust bearing (80a) aiming at a work of 1.65 million times the turbine blade cross section (4D) and equipped in five stages as an opposed series full blade impeller mercury turbine (8E).   Various energy conservation cycle coalescence engines equipped with a bearing (80) thrust bearing (80a) aiming at a work of 1.65 million times the turbine blade cross section (4D) and equipped in six stages as an opposed series full blade impeller mercury turbine (8E).   Various energy storage cycle coalescing engines equipped with a bearing (80) thrust bearing (80a) aiming at a work of 1.65 million times the turbine blade cross section (4D) and equipped in seven stages as an opposed series full blade impeller mercury turbine (8E).   Various energy storage cycle coalescing engines equipped with a bearing (80) thrust bearing (80a) aiming at 1.65 million times power of the turbine blade cross section (4D) and equipped in 8 stages as an opposed series full blade impeller mercury turbine (8E).   Various energy conservation cycle coalescence engines equipped with 9 stages as opposed series full blade impeller mercury turbine (8E) with bearing (80) thrust bearing (80a) aiming at 1.65 million times power of turbine blade cross section (4D).   Various energy storage cycle coalescing engines equipped with a bearing (80) thrust bearing (80a) aiming at 1.65 million times power of the turbine blade cross section (4D) and equipped in 10 stages as an opposed series full blade impeller mercury turbine (8E).   Various energy conservation cycle coalescence engines equipped with 11 stages as opposed series full blade impeller mercury turbine (8E) with bearing (80) thrust bearing (80a) aiming at 1.65 million times power of turbine blade cross section (4D).   Various energy conservation cycle coalescence engines equipped with 12 stages as opposed series full blade impeller mercury turbine (8E) provided with bearing (80) thrust bearing (80a) aiming at 1.65 million times power of turbine blade cross section (4D).   Combined with various energy conservation cycles, provided with a bearing (80) thrust bearing (80a) aiming at high pressure injection and large mass injection 100 to 1000 times the turbine blade cross section (4E) to form an opposed series full blade impeller gas turbine (8a) organ.   Various bearings equipped in two stages as opposed series full blade impeller gas turbine (8a) with bearing (80) thrust bearing (80a) aiming at high pressure injection and large mass injection 100-1000 times turbine blade cross section (4E) Energy conservation cycle coalescence engine.   Various bearings provided in three stages as opposed series full blade impeller gas turbine (8a) with bearing (80) thrust bearing (80a) aiming at high pressure injection and large mass injection 100-1000 times turbine blade cross section (4E) Energy conservation cycle coalescence engine.   Various bearings provided in four stages as opposed series full blade impeller gas turbine (8a) with bearing (80) thrust bearing (80a) aiming at high pressure injection and large mass injection 100-1000 times turbine blade cross section (4E) Energy conservation cycle coalescence engine.   Various bearings equipped with a bearing (80) thrust bearing (80a) aiming at high pressure injection and mass injection 100 to 1000 times the turbine blade cross section (4E) and provided in five stages as opposed series full blade impeller gas turbine (8a) Energy conservation cycle coalescence engine.   Bearings (80) and thrust bearings (80a) aiming at high pressure injection and large mass injection 100 to 1000 times the turbine blade cross section (4E) are provided in six stages as opposed series full blade impeller gas turbine (8a). Energy conservation cycle coalescence engine.   Various bearings equipped in seven stages as opposed series full blade impeller gas turbine (8a) with bearing (80) thrust bearing (80a) aiming at high pressure injection and large mass injection 100-1000 times turbine blade cross section (4E) Energy conservation cycle coalescence engine.   Various bearings equipped with a bearing (80) thrust bearing (80a) aiming at high-pressure injection and large-mass injection 100 to 1000 times the turbine blade cross section (4E) and provided in eight stages as opposed series full blade impeller gas turbine (8a) Energy conservation cycle coalescence engine.   Various bearings equipped with a bearing (80) thrust bearing (80a) aiming at high pressure injection and large mass injection 100 to 1000 times the turbine blade cross section (4E) and provided in nine stages as opposed series full blade impeller gas turbine (8a) Energy conservation cycle coalescence engine.   Various bearings equipped with a bearing (80) thrust bearing (80a) aiming at high pressure injection and large mass injection 100 to 1000 times the turbine blade cross section (4E) and provided in 10 stages as opposed series full blade impeller gas turbine (8a) Energy conservation cycle coalescence engine.   Various bearings equipped with a bearing (80) thrust bearing (80a) aiming at high pressure injection and large mass injection 100 to 1000 times the turbine blade cross section (4E) and provided in 11 stages as opposed series full blade impeller gas turbine (8a) Energy conservation cycle coalescence engine.   Various bearings equipped with a bearing (80) thrust bearing (80a) aiming at high-pressure injection and large-mass injection 100 to 1000 times the turbine blade cross section (4E) and provided in 12 stages as opposed series full blade impeller gas turbine (8a) Energy conservation cycle coalescence engine.   Various energy conservation cycle coalescing engines provided with a bearing (80) thrust bearing (80a) aiming for a 910,000-fold work rate of the turbine blade cross section (4D) and used as a series full blade impeller water turbine (8b).   Various energy conservation cycle coalescence engines equipped with a stage (80) thrust bearing (80a) aiming for a 910,000-fold work rate of the turbine blade cross section (4D) and equipped in two stages as a series full blade impeller water turbine (8b).   Various energy storage cycle coalescence engines equipped with a bearing (80) thrust bearing (80a) aiming at 910,000 times the power of the turbine blade cross section (4D) and equipped in three stages as a series full blade impeller water turbine (8b).   Various energy storage cycle coalescence engines equipped with a bearing (80) thrust bearing (80a) aiming at 910,000 times the power of the turbine blade cross section (4D) and equipped in four stages as a series full blade impeller water turbine (8b).   Various energy conservation cycle coalescing engines equipped with a bearing (80) thrust bearing (80a) aiming at 910,000 times the power of the turbine blade cross section (4D) and provided in five stages as a series full blade impeller water turbine (8b).   Various energy storage cycle coalescing engines equipped with a bearing (80) thrust bearing (80a) aiming at a 910,000-fold work rate of the turbine blade cross section (4D) and equipped in six stages as a series full blade impeller water turbine (8b).   Various energy storage cycle coalescing engines equipped with 7 stages as a series full blade impeller water turbine (8b) provided with a bearing (80) thrust bearing (80a) aiming at 910,000 times the power of the turbine blade cross section (4D).   Various energy storage cycle coalescing engines equipped with a bearing (80) thrust bearing (80a) aiming at a 910,000-fold work rate of the turbine blade cross section (4D) and equipped in 8 stages as a series full blade impeller water turbine (8b).   Various energy storage cycle coalescence engines equipped with 9 stages as a series full blade impeller water turbine (8b) provided with a bearing (80) thrust bearing (80a) aiming at a 910,000-fold work rate of the turbine blade cross section (4D).   Various energy conservation cycle coalescence engines equipped with a bearing (80) thrust bearing (80a) aiming at 910,000 times power of the turbine blade cross section (4D) and equipped in 10 stages as a series full blade impeller water turbine (8b).   Various energy storage cycle coalescing engines equipped with a bearing (80) thrust bearing (80a) aiming for a 910,000-fold work rate of the turbine blade cross section (4D) and equipped in 11 stages as a series full blade impeller water turbine (8b).   Various energy storage cycle coalescing engines equipped with 12 stages as a series full blade impeller water turbine (8b) provided with a bearing (80) thrust bearing (80a) aiming at 910,000 times the work rate of the turbine blade cross section (4D).   Various energy storage cycle coalescing engines provided with a bearing (80) thrust bearing (80a) aiming at 1.65 million times power of the turbine blade cross section (4D) to form a series full blade impeller mercury turbine (8E).   Various energy storage cycle coalescing engines equipped with a stage (80) thrust bearing (80a) aiming at 1.65 million times power of the turbine blade cross section (4D) and equipped in two stages as a series full blade impeller mercury turbine (8E).   Various energy storage cycle coalescence engines equipped with a bearing (80) thrust bearing (80a) aiming at a work of 1.65 million times the turbine blade cross section (4D) and equipped in three stages as a series full blade impeller mercury turbine (8E).   Various energy storage cycle coalescing engines provided in four stages as a series full blade impeller mercury turbine (8E) provided with a bearing (80) thrust bearing (80a) aiming at 1.65 million times power of the turbine blade cross section (4D).   Various energy conservation cycle coalescence engines equipped with a bearing (80) thrust bearing (80a) aiming at a work of 1.65 million times the turbine blade cross section (4D) and equipped in five stages as a series full blade impeller mercury turbine (8E).   Various energy storage cycle coalescing engines provided in six stages as a series full blade impeller mercury turbine (8E) provided with a bearing (80) thrust bearing (80a) aiming at a work of 1.65 million times the turbine blade cross section (4D).   Various energy storage cycle coalescence engines equipped with a bearing (80) thrust bearing (80a) aiming at 1.65 million times power of the turbine blade cross section (4D) and equipped in 7 stages as a series full blade impeller mercury turbine (8E).   Various energy storage cycle coalescing engines equipped with a bearing (80) thrust bearing (80a) aiming at 1.65 million times power of the turbine blade cross section (4D) and equipped in 8 stages as a series full blade impeller mercury turbine (8E).   Various energy storage cycle coalescence engines equipped with 9 stages as a series full blade impeller mercury turbine (8E) provided with a bearing (80) thrust bearing (80a) aiming at 1.65 million times power of the turbine blade cross section (4D).   Various energy storage cycle coalescing engines equipped with a bearing (80) and a thrust bearing (80a) aiming at a work of 1.65 million times the turbine blade cross section (4D) and equipped in 10 stages as a series full blade impeller mercury turbine (8E).   Various energy storage cycle coalescence engines equipped with 11 stages as a series full blade impeller mercury turbine (8E) provided with a bearing (80) thrust bearing (80a) aiming at 1.65 million times power of the turbine blade cross section (4D).   Various energy conservation cycle coalescence engines equipped with 12 stages as a series full blade impeller mercury turbine (8E) provided with a bearing (80) thrust bearing (80a) aiming at 1.65 million times power of the turbine blade cross section (4D).   Various energy conservation cycle coalescence engine provided with a bearing (80) thrust bearing (80a) aiming at high pressure injection and large mass injection 100 to 1000 times the turbine blade cross section (4E) to form a series full blade impeller gas turbine (8a) .   Various energy provided in two stages as a series full blade impeller gas turbine (8a) by providing a bearing (80) thrust bearing (80a) aiming at high pressure injection and large mass injection 100 to 1000 times the turbine blade cross section (4E) Conservation cycle coalescence organization.   Various energy provided in three stages as a series full blade impeller gas turbine (8a) by providing a bearing (80) thrust bearing (80a) aiming at high pressure injection and large mass injection 100 to 1000 times the turbine blade cross section (4E) Conservation cycle coalescence organization.   Various energy provided in four stages as a series full blade impeller gas turbine (8a) by providing a bearing (80) thrust bearing (80a) for high pressure injection and large mass injection 100 to 1000 times the turbine blade cross section (4E) Conservation cycle coalescence organization.   Various energy provided in five stages as a series full blade impeller gas turbine (8a) by providing a bearing (80) thrust bearing (80a) aiming at high pressure injection and large mass injection 100 to 1000 times the turbine blade cross section (4E) Conservation cycle coalescence organization.   Various energy provided in six stages as a series full blade impeller gas turbine (8a) with a bearing (80) thrust bearing (80a) aiming at high pressure injection and large mass injection 100 to 1000 times the turbine blade cross section (4E) Conservation cycle coalescence organization.   Various energy provided in seven stages as a series full blade impeller gas turbine (8a) by providing a bearing (80) thrust bearing (80a) aiming at high pressure injection and large mass injection 100 to 1000 times the turbine blade cross section (4E) Conservation cycle coalescence organization.   Various energy provided in eight stages as a series full blade impeller gas turbine (8a) by providing a bearing (80) thrust bearing (80a) aiming at high pressure injection and large mass injection 100 to 1000 times the turbine blade cross section (4E) Conservation cycle coalescence organization.   Various energy provided in nine stages as a series full blade impeller gas turbine (8a) by providing a bearing (80) thrust bearing (80a) aiming at high pressure injection and large mass injection 100 to 1000 times the turbine blade cross section (4E) Conservation cycle coalescence organization.   Various energy provided in 10 stages as a series full blade impeller gas turbine (8a) by providing a bearing (80) thrust bearing (80a) aiming at high pressure injection and large mass injection 100 to 1000 times the turbine blade cross section (4E) Conservation cycle coalescence organization.   Various energy provided in 11 stages as a series full blade impeller gas turbine (8a) with a bearing (80) thrust bearing (80a) aiming at high pressure injection and large mass injection 100 to 1000 times the turbine blade cross section (4E) Conservation cycle coalescence organization.   Various energy provided in 12 stages as a series full blade impeller gas turbine (8a) by providing a bearing (80) thrust bearing (80a) aiming at high pressure injection and large mass injection 100 to 1000 times the turbine blade cross section (4E) Conservation cycle coalescence organization.   Various energy storage cycle coalescing engines provided with a bearing (80) thrust bearing (80a) aiming for a 910,000-fold work rate of the turbine blade cross section (4D) to form a parallel saddle type full blade air turbine (8B).   Various energy storage cycles provided with a bearing (80) thrust bearing (80a) aiming for a 910,000-fold work rate of the turbine blade cross section (4D) and provided with an outer casing (77a) as a parallel saddle type all-blade water turbine (8B) Combined organization.   Various energy conservation cycles provided with bearings (80) and thrust bearings (80a) aiming at 910,000 times the power of the turbine blade cross section (4D) and having a robust blade group as a parallel saddle type all blade water turbine (8B) Combined organization.   Various energy conservation cycles provided with a bearing (80) thrust bearing (80a) aiming for a 910,000-fold work rate of the turbine blade cross section (4D) and expanding the blade group spacing as a parallel saddle-type full blade water turbine (8B) Combined organization.   Combined with various energy conservation cycles equipped with a bearing (80) thrust bearing (80a) aiming at 910,000 times the work rate of the turbine blade cross section (4D) and expanding the turbine blade interval as a parallel saddle-type full-blade water turbine (8B) organ.   Combined with various energy storage cycles equipped with a bearing (80) thrust bearing (80a) aiming at 910,000 times the work rate of the turbine blade cross section (4D) to increase the strength of the turbine blade as a parallel saddle-type all blade water turbine (8B) organ.   Various energy conservation cycles equipped with a bearing (80) thrust bearing (80a) aiming for a 910,000-fold work rate of the turbine blade cross section (4D) to increase the strength of the blade group as a parallel saddle type all blade water turbine (8B) Combined organization.   Various energy conservation cycles equipped with a bearing (80) thrust bearing (80a) aiming for a 910,000-fold work rate of the turbine blade cross section (4D) to increase the strength of the inner shaft device as a parallel saddle type full-blade water turbine (8B) Combined organization.   Various energy conservation cycles provided with a bearing (80) thrust bearing (80a) aiming at a 910,000-fold work rate of the turbine blade cross section (4D) to increase the strength of the outer shaft device as a parallel saddle-type full blade air turbine (8B) Combined organization.   Various energy storage cycles provided with a bearing (80) thrust bearing (80a) aiming for a 910,000-fold work rate of the turbine blade cross section (4D) and provided with an outer casing (77a) as a parallel saddle type all-blade water turbine (8B) Combined organization.   Combined with various energy storage cycles equipped with a robust turbine blade as a parallel saddle type all-blade water turbine (8B) provided with a bearing (80) thrust bearing (80a) aiming at a 910,000-fold work rate of the turbine blade cross section (4D) organ.   Combined with various energy storage cycles equipped with a bearing (80) thrust bearing (80a) aiming at 910,000 times the work rate of the turbine blade cross section (4D) to increase the strength of the turbine blade as a parallel saddle-type all blade water turbine (8B) organ.   Various energy conservation cycle coalescing engines provided with a bearing (80) thrust bearing (80a) aiming at a work of 1.65 million times the turbine blade cross section (4D) and used as a parallel saddle type all blade mercury turbine (8H).   Various energy storage cycles provided with a bearing (80) thrust bearing (80a) aiming at a work of 1.65 million times the turbine blade cross section (4D) and having an outer casing (77a) as a parallel saddle type full-blade mercury turbine (8H) Combined organization.   Various energy storage cycles equipped with a robust blade group as a parallel saddle type all blade mercury turbine (8H) provided with a bearing (80) thrust bearing (80a) aiming at 1.65 million times work of the turbine blade cross section (4D) Combined organization.   Various energy storage cycles equipped with a bearing (80) thrust thrust bearing (80a) aiming at a work of 1.65 million times the turbine blade cross section (4D) and expanding the blade group spacing as a parallel saddle type all blade mercury turbine (8H) Combined organization.   Combined with various energy storage cycles equipped with a bearing (80) thrust bearing (80a) aiming at 1.65 million times power of the turbine blade cross section (4D) and expanding the turbine blade interval as a parallel saddle type full blade mercury turbine (8H) organ.   Combined with various energy conservation cycles equipped with a bearing (80) thrust bearing (80a) aiming at a work of 1.65 million times the turbine blade cross section (4D) and increasing the strength of the turbine blade as a parallel saddle type all-blade mercury turbine (8H) organ.   Various energy conservation cycles equipped with a bearing (80) thrust bearing (80a) aiming at a work of 1.65 million times the turbine blade cross section (4D) and increasing the strength of the blade group as a parallel saddle type all blade mercury turbine (8H) Combined organization.   Various energy storage cycles equipped with a bearing (80) thrust bearing (80a) aiming at a work of 1.65 million times the turbine blade cross-section (4D) and increasing the strength of the inner shaft device as a parallel saddle type full-blade mercury turbine (8H) Combined organization.   Various energy storage cycles equipped with a bearing (80) thrust bearing (80a) aiming at a work of 1.65 million times the turbine blade cross section (4D) and increasing the strength of the outer shaft device as a parallel saddle type full-blade mercury turbine (8H) Combined organization.   Various energy storage cycles provided with a bearing (80) thrust bearing (80a) aiming at a 1.65 million times power of the turbine blade cross section (4D) and having an outer casing (77a) as an opposed series full blade impeller mercury turbine (8E) Combined organization.   Combined with various energy storage cycles equipped with a robust turbine blade as an opposed series full blade impeller mercury turbine (8E) provided with a bearing (80) thrust bearing (80a) aiming at 1.65 million times power of the turbine blade cross section (4D) organ.   Various bearings with increased turbine blade strength as opposed series full blade impeller mercury turbine (8E) by providing bearing (80) thrust bearing (80a) aiming at 1.65 million times power of turbine blade cross section (4D) aiming at CO2 exhaust 0 Energy conservation cycle coalescence engine.   Combined with various energy storage cycles by providing a bearing (80) thrust bearing (80a) for high pressure injection and large mass injection 100 to 1000 times the turbine blade cross section (4E) to form a parallel saddle type all blade air turbine (8A) organ.   A bearing (80) thrust bearing (80a) aiming at high pressure injection and large mass injection 100 to 1000 times the turbine blade cross section (4E) is provided, and the outer casing (77a) is formed as a parallel saddle type full blade air turbine (8A). Various energy storage cycle coalescence engine equipped.   A robust blade group as a parallel saddle type all-blade gas turbine (8A) by providing a bearing (80) thrust bearing (80a) aiming at high pressure injection and large mass injection 100 to 1000 times the turbine blade cross section (4E) Various energy storage cycle coalescence engine equipped.   Bearings (80) and thrust bearings (80a) aiming at high pressure injection and large mass injection 100 to 1000 times the turbine blade cross section (4E) are provided to expand the blade group spacing as a parallel saddle type all blade gas turbine (8A) Various energy storage cycle coalescence engine equipped.   Bearing (80) thrust bearing (80a) aiming at high pressure injection and large mass injection 100 to 1000 times the turbine blade cross section (4E) is provided, and the turbine blade interval is expanded as a parallel saddle type full blade air turbine (8A). Various energy conservation cycle coalescence engine.   Bearing (80) thrust bearing (80a) aiming at high pressure injection and large mass injection 100 to 1000 times the turbine blade cross section (4E) is provided to increase turbine blade strength as a parallel saddle type all-blade gas turbine (8A) Various energy conservation cycle coalescence engine.   Bearing (80) thrust bearing (80a) aiming at high pressure injection and large mass injection 100 to 1000 times the turbine blade cross section (4E) is provided to increase the strength of the blade group as a parallel saddle type all blade gas turbine (8A) Various energy storage cycle coalescence engine equipped.   A bearing (80) thrust bearing (80a) aiming at high pressure injection and large mass injection 100 to 1000 times the turbine blade cross section (4E) is provided to increase the strength of the inner shaft device as a parallel saddle type full blade air turbine (8A) Various energy storage cycle coalescence engine equipped.   A bearing (80) thrust bearing (80a) aiming at high pressure injection and large mass injection 100 to 1000 times the turbine blade cross section (4E) is provided to increase the strength of the outer shaft device as a parallel saddle type full blade air turbine (8A) Various energy storage cycle coalescence engine equipped.   A bearing (80) thrust bearing (80a) aiming at high-pressure injection and large-mass injection 100 to 1000 times the turbine blade cross section (4E) is provided, and the outer casing (77a) is used as an opposed in-series full blade impeller gas turbine (8a). Various energy storage cycle coalescence engine equipped.   Bearing (80) thrust bearing (80a) aiming at high pressure injection and large mass injection 100 to 1000 times the turbine blade cross section (4E) is provided, and a robust turbine blade is provided as an opposed series full blade impeller gas turbine (8a). Various energy conservation cycle coalescence engine.   Bearing (80) thrust bearing (80a) aiming at high pressure injection and large mass injection 100 to 1000 times the turbine blade cross section (4E) is provided, and the turbine blade strength is increased as an opposed series full blade impeller gas turbine (8a). Various energy conservation cycle coalescence engine.   Various energy storage cycle coalescing engines provided with a bearing (80) thrust bearing (80a) aiming for a 910,000-fold work rate of the turbine blade cross section (4D) to form a series vertical all-blade water turbine (8B).   Various energy storage cycles provided with a bearing (80) thrust bearing (80a) aiming for a 910,000-fold work rate of the turbine blade cross section (4D) and having an outer casing (77a) as a series vertical-type all blade water turbine (8B) Combined organization.   Various energy conservation cycles provided with bearings (80) and thrust bearings (80a) aiming for a 910,000-fold work rate of the turbine blade cross section (4D) and having a robust blade group as a series vertical all blade water turbine (8B) Combined organization.   Various energy conservation cycles provided with a bearing (80) thrust bearing (80a) aiming at 910,000 times the power of the turbine blade cross section (4D) and expanding the blade group spacing as a series vertical all blade water turbine (8B) Combined organization.   Combined with various energy conservation cycles with a turbine bearing (80) thrust bearing (80a) aiming for a 910,000-fold work rate of the turbine blade cross section (4D) and an increased turbine blade spacing as a series vertical bladed water turbine (8B) organ.   Combined with various energy conservation cycles equipped with a bearing (80) thrust bearing (80a) aiming for a 910,000-fold work rate of the turbine blade cross section (4D) and increasing the turbine blade strength as a series vertical type full-blade water turbine (8B) organ.   Various energy conservation cycles equipped with a bearing (80) thrust bearing (80a) aiming at 910,000 times the power of the turbine blade cross section (4D) and increasing the strength of the blade group as a series vertical all blade water turbine (8B) Combined organization.   Various energy conservation cycles equipped with a bearing (80) thrust bearing (80a) aiming at 910,000 times the power of the turbine blade cross section (4D) and increasing the strength of the inner shaft device as a series vertical bladed water turbine (8B) Combined organization.   Various energy conservation cycles equipped with a bearing (80) thrust bearing (80a) aiming at 910,000 times the power of the turbine blade cross section (4D) and increasing the strength of the outer shaft device as a series vertical bladed water turbine (8B) Combined organization.   Combined with various energy storage cycles provided with a bearing (80) thrust bearing (80a) aiming at 910,000 times the power of the turbine blade cross section (4D) and having an outer casing (77a) as a series full blade impeller water turbine (8b) organ.   Various energy conservation cycle coalescence engines equipped with a solid turbine blade (8b) provided with a bearing (80) thrust bearing (80a) aiming at 910,000 times the work rate of the turbine blade cross section (4D) .   Various energy storage cycle coalescence engines provided with a bearing (80) thrust bearing (80a) aiming at 910,000 times the power of the turbine blade cross section (4D) and increasing the turbine blade strength as a series full blade impeller water turbine (8b) .   Various energy storage cycle coalescing engines provided with a bearing (80) thrust bearing (80a) aiming at a work of 1.65 million times the turbine blade cross section (4D) and used as a series vertical all blade mercury turbine (8H).   Various energy storage cycles provided with a bearing (80) thrust bearing (80a) aiming at a work of 1.65 million times the turbine blade cross section (4D) and having an outer casing (77a) as a series vertical type all blade mercury turbine (8H) Combined organization.   Various energy storage cycles equipped with a robust blade group as a series vertical all blade mercury turbine (8H) provided with a bearing (80) thrust bearing (80a) aiming at a work of 1.65 million times the turbine blade cross section (4D) Combined organization.   Various energy conservation cycles equipped with a bearing (80) thrust bearing (80a) aiming at a work of 1.65 million times the turbine blade cross-section (4D), and expanding the blade group spacing as a series vertical all-blade mercury turbine (8H) Combined organization.   Combined with various energy storage cycles, with a turbine blade cross section (4D) with a bearing aiming at a work rate of 1.65 million times (80) and a thrust bearing (80a), and a turbine blade spacing as a series vertical all blade mercury turbine (8H). organ.   Combined with various energy storage cycles equipped with a bearing (80) thrust bearing (80a) aiming at 1.65 million times power of the turbine blade cross section (4D) and increasing the turbine blade strength as a series vertical type full-blade mercury turbine (8H) organ.   Various energy conservation cycles equipped with a bearing (80) thrust bearing (80a) aiming for a work of 1.65 million times the turbine blade cross section (4D) and increasing the strength of the blade group as a series vertical all blade mercury turbine (8H) Combined organization.   Various energy conservation cycles equipped with a bearing (80) thrust bearing (80a) aiming at a work of 1.65 million times the turbine blade cross section (4D) and increasing the strength of the inner shaft device as a series vertical type full-blade mercury turbine (8H) Combined organization.   Various energy storage cycles provided with a bearing (80) thrust bearing (80a) aiming at a work of 1.65 million times the turbine blade cross section (4D) and increasing the strength of the outer shaft device as a series vertical full blade mercury turbine (8H) Combined organization.   Combined with various energy storage cycles provided with a bearing (80) thrust bearing (80a) aiming at a work of 1.65 million times the turbine blade cross section (4D) and having an outer casing (77a) as a series full blade impeller mercury turbine (8E) organ.   Various energy storage cycle coalescing engines equipped with a solid turbine blade (8E) provided with a bearing (80) thrust bearing (80a) aiming for a work of 1.65 million times the turbine blade cross section (4D) .   Various energy storage cycle coalescing engines provided with a bearing (80) thrust bearing (80a) aiming at a work of 1.65 million times the turbine blade cross section (4D), and increasing the turbine blade strength as a series full blade impeller mercury turbine (8E) .   Combined with various energy conservation cycles by providing a bearing (80) thrust bearing (80a) aiming at high pressure injection and large mass injection 100 to 1000 times the turbine blade cross section (4E) to form a serial vertical all blade gas turbine (8A) organ.   A bearing (80) thrust bearing (80a) aiming at high-pressure injection and large-mass injection 100 to 1000 times the turbine blade cross section (4E) is provided, and the outer casing (77a) is formed as a series vertical all-blade gas turbine (8A). Various energy storage cycle coalescence engine equipped.   A robust blade group as a series vertical all-blade gas turbine (8A) by providing a bearing (80) thrust bearing (80a) aiming at high pressure injection and large mass injection 100 to 1000 times the turbine blade cross section (4E) Various energy storage cycle coalescence engine equipped.   Bearings (80) and thrust bearings (80a) aiming at high pressure injection and large mass injection 100 to 1000 times the turbine blade cross section (4E) are provided to expand the interval between the blade groups as a series vertical all-blade gas turbine (8A) Various energy storage cycle coalescence engine equipped.   Bearing (80) thrust bearing (80a) aiming at high pressure injection and large mass injection 100 to 1000 times the turbine blade cross section (4E) is provided, and the turbine blade interval is expanded as a series vertical type full blade air turbine (8A). Various energy conservation cycle coalescence engine.   Bearing (80) thrust bearing (80a) aiming at high pressure injection and large mass injection 100 to 1000 times the turbine blade cross section (4E) is provided to increase turbine blade strength as a series vertical type full blade air turbine (8A) Various energy conservation cycle coalescence engine.   Bearing (80) thrust bearing (80a) aiming at high pressure injection and large mass injection 100 to 1000 times the turbine blade cross section (4E) is provided to increase the strength of the blade group as a series vertical type all blade gas turbine (8A) Various energy storage cycle coalescence engine equipped.   A bearing (80) thrust bearing (80a) aiming at high pressure injection and large mass injection 100 to 1000 times the turbine blade cross section (4E) is provided to increase the strength of the inner shaft device as a series vertical type full blade air turbine (8A) Various energy storage cycle coalescence engine equipped.   A bearing (80) thrust bearing (80a) aiming at high pressure injection and large mass injection 100 to 1000 times the turbine blade cross section (4E) is provided to increase the strength of the outer shaft device as a series vertical type full blade air turbine (8A) Various energy storage cycle coalescence engine equipped.   A bearing (80) thrust bearing (80a) aiming at high pressure injection and large mass injection 100 to 1000 times the turbine blade cross section (4E) is provided, and an outer casing (77a) is provided as a serial all blade impeller gas turbine (8a). Various energy conservation cycle coalescence engine.   The bearing (80) thrust bearing (80a) aiming at high pressure injection and large mass injection 100 to 1000 times the turbine blade cross section (4E) is provided, and a robust turbine blade is provided as a series full blade impeller gas turbine (8a). Various energy conservation cycle coalescence engine.   Bearing (80) thrust bearing (80a) aiming at 100 to 1000 times high pressure injection and large mass injection of turbine blade cross section (4E) is provided to increase turbine blade strength as a series full blade impeller gas turbine (8a). Various energy conservation cycle coalescence engine.   Combined engine of various energy conservation cycles corresponding to high pressure injection of 100 to 1000 times by integrally casting the cylindrical body (8e) and turbine blade (8c) of the serial all blade impeller gas turbine (8a) of the turbine blade cross section (4E). .   Combined engine of various energy conservation cycles corresponding to high pressure injection of 10 to 100 times by integrally processing the cylindrical body (8e) and turbine blade (8c) of the serial all-blade propeller wheel gas turbine (8a) of the turbine blade cross section (4E). .   Cylindrical barrel (8e) and turbine blades (8c) of a series all-blade propeller wheel gas turbine (8a) with a turbine blade cross section (4E), and various energy corresponding to 100 to 1000 times high pressure injection and large mass injection Conservation cycle coalescence organization.   Cylindrical barrel (8e) and turbine blades (8c) of an in-series all blade impeller gas turbine (8a) having a turbine blade cross section (4E) are integrally cast and integrally processed so that various energies corresponding to 10 to 100 times high pressure injection and large mass injection are obtained. Conservation cycle coalescence organization.   Combined with various energy storage cycles corresponding to high pressure injection of 100 to 1000 times by integrally casting the cylindrical body (8e) and turbine blade (8c) of the opposed series full blade impeller gas turbine (8a) of the turbine blade cross section (4E) organ.   Combined with various energy storage cycles corresponding to 10 to 100 times high pressure injection by integrally casting the cylindrical body (8e) and turbine blade (8c) of the opposed series full blade impeller gas turbine (8a) of the turbine blade cross section (4E). organ.   Various types of high pressure injection and large mass injection of 100 to 1000 times by integrally casting the cylindrical body (8e) and turbine blade (8c) of the opposed series full blade impeller gas turbine (8a) of the turbine blade cross section (4E). Energy conservation cycle coalescence engine.   Cylindrical body (8e) and turbine blade (8c) of opposed series full blade impeller gas turbine (8a) with a turbine blade cross-section (4E) Energy conservation cycle coalescence engine.   Various energy conservation cycle coalescence engines corresponding to 910,000 times work rate by integrally casting the cylindrical body (8e) and turbine blade (8c) of the opposed series full blade impeller water turbine (8b) of the turbine blade cross section (4E).   Various energy storage cycles corresponding to the addition of 910,000 times power gravity acceleration by integrally casting the cylindrical body (8e) and turbine blade (8c) of the opposed series full blade impeller water turbine (8b) of the turbine blade cross section (4E). Combined organization.   Turbine blade cross-section (4E) opposed in series all blade impeller water turbine (8b) cylindrical body (8e) turbine blade (8c) is integrally cast and integrated, 910,000 times power gravitational acceleration 9.8m / second per second added Various energy conservation cycle coalescing engines.   Various energy storage cycle coalescing engines capable of adding gravity acceleration by integrally casting the cylindrical body (8e) and turbine blade (8c) of the opposed series full blade impeller water turbine (8b) of the turbine blade cross section (4E).   Various types of energy storage corresponding to the addition of gravity acceleration of 9.8 m / sec per second by integrally casting the cylindrical body (8e) and turbine blade (8c) of the opposed series full blade impeller water turbine (8b) of the turbine blade cross section (4E) Cycle coalescence engine.   Various energy storage cycle coalescence engines corresponding to a large output by integrally casting the cylindrical body (8e) and the turbine blade (8c) of the opposed series full blade impeller water turbine (8b) of the turbine blade cross section (4E).   Various energy storage cycle coalescing engines in which the cylindrical body (8e) and turbine blades (8c) of the opposed in-series full blade impeller water turbine (8b) of the turbine blade cross section (4E) are made as a single body by integral casting.   Various energy storage cycle coalescence engines corresponding to 910,000 times power by integrally casting the cylindrical body (8e) and turbine blades (8c) of the series all blade impeller water turbine (8b) of the turbine blade cross section (4E).   Combined with various energy conservation cycles corresponding to the addition of 910,000 times power gravitational acceleration by integrally casting the cylindrical body (8e) and turbine blade (8c) of the series all blade impeller water turbine (8b) of the turbine blade cross section (4E) organ.   Turbine blade cross-section (4E) series all blade impeller water turbine (8b) cylindrical body (8e) Turbine blade (8c) is integrally cast and integrated, 910,000 times power gravitational acceleration 9.8m / second per second added Various energy conservation cycle coalescence engine.   Various energy conservation cycle coalescing engines corresponding to the addition of gravitational acceleration by integrally casting the cylindrical body (8e) and turbine blade (8c) of the in-series full blade impeller water turbine (8b) of the turbine blade cross section (4E).   Cylindrical body (8b) cylindrical body (8e) turbine blade (8c) of in-series full blade moving turbine water turbine (8b) with turbine blade cross section (4E) integrated casting and machining, various energy storage cycles corresponding to gravity acceleration of 9.8 m / second per second addition Combined organization.   Various energy storage cycle coalescing engines corresponding to a large output by integrally casting the cylindrical body (8e) and the turbine blade (8c) of the serial all blade impeller water turbine (8b) of the turbine blade cross section (4E).   Various energy storage cycle coalescing engines in which the cylindrical body (8e) and turbine blades (8c) of the series all-blade propeller turbine water turbine (8b) having a turbine blade cross section (4E) are integrally cast and made to have high strength.   Various energy storage cycle coalescence engine corresponding to 910,000 times power by integrally casting and integrally processing the inner shaft device (60A) of a parallel vertical type all-blade water turbine (8B) with turbine blade cross section (4E) .   Various energy conservation corresponding to the addition of gravity acceleration of 910,000 times as integral casting integrated processing of the inner shaft device (60A) of the parallel vertical type all-blade water turbine (8B) with turbine blade cross section (4E) Cycle coalescence engine.   910,000 times power gravitational acceleration 9.8m / sec added per second as integral casting integrated machining of parallel vertical type all-blade water turbine (8B) inner shaft device (60A) with turbine blade cross section (4E) Various energy conservation cycle coalescing engines corresponding to.   Various energy storage cycle coalescing engines that support the addition of gravitational acceleration by integrally casting the parallel vertical type all-blade water turbine (8B) inner shaft device (60A) of the turbine blade cross section (4E) as a single unit of the blade group.   Various energies corresponding to the addition of 9.8m / s / s per second by integrally casting and integrally processing the inner shaft device (60A) of the parallel vertical type all-blade water turbine (8B) with turbine blade cross section (4E) in units of rotor blade groups Conservation cycle coalescence organization.   Various energy storage cycle coalescing engines corresponding to a large output by integrally casting and integrally processing the inner shaft device (60A) of the parallel saddle type all-blade water turbine (8B) having a turbine blade cross section (4E) in units of rotor blade rows.   Various energy storage cycle coalescing engines in which a parallel vertical type all-blade water turbine (8B) inner shaft device (60A) having a turbine blade cross section (4E) is integrally cast and integrally processed in units of rotor blade groups.   Combined engine with various energy conservation cycles corresponding to 910,000 times higher work by integrally casting integral series of all-blade water turbine (8B) inner shaft device (60A) with turbine blade cross section (4E) in units of moving blade groups .   Various types of energy storage corresponding to gravity acceleration addition of 910,000 times as integral casting integrated machining of the inner shaft device (60A) of the series vertical type water turbine (8B) inner turbine device (60A) of the turbine blade cross section (4E) Cycle coalescence engine.   Turbine blade cross section (4E) in-line vertical all-blade water turbine (8B) inner shaft device (60A) is integrally cast and integrated in units of rotor blade groups, and 910,000 times power gravitational acceleration 9.8m / sec added per second Various energy conservation cycle coalescing engines corresponding to   Various energy storage cycle coalescing engines that support the addition of gravitational acceleration by integrally casting a series vertical type all-blade water turbine (8B) inner shaft device (60A) having a turbine blade cross section (4E) in a unit of a blade group.   Various types of energy corresponding to the addition of gravity acceleration of 9.8 m / second per second by integrally casting and integrally processing the inner shaft device (60A) of the series vertical type all-blade water turbine (8B) with turbine blade cross section (4E) in units of rotor blade groups Conservation cycle coalescence organization.   Various energy storage cycle coalescing engines corresponding to a large output by integrally casting a series vertical type all-blade water turbine (8B) inner shaft device (60A) having a turbine blade cross section (4E) in a unit of a blade group.   Various energy storage cycle coalescing engines in which the turbine blade cross section (4E) in-line vertical all-blade water turbine (8B) inner shaft device (60A) is integrally cast and integrally processed in units of blade groups.   Various energy storage cycle coalescence engine corresponding to 910,000 times work rate by integrally casting and integrally processing the outer shaft device (60B) of the parallel vertical type all-blade water turbine (8B) with turbine blade cross section (4E) .   Various energy conservation corresponding to the addition of gravitational acceleration of 910,000 times as a unitary casting integrated processing of a parallel vertical type all-blade water turbine (8B) outer shaft device (60B) of turbine blade cross section (4E) in units of moving blade groups Cycle coalescence engine.   A 910,000 times power gravitational acceleration of 9.8 m / sec is added per second as an integral casting and integrated machining of a turbine blade cross section (4E) parallel vertical all-blade water turbine (8B) outer shaft device (60B) in units of moving blade groups. Various energy conservation cycle coalescing engines corresponding to.   Various energy conservation cycle coalescing engines that support the addition of gravitational acceleration by integrally casting and integrally processing the outer shaft device (60B) of the parallel saddle type all-blade water turbine (8B) with the turbine blade cross section (4E) in units of rotor blade rows.   Various energies corresponding to the addition of 9.8m / s / s per second by integrally casting the parallel vertical type all-blade water turbine (8B) outer shaft device (60B) of the turbine blade cross section (4E) as a single unit in a single blade group row Conservation cycle coalescence organization.   Various energy storage cycle coalescing engines corresponding to a large output by integrally casting the parallel vertical type all-blade water turbine (8B) outer shaft device (60B) of the turbine blade cross section (4E) in a unitary blade group row.   Various energy conservation cycle coalescing engines in which a parallel vertical type all-blade water turbine (8B) outer shaft device (60B) having a turbine blade cross section (4E) is integrally cast and integrally processed in units of blade groups.   Combined engine with various energy conservation cycles corresponding to 910,000 times power by integrally casting a single blade type all-blade water turbine (8B) outer shaft device (60B) with a turbine blade cross section (4E) as a single unit in a single blade group row .   Various types of energy storage corresponding to gravity acceleration addition of 910,000 times as integral casting integrated machining of series blade type all rotor blade water turbine (8B) outer shaft device (60B) of turbine blade cross section (4E) for each blade group row Cycle coalescence engine.   Turbine blade cross section (4E) in-line vertical all-blade water turbine (8B) outer shaft device (60B) is integrally cast and integrated in units of rotor blade groups, and 910,000-fold power gravitational acceleration 9.8 m / second per second is added Various energy conservation cycle coalescing engines corresponding to.   Various energy storage cycle coalescing engines that support the addition of gravitational acceleration by integrally casting the series vertical type all-blade water turbine (8B) outer shaft device (60B) of the turbine blade cross section (4E) as a unit of the blade group.   Various energies corresponding to the addition of gravity acceleration of 9.8 m / second per second by integrally casting and integrally processing the vertical shaft type all-blade water turbine (8B) outer shaft device (60B) of the turbine blade cross section (4E) in units of blade groups Conservation cycle coalescence organization.   Various energy storage cycle coalescing engines that support large output by integrally casting and integrally processing a series blade-type all-blade water turbine (8B) outer shaft device (60B) having a turbine blade cross section (4E) in units of rotor blade groups.   Various energy conservation cycle coalescing engines in which the turbine blade cross section (4E) series vertical all-blade water turbine (8B) outer shaft device (60B) is integrally cast and integrally processed in units of blade groups.   Combined engine with various energy conservation cycles corresponding to a work rate of 1.65 million times by integrally casting a single vertical all blade mercury turbine (8H) inner shaft device (60A) with a turbine blade cross section (4E) as a single unit of the blade group. .   Various types of energy storage corresponding to the addition of 1.65 million times power gravitational acceleration by integrally casting and integrally processing the inner shaft device (60A) of a parallel vertical type all-blade mercury turbine (8H) with turbine blade cross section (4E) Cycle coalescence engine.   Turbine blade cross section (4E) parallel saddle type all blade mercury turbine (8H) inner shaft device (60A) is integrally cast and integrally processed in units of blade groups and added 16.5 million times power gravitational acceleration 9.8m / second per second Various energy conservation cycle coalescing engines corresponding to   Various energy storage cycle coalescing engines that support the addition of gravitational acceleration by integrally casting a single vertical all-blade mercury turbine (8H) inner shaft device (60A) with a turbine blade cross section (4E) as a single unit for a single blade group.   Various energies corresponding to the addition of gravity acceleration of 9.8 m / sec per second by integrally casting and integrally processing the inner shaft device (60A) of the parallel vertical type all-blade mercury turbine (8H) with turbine blade cross section (4E) in units of moving blade groups Conservation cycle coalescence organization.   Various energy storage cycle coalescing engines that support large output by integrally casting and integrally processing the inner shaft device (60A) of a parallel vertical type all-blade mercury turbine (8H) having a turbine blade section (4E) in units of rotor blade groups.   Various energy conservation cycle coalescing engines in which a parallel vertical type all-blade mercury turbine (8H) inner shaft device (60A) having a turbine blade cross section (4E) is integrally cast and integrally processed in units of blade groups.   Combined engine with various energy storage cycles corresponding to a work rate of 16.5 million times by integrally casting a single vertical type all-blade mercury turbine (8H) inner shaft device (60A) with a turbine blade cross section (4E) as a unit of a single blade group .   Various types of energy storage corresponding to the addition of gravity acceleration of 1.65 million times by integrally casting the inner shaft device (60A) of the series vertical-type all-blade mercury turbine (8H) with turbine blade cross-section (4E) as a single unit of the blade group. Cycle coalescence engine.   Turbine blade cross section (4E) series vertical all-blade mercury turbine (8H) inner shaft device (60A) is integrally cast and integrally processed in units of blade groups, adding 16.5 million times power gravitational acceleration 9.8m / sec per second Various energy conservation cycle coalescing engines corresponding to.   Various energy storage cycle coalescing engines that support the addition of gravitational acceleration by integrally casting a single vertical all-blade mercury turbine (8H) inner shaft device (60A) with a turbine blade cross-section (4E) as a single unit for each blade group.   Various energies corresponding to the addition of gravity acceleration of 9.8 m / sec per second by integrally casting the inner shaft device (60A) of the series vertical type all-blade mercury turbine (8H) with turbine blade cross section (4E) in units of moving blade groups Conservation cycle coalescence organization.   Various energy storage cycle coalescing engines capable of large output by integrally casting and integrally processing the inner shaft device (60A) of the series vertical type all-blade mercury turbine (8H) with turbine blade cross section (4E) in units of rotor blade rows.   Various energy storage cycle coalescence engines in which the turbine blade cross section (4E) in-line vertical all-blade turbine (8H) inner shaft device (60A) is integrally cast and integrally processed in units of blade groups.   Combined engine with various energy conservation cycles corresponding to a work of 1.65 million times by integrally casting a single vertical all blade mercury turbine (8H) outer shaft device (60B) with a turbine blade cross section (4E) as a single unit of the blade group. .   Various types of energy storage corresponding to the addition of 16.5 million times the work gravity acceleration by integrally casting and integrally processing the outer shaft device (60B) of the parallel vertical type all-blade mercury turbine (8H) with turbine blade cross section (4E) Cycle coalescence engine.   Turbine blade cross section (4E) parallel saddle type full-blade mercury turbine (8H) outer shaft device (60B) is integrally cast and integrally processed in units of rotor blade groups. Various energy conservation cycle coalescing engines corresponding to   Various energy storage cycle coalescing engines that support the addition of gravitational acceleration by integrally casting and integrally processing a parallel vertical type all-blade mercury turbine (8H) outer shaft device (60B) having a turbine blade cross section (4E) in units of rotor blade groups.   Various energies corresponding to the addition of gravity acceleration of 9.8 m / sec per second by integrally casting and integrally processing the outer shaft device (60B) of the parallel vertical type all-blade mercury turbine (8H) with turbine blade cross section (4E) in units of moving blade groups Conservation cycle coalescence organization.   Various energy storage cycle coalescing engines capable of large output by integrally casting and integrally processing the outer shaft device (60B) of the parallel vertical type all-blade mercury turbine (8H) with turbine blade cross section (4E) in units of rotor blade rows.   Various energy conservation cycle coalescing engines in which a parallel vertical type all blade mercury turbine (8H) outer shaft device (60B) having a turbine blade cross section (4E) is integrally cast and integrally processed in units of blade groups.   Combined engine with various energy storage cycles corresponding to a work rate of 1.65 million times by integrally casting a single vertical all-blade mercury turbine (8H) outer shaft device (60B) with a turbine blade cross section (4E) as a single unit of a single blade group. .   Various types of energy storage corresponding to the addition of 16.5 million times power gravitational acceleration by integrally casting the turbine blade cross-section (4E) series vertical type full-blade mercury turbine (8H) outer shaft device (60B) as a single unit for each blade group. Cycle coalescence engine.   Turbine blade cross-section (4E) series vertical all-blade turbine (8H) outer shaft device (60B) is integrally cast and integrated in units of rotor blade groups, and increased by 16.5 million times, gravity acceleration 9.8m / second per second Various energy conservation cycle coalescing engines corresponding to   Various energy storage cycle coalescing engines that support the addition of gravitational acceleration by integrally casting and integrally processing a series vertical type all-blade mercury turbine (8H) outer shaft device (60B) having a turbine blade cross section (4E) in units of rotor blade groups.   Various types of energy corresponding to the addition of gravity acceleration of 9.8 m / sec per second by integrally casting and integrally casting the series vertical type all-blade mercury turbine (8H) outer shaft device (60B) with turbine blade cross section (4E) in units of moving blade groups Conservation cycle coalescence organization.   Various energy storage cycle coalescing engines that support large output by integrally casting and integrally processing a series vertical type all-blade mercury turbine (8H) outer shaft device (60B) having a turbine blade cross section (4E) in units of rotor blade groups.   Various energy storage cycle coalescing engines in which the turbine blade cross section (4E) in-line vertical all-blade mercury turbine (8H) outer shaft device (60B) is integrally cast and integrated into a single unit for each blade group.   Various energy storage cycles corresponding to high pressure injection of 100 to 1000 times by integrally casting and integrally processing the inner shaft device (60A) of the parallel saddle type all-blade gas turbine (8A) with turbine blade cross section (4E) in units of rotor blade groups Combined organization.   Various energy storage cycles corresponding to 10 to 100 times high-pressure injection by integrally casting a single vertical all-blade gas turbine (8A) inner shaft device (60A) with a turbine blade cross section (4E) as a unitary casting unit for each blade group row Combined organization.   The turbine blade cross section (4E) parallel saddle-type all-blade gas turbine (8A) inner shaft device (60A) is integrally cast and integrated in units of rotor blade groups to support 100 to 1000 times high pressure injection and large mass injection Various energy conservation cycle coalescence engine.   The turbine blade cross section (4E) parallel saddle-type all-blade gas turbine (8A) inner shaft device (60A) is integrally cast and integrated for each blade group to support 10 to 100 times high pressure injection and large mass injection. Various energy conservation cycle coalescence engine.   Various energies corresponding to the addition of gravity acceleration of 9.8 m / sec per second by integrally casting and integrally processing the inner shaft device (60A) of the parallel saddle type all-blade gas turbine (8A) with turbine blade cross section (4E) Conservation cycle coalescence organization.   Various energy storage cycle coalescing engines capable of large output by integrally casting and integrally processing the inner shaft device (60A) of the parallel saddle type all-blade gas turbine (8A) with turbine blade cross section (4E) in units of rotor blade groups.   Various energy storage cycle coalescing engines in which a parallel saddle type all-blade gas turbine (8A) inner shaft device (60A) having a turbine blade cross section (4E) is integrally cast and integrally processed in units of blade groups.   Various energy storage cycles corresponding to high pressure injection of 100 to 1000 times by integrally casting and integrally processing the inner shaft device (60A) of the series vertical type all-blade gas turbine (8A) with turbine blade cross section (4E) in units of rotor blade groups Combined organization.   Various energy storage cycles corresponding to high-pressure injection 10 to 100 times by integrally casting and integrally processing the inner shaft device (60A) of the series vertical type all-blade gas turbine (8A) with turbine blade cross section (4E) in units of rotor blade groups Combined organization.   The turbine blade cross section (4E) in-line vertical all-blade gas turbine (8A) inner shaft device (60A) is integrally cast and integrated in units of rotor blade rows to support 100 to 1000 times high pressure injection and large mass injection Various energy conservation cycle coalescence engine.   The turbine blade cross section (4E) in-line vertical all-blade gas turbine (8A) inner shaft device (60A) is integrally cast and integrated in units of blade groups, and supports 10 to 100 times high pressure injection and large mass injection. Various energy conservation cycle coalescence engine.   Various energies corresponding to the addition of gravity acceleration of 9.8 m / second per second by integrally casting and integrally processing the inner shaft device (60A) of the series vertical type gas turbine (8A) inner turbine unit (60A) of the turbine blade cross section (4E). Conservation cycle coalescence organization.   Various energy storage cycle coalescing engines capable of large output by integrally casting and integrally processing a series vertical type all-blade gas turbine (8A) inner shaft device (60A) of turbine blade cross section (4E) in units of rotor blade groups.   Various energy storage cycle coalescing engines in which a series blade type all-blade gas turbine (8A) inner shaft device (60A) having a turbine blade cross section (4E) is integrally cast and integrally processed in units of blade groups.   Various energy storage cycles corresponding to high pressure injection of 100 to 1000 times by integrally casting and integrally processing the outer shaft device (60A) of the parallel saddle type full blades turbine turbine (8A) of the turbine blade cross section (4E) in units of blade groups. Combined organization.   Various energy storage cycles corresponding to high pressure injection of 10 to 100 times by integrally casting and integrally processing the outer shaft device (60A) of parallel saddle type all blades gas turbine (8A) with turbine blade cross section (4E) in units of rotor blade groups. Combined organization.   The turbine blade cross section (4E) parallel saddle-type all-blade gas turbine (8A) outer shaft device (60A) is integrally cast and integrated for each blade group to support 100 to 1000 times high pressure injection and large mass injection. Various energy conservation cycle coalescence engine.   The turbine blade cross section (4E) parallel saddle-type all-blade gas turbine (8A) outer shaft device (60A) is integrally cast and integrated for each blade group, and supports 10 to 100 times high pressure injection and large mass injection. Various energy conservation cycle coalescence engine.   Various energies corresponding to the addition of gravity acceleration of 9.8 m / sec per second by integrally casting and integrally processing the outer shaft device (60A) of the parallel saddle type all-blade gas turbine (8A) with turbine blade cross section (4E) in units of moving blade groups Conservation cycle coalescence organization.   Various energy storage cycle coalescing engines corresponding to a large output by integrally casting the parallel vertical type all-blade gas turbine (8A) outer shaft device (60A) of the turbine blade cross section (4E) in a unit of a blade group.   Various energy storage cycle coalescing engines in which the parallel vertical type all-blade gas turbine (8A) outer / inner shaft device (60A) having a turbine blade cross section (4E) is integrally cast and integrally processed in units of moving blade groups.   Various energy storage cycles corresponding to high pressure injection of 100 to 1000 times by integrally casting and integrally processing the outer shaft device (60A) of the series vertical type full-rotor blade turbine turbine (8A) with turbine blade cross section (4E) in units of rotor blade groups. Combined organization.   Various energy storage cycles corresponding to high pressure injection 10 to 100 times by integrally casting and integrally processing an outer shaft device (60A) of a series vertical type full-blade gas turbine (8A) having a turbine blade cross section (4E) in units of rotor blade rows. Combined organization.   The turbine blade cross section (4E) series vertical type full-blade gas turbine (8A) outer shaft device (60A) is integrally cast and integrated in units of blade groups to support 100 to 1000 times high pressure injection and large mass injection. Various energy conservation cycle coalescence engine.   The turbine blade cross section (4E) series vertical type full-blade gas turbine (8A) outer shaft device (60A) is integrally cast and integrated in units of rotor blade groups to support 10 to 100 times high pressure injection and large mass injection. Various energy conservation cycle coalescence engine.   Various types of energy corresponding to the addition of gravity acceleration of 9.8 m / sec per second by integrally casting the series vertical type all-blade gas turbine (8A) outer shaft device (60A) of the turbine blade cross section (4E) in a unit of the blade group Conservation cycle coalescence organization.   Various energy storage cycle coalescing engines capable of large output by integrally casting and integrally processing the outer shaft device (60A) of the series vertical type all-blade gas turbine (8A) having a turbine blade cross section (4E) in units of rotor blade groups.   Various energy conservation cycle coalescing engines in which the turbine blade cross section (4E) in-line vertical all-blade gas turbine (8A) outer shaft device (60A) is integrally cast and integrally processed in units of blade groups.   Various energy storage cycle coalescing engines that have a turbine blade cross section (4D) full blade combustion section (32X) and aim for 200 times the rotational output of existing engines.   Various energy storage cycle coalescing engines that have a turbine blade cross section (4D) full blade combustion part (32Y) and aim for 200 times rotation output of existing engines.   Various energy storage cycle coalescing engines that have a combined engine combustion section (31X) with a turbine blade cross section (4D) and aim for a 200-fold rotational output of existing engines.   Various energy storage cycle coalescing engines that have a combined engine combustion section (31Y) with a turbine blade cross section (4D) and aim for a 200-fold rotational output of existing engines.   Various energy storage cycle coalescing engines that have a turbine blade cross section (4D) full blade combustion part (32X) and aim for 10 times the propulsion output of existing engines.   Various energy storage cycle coalescing engines that have a turbine blade cross section (4D) full blade combustion part (32Y) and aim for 10 times the propulsion output of existing engines.   Various energy storage cycle coalescence engines equipped with a combined engine combustion section (31X) with a turbine blade cross section (4D) and aiming for 10 times the injection propulsion output of existing engines.   Various energy storage cycle coalescence engines equipped with a combined engine combustion section (31Y) with a turbine blade cross section (4D) and aiming for 10 times the injection propulsion output of existing engines.   Various energy storage cycle coalescing engine with turbine blade cross section (4A).   Various energy storage cycle coalescing engine with turbine blade cross section (4B).   Various energy storage cycle coalescing engine with turbine blade cross section (4C).   Various energy storage cycle coalescing engine with turbine blade cross section (4D).   Various energy storage cycle coalescing engine with turbine blade cross section (4E).   Various energy storage cycle coalescing engine with turbine blade cross section (4F).   Various energy storage cycle coalescing engine with turbine blade cross section (4X).   Turbine blade cross section (4A) Various energy storage cycle coalescence engine equipped with vertical all blade mercury turbine (8H).   Turbine blade cross section (4B) vertical energy blade mercury turbine (8H) equipped with various energy storage cycle coalescence engine.   Turbine blade cross section (4C) Vertical energy blade mercury turbine (8H) equipped with various energy storage cycle coalescing engines.   Turbine blade cross section (4D) Combined engine with various energy storage cycles equipped with vertical type moving blade mercury turbine (8H).   Turbine blade cross section (4E) Various energy storage cycle coalescing engine equipped with vertical all blade mercury turbine (8H).   Turbine blade cross section (4F) vertical energy blade mercury turbine (8H) equipped with various energy storage cycle coalescence engine.   Turbine blade cross section (4X) vertical all-moving blade mercury turbine (8H) equipped with various energy storage cycle coalescence engine.   Turbine blade cross section (4A) Various energy storage cycle coalescing engine equipped with vertical all blade water turbine (8B).   Turbine blade cross section (4B) various energy storage cycle coalescing engine equipped with vertical all blade water turbine (8B).   Turbine blade cross section (4C) various energy storage cycle coalescing engine equipped with vertical all blade water turbine (8B).   Turbine blade cross section (4D) various energy storage cycle coalescence engine equipped with vertical all blade water turbine (8B).   Turbine blade cross-section (4E) various energy storage cycle coalescing engine equipped with a vertical all blade water turbine (8B).   Turbine blade cross section (4F) various energy storage cycle coalescing engine equipped with a vertical all blade water turbine (8B).   Turbine blade cross section (4X) vertical energy blade water turbine (8B) equipped with various energy storage cycle coalescence engine.   Turbine blade cross section (4A) Combined engine with various energy storage cycles equipped with vertical all blade gas turbine (8A).   Turbine blade cross section (4B) various energy storage cycle coalescing engine equipped with vertical all blade gas turbine (8A).   Turbine blade cross section (4C) various energy storage cycle coalescing engine equipped with vertical all blade vane turbine (8A).   Turbine blade cross section (4D) various energy storage cycle coalescing engine equipped with a vertical all blade gas turbine (8A).   Turbine blade cross section (4E) Various energy storage cycle coalescing engine equipped with vertical all blade vane gas turbine (8A).   Turbine blade cross section (4F) various energy storage cycle coalescing engine equipped with a vertical all blade gas turbine (8A).   Turbine blade cross-section (4X) various energy storage cycle coalescing engine equipped with a vertical all blade gas turbine (8A).   Turbine blade cross-section (4A) various energy storage cycle coalescing engine equipped with opposed series full blade impeller mercury turbine (8E).   Turbine blade cross section (4B) various in-line energy storage cycle coalescence engine equipped with opposed in-series full blade impeller mercury turbine (8E).   Turbine blade cross section (4C) various energy storage cycle coalescence engine equipped with opposed series full blade impeller mercury turbine (8E).   Turbine blade cross-section (4D) various energy storage cycle coalescing engine equipped with opposed series full blade impeller mercury turbine (8E).   Turbine blade cross section (4E) various energy storage cycle coalescence engine equipped with opposed series full blade impeller mercury turbine (8E).   Turbine blade cross section (4F) various energy storage cycle coalescence engine equipped with opposed in-series full blade impeller mercury turbine (8E).   Turbine blade cross section (4X) opposed series full blade impeller mercury turbine (8E) equipped with various energy conservation cycle coalescence engine.   Turbine blade cross section (4A) Series of all blade impeller mercury turbine (8E) equipped with various energy conservation cycle coalescence engines.   Turbine blade cross section (4B) in-line full blade impeller mercury turbine (8E) equipped with various energy storage cycle coalescing engines.   Turbine blade cross section (4C) Inline all blade impeller mercury turbine (8E) equipped with various energy storage cycle coalescing engines.   Turbine blade cross section (4D) All energy storage cycle coalescence engine equipped with in-line all blade impeller mercury turbine (8E).   Turbine blade cross section (4E) In-line full blade impeller mercury turbine (8E) equipped with various energy storage cycle coalescing engines.   Turbine blade cross section (4F) Inline all blade impeller mercury turbine (8E) equipped with various energy storage cycle coalescing engines.   Turbine blade cross section (4X) in-line full blade impeller mercury turbine (8E) equipped with various energy storage cycle coalescing engines.   Turbine blade cross section (4A) various energy storage cycle coalescing engines equipped with a series full blade impeller water turbine (8b).   Turbine blade cross section (4B) All energy storage cycle coalescing engine equipped with in-line full blade impeller water turbine (8b).   Turbine blade cross section (4C) various energy storage cycle coalescing engine equipped with a series all blade impeller water turbine (8b).   Turbine blade cross section (4D) various energy storage cycle coalescing engine equipped with a series full blade impeller water turbine (8b).   Turbine blade cross-section (4E) In-line full blade impeller water turbine (8b) equipped with various energy storage cycle combined engines.   Turbine blade cross section (4F) Inline all blade impeller water turbine (8b) equipped with various energy storage cycle coalescence engine.   Turbine blade cross section (4X) in-line full blade impeller water turbine (8b) equipped with various energy storage cycle coalescing engines.   Turbine blade cross section (4A) various energy storage cycle coalescing engine equipped with opposed series full blade impeller water turbine (8b).   Turbine blade cross section (4B) various energy storage cycle coalescing engine equipped with opposed series full blade impeller water turbine (8b).   Turbine blade cross section (4C) various energy storage cycle coalescing engine equipped with opposed series full blade impeller water turbine (8b).   Various energy storage cycle coalescing engines equipped with turbine blade cross section (4D) opposed in-line full blade impeller water turbine (8b).   Turbine blade cross section (4E) various energy storage cycle coalescing engine equipped with opposed series full blade impeller water turbine (8b).   Various energy storage cycle coalescing engines equipped with turbine blade cross section (4F) opposed in-line full blade impeller water turbine (8b).   Turbine blade cross section (4X) opposed series full blade impeller water turbine (8b) equipped with various energy conservation cycle coalescence engine.   Turbine blade cross section (4A) various energy storage cycle coalescing engine equipped with opposed series full blade impeller gas turbine (8a).   Turbine blade cross section (4B) various in-line energy storage cycle coalescence engine equipped with opposed in-series full blade impeller gas turbine (8a)   Turbine blade cross section (4C) various energy storage cycle coalescing engine equipped with opposed series full blade impeller gas turbine (8a).   Turbine blade cross section (4D) various energy storage cycle coalescing engine equipped with opposed in-series full blade impeller gas turbine (8a).   Turbine blade cross section (4E) various energy storage cycle coalescing engine equipped with opposed series full blade impeller gas turbine (8a).   Turbine blade cross section (4F) various energy storage cycle coalescing engine equipped with opposed in-series full blade impeller gas turbine (8a).   Turbine blade cross section (4X) opposed in-series full blade impeller gas turbine (8a) equipped with various energy storage cycle combined engines.   Turbine blade cross section (4A) Series of all blade impeller gas turbine (8a) equipped with various energy storage cycle coalescing engines.   Turbine blade cross section (4B) In-line all blade impeller gas turbine (8a) equipped with various energy storage cycle combined engines.   Turbine blade cross section (4C) In-line all blade impeller gas turbine (8a) equipped with various energy storage cycle combined engines.   Turbine blade cross section (4D) various energy storage cycle coalescing engines equipped with in-line full blade impeller gas turbine (8a).   Turbine blade cross-section (4E) In-line all blade impeller gas turbine (8a) equipped with various energy storage cycle combined engines.   Turbine blade cross-section (4F) In-line all blade impeller gas turbine (8a) equipped with various energy storage cycle combined engines.   Turbine blade cross section (4X) in-line full blade impeller gas turbine (8a) equipped with various energy storage cycle coalescing engines.   Vertical bearing blade mercury turbine (8H), vertical rotor blade water turbine (8B), vertical rotor blade gas turbine (8A), bearing (80) thrust bearing (80a) between outer casing (77a) Combined engine of various energy storage cycles equipped with a heavy reversal magnetic friction power transmission device (84) and a counter reversal power device (84Y).   A bearing (80) thrust bearing (80a) counter-rotating magnetic friction power transmission device (84) between the vertical all blade water turbine (8B) or the vertical all blade gas turbine (8A) and the outer casing (77a) Various energy storage cycle coalescence engine equipped with heavy reversing power unit (84Y).   A bearing (80) thrust bearing (80a) counter-rotating magnetic friction power transmission device (84) is provided between the vertical all blade water turbine (8B) or the vertical all blade gas turbine (8A) and the outer casing (77a). Various energy storage cycle coalescence engine equipped.   Various types of bearings (80) thrust bearing (80a) counter-rotating power unit (84Y) between vertical type full-blade water turbine (8B), vertical type full-blade gas turbine (8A) and outer casing (77a) Energy conservation cycle coalescence engine.   Various energy storage cycle coalescing engines comprising a bearing (80), a thrust bearing (80a) and a counter-rotating power unit (84Y) between the vertical all blade gas turbine (8A) and the outer box (77a).   Various energy storage cycle coalescing engines provided with a bearing (80) thrust bearing (80a) counter-rotating magnetic frictional power transmission device (84) between the vertical all blade gas turbine (8A) and the outer casing (77a).   Various energy storage cycle coalescing engines having a bearing (80), a thrust bearing (80a) and a counter-rotating power unit (84Y) between the vertical all-blade water turbine (8B) and the outer casing (77a).   Various energy storage cycle coalescing engines provided with a bearing (80) thrust bearing (80a) counter-rotating magnetic friction power transmission device (84) between the vertical all blade water turbine (8B) and the outer casing (77a).   Bearings between the inner shaft device (60A) and the outer shaft device (60B) of the vertical all blade mercury turbine (8H), the vertical all blade water turbine (8B), and the vertical all blade gas turbine (8A) (80) Various energy storage cycle coalescence engines provided with thrust bearings (80a).   A bearing (80) thrust bearing (80a) is provided between the inner shaft device (60A) and the outer shaft device (60B) of the vertical all blade water turbine (8B) and the vertical all blade gas turbine (8A). Various energy conservation cycle coalescence engine.   A bearing (80) thrust bearing (80a) is provided between the inner shaft device (60A) and the outer shaft device (60B) of the vertical type moving blade mercury turbine (8H) and vertical type moving blade water turbine (8B). Various energy conservation cycle coalescence engine.   Various energy storage cycle coalescing engines provided with a bearing (80) thrust bearing (80a) between the inner shaft device (60A) and the outer shaft device (60B) of the vertical rotor blade water turbine (8B).   A bearing (80) thrust bearing (80a) is provided between the inner shaft device (60A) and the outer shaft device (60B) of the vertical all blade water turbine (8B) and the vertical all blade gas turbine (8A). Various energy conservation cycle coalescence engine.   Various energy storage cycle coalescing engines comprising a bearing (80) thrust bearing (80a) between the inner shaft device (60A) and the outer shaft device (60B) of the vertical all blade gas turbine (8A).   An inner shaft device (60A) and an outer shaft device (60B) are coupled to each other by bearings (80), (80), and (80) in a fixed outer casing (94), and the counter rotating magnetic friction blade transmission device (84) is provided. Various energy conservation cycle coalescing engines.   An inner shaft device (60A) and an outer shaft device (60B) are coupled to each other by bearings (80), (80), and (80) in a fixed outer casing (94), and a water pump and a counter rotating magnetic friction blade transmission device. (84) Various energy conservation cycle coalescence engines.   Various energies of the counter-rotating gear device (84Y) by coupling the inner shaft device (60A) and the outer shaft device (60B) with the bearings (80) (80) (80) in the fixed outer casing (94). Conservation cycle coalescence organization.   An inner shaft device (60A) and an outer shaft device (60B) are coupled to each other by bearings (80), (80), and (80) in a fixed outer casing (94) fixed to a water pump and counter rotating gear device (84Y). Various energy conservation cycle coalescence engine.   Various energy storage cycle coalescing engines, in which the inner shaft device (60A) is coupled by a bearing (80) in a fixed outer case (94), thereby providing a counter-rotating magnetic friction blade transmission device (84).   Various energy storage cycle coalescing engines in which the inner shaft device (60A) is coupled to the fixed outer case (94) by a bearing (80) to form a water pump and counter-rotating magnetic friction blade transmission device (84).   Various energy storage cycle coalescing engines in which the inner shaft device (60A) is connected to the fixed outer case (94) by a bearing (80) to form a counter-rotating gear device (84Y).   Various energy storage cycle coalescing engines in which the inner shaft device (60A) is connected to the fixed outer case (94) by a bearing (80) to form a water pump and counter rotating gear device (84Y).   Various energy storage cycle coalescing engines in which the outer shaft device (60B) is connected to the fixed outer casing (94) by a bearing (80) to form a counter rotating magnetic friction blade transmission device (84).   Various energy storage cycle coalescing engines in which the outer shaft device (60B) is coupled to the fixed outer case (94) by a bearing (80) to form a water pump and counter-rotating magnetic friction blade transmission device (84).   Various energy storage cycle coalescing engines in which the outer shaft device (60B) is coupled to the fixed outer case (94) by a bearing (80) to form a counter-rotating gear device (84Y).   Various energy storage cycle coalescing engines in which the outer shaft device (60B) is coupled to the fixed outer case (94) by a bearing (80) to form a water pump and counter-rotating gear device (84Y).   An inner shaft device (60A) and an outer shaft device (60B) are coupled to each other by a thrust bearing (80a) (80a) (80a) in a fixed outer casing (94), and the counter rotating magnetic friction blade transmission device (84) is connected. ) Various energy conservation cycle coalescing engines.   The inner shaft device (60A) and the outer shaft device (60B) are connected to each other by a thrust bearing (80a) (80a) (80a) in a fixed outer casing (94), and the water pump and counter-rotating magnetic friction blade are transmitted. Various energy storage cycle coalescence engine as device (84).   Various types of contra-rotating gear devices (84Y) are obtained by connecting the inner shaft device (60A) and the outer shaft device (60B) with a thrust bearing (80a) (80a) (80a) in a fixed outer case (94). Energy conservation cycle coalescence engine.   The inner shaft device (60A) and the outer shaft device (60B) are coupled to each other by a thrust bearing (80a) (80a) (80a) in a fixed outer casing (94) which is fixed to the water pump and counter rotating gear device (84Y). Various energy conservation cycle coalescing engines.   Various energy storage cycle coalescing engines in which the inner shaft device (60A) is coupled with a thrust bearing (80a) in a fixed outer case (94) to form a counter rotating magnetic friction blade transmission device (84).   Various energy storage cycle coalescing engines in which an inner shaft device (60A) is coupled to a fixed outer casing (94) by a thrust bearing (80a) to form a water pump and counter-rotating magnetic friction blade transmission device (84).   Various energy storage cycle coalescing engines in which the inner shaft device (60A) is coupled with a thrust bearing (80a) in a fixed outer casing (94) to form a counter rotating gear device (84Y).   Various energy storage cycle coalescing engines in which the inner shaft device (60A) is connected to the fixed outer casing (94) by a thrust bearing (80a) to form a water pump and counter rotating gear device (84Y).   Various energy storage cycle coalescing engines in which the outer shaft device (60B) is coupled with a thrust bearing (80a) in a fixed outer casing (94) to form a counter-rotating magnetic friction blade transmission device (84).   Various energy storage cycle coalescing engines in which the outer shaft device (60B) is connected to the fixed outer casing (94) by a thrust bearing (80a) to form a water pump and counter-rotating magnetic friction blade transmission device (84).   Various energy storage cycle coalescing engines in which the outer shaft device (60B) is coupled with a thrust bearing (80a) in a fixed outer casing (94) to form a counter rotating gear device (84Y).   Various energy storage cycle coalescing engines in which the outer shaft device (60B) is coupled to the fixed outer case (94) by a thrust bearing (80a) to form a water pump and counter rotating gear device (84Y).   Various energy storage cycle coalescence engine that recovers high-temperature mercury (1d) exhaust heat with heat pump (1G).   Various energy storage cycle coalescence engine that collects compressed air heat (28b) with heat pump (1G).   Various energy storage cycle coalescing engines that recover combustion gas (49) heat quantity with heat pump (1G).   Various energy storage cycle coalescence engine that recovers heat with heat pump (1G).   Various energy storage cycle coalescing engine that recovers with high temperature mercury (1d) exhaust heat quantity around 220 degrees with intake air (28a) with heat pump (1G).   Various energy storage cycle coalescence engine that recovers with intake air (28a) from around 900 degrees of heat of compressed air (28b) with heat pump (1G).   Various energy storage cycle coalescing engine that recovers with intake air (28a) from about 900 degrees of heat of combustion gas (49) with heat pump (1G).   Various energy storage cycle coalescence engine that recovers with intake air (28a) from around 900 degrees of heat with heat pump (1G).   Various energy storage cycle coalescence engine that recovers with intake air (28a) from over 900 degrees of compressed air heat (28b) with heat pump (1G).   Various energy storage cycle coalescing engines that recover from combustion gas (49) with an intake air (28a) from 900 ° C. or higher with a heat pump (1G).   Various energy storage cycle coalescence engine that recovers with intake air (28a) from over 900 degrees of heat with heat pump (1G).   Various energy storage cycle coalescence engine that recovers with intake air (28a) from 900 ° C or less of compressed air calorie (28b) with heat pump (1G).   Various energy storage cycle coalescing engines that recover with combustion air (49) with intake air (28a) from a heat quantity of 900 degrees or less with a heat pump (1G).   Various energy storage cycle coalescence engine that recovers with intake air (28a) from heat of 900 degrees or less with heat pump (1G).   Various energy storage cycle coalescing engines that recover high-temperature mercury (1d) exhaust heat with a heat pump (1G) and recover compression heat.   Various energy storage cycle coalescence engine that collects compressed air heat (28b) by heat pump (1G) and recovers compression heat.   Various energy storage cycle coalescence engine that recovers combustion gas (49) calorie with a heat pump (1G) and recovers compression heat.   Various energy storage cycle coalescing engines that recover heat and heat with a heat pump (1G).   Various energy storage cycle coalescing engines that recover high-temperature mercury (1d) exhaust heat from around 220 degrees with intake air (28a) using a heat pump (1G).   Various energy storage cycle coalescing engine that recovers compressed heat with intake air (28a) from around 900 degrees of heat of compressed air (28b) with heat pump (1G).   Various energy storage cycle coalescence engine that recovers compression heat with intake air (28a) from about 900 degrees of heat of combustion gas (49) with heat pump (1G).   Various energy storage cycle coalescing engine that recovers compression heat with intake air (28a) from about 900 degrees of heat with heat pump (1G).   Various energy storage cycle coalescing engines that recover heat from compressed air by the intake air (28a) from over 900 degrees of compressed air heat (28b) with a heat pump (1G).   Various energy storage cycle coalescing engine that recovers compressed heat with intake air (28a) from a combustion gas (49) calorie of 900 degrees or more with a heat pump (1G).   Various energy storage cycle coalescing engine that recovers compression heat with intake air (28a) from over 900 degrees of heat with heat pump (1G).   Various energy storage cycle coalescing engines that recover heat from compressed air using a heat pump (1G) and recovering compressed heat from intake air (28a) from 900 degrees or less.   Various energy storage cycle coalescing engines that use a heat pump (1G) to recover combustion heat from combustion gas (49) with an intake air (28a) from a temperature of 900 degrees or less.   Various energy storage cycle coalescing engine that recovers heat of compression and recovery with suction air (28a) from heat of 900 degrees or less with heat pump (1G).   Various energy storage cycle coalescing engines that recover high-temperature mercury (1d) exhaust heat with a heat pump (1G) and compression heat with a recovery heat pump (1G).   Various energy storage cycle coalescing engines that collect heat of compressed air (28b) with a recovery heat pump (1G) using a heat pump (1G).   Various energy storage cycle coalescing engines that recover combustion gas (49) calorie with a heat pump (1G) and compression heat with a recovery heat pump (1G).   Various energy storage cycle coalescing engines that recover heat from a heat pump (1G) and heat from a recovery heat pump (1G).   Various energy storage cycle coalescing engines that recover high-temperature mercury (1d) with a heat pump (1G) and exhaust heat from around 220 ° C. with intake air (28a) and recovery heat pump (1G).   Various energy storage cycle coalescing engines that recover heat of compression air with the recovery heat pump (1G) from the intake air (28a) from around 900 degrees of heat of compressed air (28b) with the heat pump (1G).   Various energy storage cycle coalescence engine that recovers compression heat with a recovery heat pump (1G) from intake air (28a) from about 900 degrees of heat of combustion gas (49) with a heat pump (1G).   Various energy storage cycle coalescing engines that recover heat from around 900 degrees of heat with a heat pump (1G) and suction heat (28a) with a recovery heat pump (1G).   Various energy storage cycle coalescing engines that recover heat of compression air (28a) with a recovery heat pump (1G) from over 900 degrees of compressed air heat (28b) with a heat pump (1G).   Various energy storage cycle coalescing engine that recovers compression heat from the combustion gas (49) with an intake air (28a) with a recovery heat pump (1G) from a combustion gas (49) with a heat pump (1G) at 900 ° C or more.   Various energy storage cycle coalescence engine that recovers compression heat with intake heat (28a) and recovery heat pump (1G) from heat of 900 degrees or more with heat pump (1G).   Various energy storage cycle coalescing engines that recover heat of compression air with a recovery heat pump (1G) from intake air (28a) from 900 degrees or less of compressed air heat (28b) with a heat pump (1G).   Various energy storage cycle coalescing engines that recover combustion gas (49) with an intake air (28a) from a combustion gas (49) with a heat recovery pump (1G) using a heat pump (1G) from 900 degrees C or less.   Various energy storage cycle coalescing engine that recovers compression heat with intake heat (28a) and recovery heat pump (1G) from heat of 900 degrees or less with heat pump (1G).   Various energy storage cycle coalescing engines that recover heat of compressed air (28b) using a heat pump (1G) and using a recovered heat pump (1G) using a compressed water heat exchanger (2Y).   Various energy storage cycle coalescing engines that recover heat from the combustion gas (49) by the heat pump (1G) and heat from the compressed water heat exchanger (2Y) by the recovery heat pump (1G).   Various energy storage cycle coalescing engines that recover heat from a heat pump (1G) and heat from a compressed water heat exchanger (2Y) from a recovery heat pump (1G).   Various energy storage cycle coalescing engines that recover heat from the high-temperature mercury (1d) exhaust heat quantity around 220 degrees with the heat pump (1G) and the intake air (28a) with the recovery heat pump (1G) with the compressed water heat exchanger (2Y).   Various energy storage cycle coalescing engine that recovers heat with compressed air heat exchanger (2Y) with intake heat (28a) with intake air (28a) from about 900 degrees of heat of compressed air (28b) with heat pump (1G).   Various energy storage cycle coalescence engine that recovers heat from combustion gas (49) with a heat pump (1G) from about 900 degrees Celsius and intake air (28a) with a recovery heat pump (1G) with a compressed water heat exchanger (2Y).   Various energy storage cycle coalescing engine that recovers heat with a recovery heat pump (1G) with a compressed water heat exchanger (2Y) with intake air (28a) from about 900 degrees of heat with a heat pump (1G).   Various energy storage cycle coalescing engines that recover heat from the compressed air heat quantity (28b) from 900 ° C. or higher with the heat pump (1G) and the recovered heat pump (1G) with the compressed water heat exchanger (2Y).   Various energy storage cycle coalescing engine that recovers heat from combustion gas (49) with a heat pump (1G) from 900 degrees Celsius or higher and intake air (28a) with a recovery heat pump (1G) with a compressed water heat exchanger (2Y).   Various energy storage cycle coalescing engines that recover heat from a heat quantity of 900 ° C. or more with a heat pump (1G) and intake air (28a) with a recovery heat pump (1G) with a compressed water heat exchanger (2Y).   Various energy storage cycle coalescing engines that recover heat with compressed air heat exchanger (2Y) with intake heat (28a) from intake air (28a) from 900 degrees or less of compressed air heat (28b) with heat pump (1G).   Various energy storage cycle coalescing engines that recover combustion gas (49) with a heat pump (1G) from an amount of heat of 900 degrees C or less with intake air (28a) with a recovery heat pump (1G) with a compressed water heat exchanger (2Y).   Various energy storage cycle coalescing engines that recover heat from a heat quantity of 900 degrees C or less with a heat pump (1G) with intake air (28a) with a recovery heat pump (1G) with a compressed water heat exchanger (2Y).   Various energy storage cycle coalescing engines that recover heat from a high-temperature mercury (1d) exhaust heat with a heat pump (1G) and a recovery heat pump (1G) with a compression / reduction compression chamber mercury heat exchanger (2Z).   Various energy storage cycle coalescence engines that recover heat of compressed air (28b) with a heat pump (1G) and heat with a recovery heat pump (1G) with a compression / reduction compression chamber mercury heat exchanger (2Z).   Various energy storage cycle coalescing engines that recover heat from the combustion gas (49) with a heat pump (1G) and heat with a recovery heat pump (1G) using a compression / reduction compression chamber mercury heat exchanger (2Z).   Various energy storage cycle coalescing engines that recover heat with a heat pump (1G) and with a recovery heat pump (1G) with a compression / reduction compression chamber mercury heat exchanger (2Z).   Various energy storage cycles in which high-temperature mercury (1d) is exhausted by a heat pump (1G) and exhaust heat is about 220 degrees, and intake air (28a) is recovered by a recovery heat pump (1G) by a compression / reduction compression chamber mercury heat exchanger (2Z). Combined organization.   Combined with various energy storage cycles to recover heat from compressed air calorie (28b) from around 900 degrees with heat pump (1G), intake air (28a) with recovery heat pump (1G) with compression-reduction compression chamber mercury heat exchanger (2Z) organ.   Combustion gas (49) with a heat pump (1G) Combined with various energy storage cycles to recover heat from around 900 degrees of intake air (28a) with a recovery heat pump (1G) with a compression / reduction compression chamber mercury heat exchanger (2Z) organ.   Various energy storage cycle coalescing engines that recover heat with a heat pump (1G) from about 900 degrees Celsius and intake air (28a) with a recovery heat pump (1G) with a compression / reduction compression chamber mercury heat exchanger (2Z).   Combined with various energy storage cycles to recover heat from compressed air calorie (28b) over 900 degrees with heat pump (1G), intake air (28a) with heat recovery pump (1G) with compression / reduction compression chamber mercury heat exchanger (2Z) organ.   Combining various energy storage cycles with a heat pump (1G) for recovering heat with combustion gas (49) from an amount of heat of 900 ° C. or higher and intake air (28a) with a recovery heat pump (1G) using a compression / reduction compression chamber mercury heat exchanger (2Z) organ.   Various energy storage cycle coalescence engine that recovers heat with a heat pump (1G) from 900 degrees Celsius or higher with intake air (28a) with a recovery heat pump (1G) with a compression / reduction compression chamber mercury heat exchanger (2Z).   Combined with various energy storage cycles to recover heat from heat of compressed air (28b) from 900 ° C or less with heat pump (1G) and suction heat (28a) with heat recovery pump (1G) with compression / reduction compression chamber mercury heat exchanger (2Z) organ.   Combining various energy storage cycles with a heat pump (1G) for recovering heat from a combustion gas (49) with an intake air (28a) from a heat quantity of 900 degrees or less with a recovery heat pump (1G) with a compression / reduction compression chamber mercury heat exchanger (2Z) organ.   Various energy storage cycle coalescing engines that recover heat from a heat quantity of 900 degrees or less with a heat pump (1G) and intake air (28a) with a recovery heat pump (1G) with a compression / reduction compression chamber mercury heat exchanger (2Z).   Various energy storage cycle coalescing engines that recover high-temperature mercury (1d) exhaust heat with a heat pump (1G) and drive compression blades to drive all blade turbines (8X).   A combined energy storage cycle engine that recovers compressed air heat (28b) with a heat pump (1G) and recovers compressed heat to drive all rotor blade turbines (8X).   Various energy storage cycle coalescing engines that drive combustion blades (8X) by recovering the amount of combustion gas (49) heat with a heat pump (1G) and recovering compression heat.   A combined energy storage cycle engine that recovers the amount of heat with a heat pump (1G) and recovers compression heat to drive the entire rotor blade turbine (8X).   Various energy storage cycle coalescing engines that drive the entire blade turbine (8X) by recovering compression heat from the high-temperature mercury (1d) exhaust heat quantity of around 220 degrees with the intake air (28a) by the heat pump (1G).   Various energy storage cycle coalescence engines that drive the entire blade turbine (8X) by recovering the compressed heat of the compressed air with the intake air (28a) from around 900 degrees of heat (28b) with the heat pump (1G).   Various energy storage cycle coalescing engines that drive the entire blade turbine (8X) by recovering compression heat with the intake air (28a) from about 900 degrees of heat of combustion gas (49) with a heat pump (1G).   Various energy storage cycle coalescing engines that drive the entire rotor blade turbine (8X) by recovering the compressed heat of the intake air (28a) from about 900 degrees of heat with a heat pump (1G).   Various energy storage cycle coalescing engines that drive the entire rotor blade turbine (8X) by recovering the compressed heat of the compressed air using the heat pump (1G) and the intake air (28a) from 900 degrees or more of the compressed air heat (28b).   Various energy storage cycle coalescing engines that drive combustion blades (8X) by recovering compressed heat from the combustion gas (49) with an intake air (28a) from a combustion gas (49) heat of 900 degrees or more with a heat pump (1G).   Various energy storage cycle coalesced engines that drive the entire rotor blade turbine (8X) by recovering the compressed heat of the intake air (28a) from the heat quantity of 900 degrees or more with a heat pump (1G).   Various energy storage cycle coalescing engines that drive the entire rotor blade turbine (8X) by recovering the compressed heat of the compressed air by using the intake air (28a) from the heat of the compressed air (28b) below 900 degrees with the heat pump (1G).   Various energy storage cycle coalescing engines that drive the entire rotor blade turbine (8X) by recovering compression heat with the intake air (28a) from a combustion gas (49) calorie of 900 degrees or less with a heat pump (1G).   Various energy storage cycle coalesced engines that drive the entire rotor blade turbine (8X) by recovering the compressed heat of the intake air (28a) from a heat quantity of 900 degrees or less with a heat pump (1G).   Various energy storage cycle coalescing engines that drive all rotor blade turbines (8X) by collecting high-temperature mercury (1d) exhaust heat with a heat pump (1G) and compression heat with a recovery heat pump (1G).   Various energy storage cycle combined engines that drive the entire blade turbine (8X) by recovering the amount of compressed air heat (28b) with the recovery heat pump (1G) with the heat pump (1G).   Various energy storage cycle coalescing engines that drive combustion turbines (8X) by recovering the amount of combustion gas (49) heat with a recovery heat pump (1G) with a heat pump (1G).   Various energy storage cycle coalesced engines that drive all rotor blade turbines (8X) by recovering the amount of heat with a heat pump (1G) and recovering compression heat with a recovery heat pump (1G).   Combined with various energy storage cycles to drive all blade turbines (8X) by collecting high-temperature mercury (1d) with a heat pump (1G) and exhaust heat from around 220 degrees with intake air (28a) with a recovery heat pump (1G). organ.   Combined engine with various energy storage cycles that drives the entire blade turbine (8X) by recovering the compressed air heat (28a) with the recovery heat pump (1G) from around 900 degrees of the compressed air calorie (28b) with the heat pump (1G) .   Various energy storage cycle coalescing engines that drive the entire blade turbine (8X) by recovering the compression gas with the recovery heat pump (1G) with the intake air (28a) from the combustion gas (49) calorific value of around 900 degrees with the heat pump (1G) .   Various energy storage cycle coalescing engines that drive the entire rotor blade turbine (8X) by recovering compression heat with the recovered heat pump (1G) from the intake air (28a) from about 900 degrees C with the heat pump (1G).   Various energy storage cycle coalescence engines that drive all blade turbines (8X) by recovering compression heat with recovered heat pump (1G) from intake air (28a) from over 900 degrees of compressed air heat (28b) with heat pump (1G) .   Various energy storage cycle coalescence engine that drives combustion blade (8X) by recovering compression heat with intake heat (28a) with recovery heat pump (1G) from combustion gas (49) calorie over 900 degrees with heat pump (1G) .   Various energy storage cycle coalescing engines that drive all rotor blade turbines (8X) by recovering compression heat with a recovery heat pump (1G) with intake air (28a) from a heat quantity of 900 degrees or more with a heat pump (1G).   Various energy storage cycle coalescence engine that drives the whole blade turbine (8X) by recovering the compression heat with the recovery heat pump (1G) with the intake air (28a) from 900 degrees or less of the compressed air heat quantity (28b) with the heat pump (1G) .   Various energy storage cycle combined engines that drive combustion blades (8X) by combustion gas (49) with a heat pump (1G) and recovering compression heat with a recovery heat pump (1G) from intake air (28a) from 900 degrees C or less .   Various energy storage cycle coalescing engines that drive the entire blade turbine (8X) by recovering the compression heat with the recovered heat pump (1G) from the heat quantity of 900 degrees or less with the heat pump (1G) and the intake air (28a).   Various energy storage cycle coalescing engines that drive the entire blade turbine (8X) by recovering heat (28b) of compressed air with a heat pump (1G) and recovering heat with a compressed water heat exchanger (2Y) with a recovery heat pump (1G).   Various energy storage cycle coalescing engines that drive the entire rotor blade turbine (8X) by recovering the heat quantity of the combustion gas (49) with the heat pump (1G) and the recovered heat pump (1G) with the compressed water heat exchanger (2Y).   Various energy storage cycle coalescing engines that drive the entire blade turbine (8X) by recovering heat with a heat recovery pump (1G) and heat with a compressed water heat exchanger (2Y) with a heat pump (1G).   High-temperature mercury (1d) with heat pump (1G) Exhaust calorific value around 220 degrees C Various energy storage cycle coalescence engine that drives   Compressed air calorie (28b) from around 900 degrees with heat pump (1G) From intake air (28a), recovered heat pump (1G) recovers heat with compressed water heat exchanger (2Y), and complete rotor blade turbine (8X) Various energy storage cycle coalescence engine to drive.   The combustion gas (49) with a heat pump (1G) recovers heat with an intake air (28a) from around 900 ° C. with a recovery heat pump (1G) and with a compressed water heat exchanger (2Y) to recover an all blade turbine (8X). Various energy storage cycle coalescence engine to drive.   Various types of energy storage to drive all blade turbines (8X) by recovering heat from intake air (28a) with recovered heat pump (1G) with compressed water heat exchanger (2Y) from about 900 degrees of heat with heat pump (1G) Cycle coalescence engine.   Compressed air calorie (28b) from 900 degrees or more with heat pump (1G), intake air (28a) with recovered heat pump (1G), heat recovery with compressed water heat exchanger (2Y), and all rotor blade turbine (8X) Various energy storage cycle coalescence engine to drive.   The heat pump (1G) recovers heat from the combustion gas (49) with an intake air (28a) from a heat quantity of 900 ° C. or more, and the recovered heat pump (1G) recovers heat with the compressed water heat exchanger (2Y), thereby Various energy storage cycle coalescence engine to drive.   Various types of energy storage to drive all rotor blade turbines (8X) by recovering heat with heat pump (1G) from intake air (28a) with recovered heat pump (1G) using compressed water heat exchanger (2Y) Cycle coalescence engine.   Compressed air calorie (28b) from 900 degrees or less with heat pump (1G) Recover heat pump (1G) with recovered heat pump (1G) with compressed water heat exchanger (2Y) to recover all blade turbine (8X) Various energy storage cycle coalescence engine to drive.   The heat pump (1G) recovers heat from the combustion gas (49) from an amount of heat of 900 ° C. or less to the intake air (28a), the recovered heat pump (1G) recovers heat from the compressed water heat exchanger (2Y), and the whole rotor blade turbine (8X) Various energy storage cycle coalescence engine to drive.   Various types of energy storage to drive all blade turbines (8X) by recovering heat with intake heat (28a) with heat pump (1G) using intake air (28a) with recovered heat pump (1G) with compressed water heat exchanger (2Y) Cycle coalescence engine.   Various energies that drive the whole blade turbine (8X) by recovering the heat of the high-temperature mercury (1d) exhaust heat with the heat pump (1G) with the recovery heat pump (1G) with the compression / reduction compression chamber mercury heat exchanger (2Z) Conservation cycle coalescence organization.   Compressed air calorie (28b) is recovered by heat pump (1G), heat recovery is performed by recovery heat pump (1G) by compression / reduction compression chamber mercury heat exchanger (2Z), and various energy storage is performed to drive all blade turbine (8X) Cycle coalescence engine.   Various energy storages that drive combustion blade (8X) by recovering heat from combustion gas (49) with heat pump (1G) and recovery heat pump (1G) with compression / reduction compression chamber mercury heat exchanger (2Z) Cycle coalescence engine.   A combined energy storage cycle engine that recovers heat with a heat pump (1G) and recovers heat with a compression / reduction compression chamber mercury heat exchanger (2Z) with a recovery heat pump (1G) to drive an entire blade turbine (8X).   High temperature mercury (1d) with heat pump (1G), exhaust heat from around 220 degrees, intake air (28a) with recovery heat pump (1G), heat recovery with compression / reduction compression chamber mercury heat exchanger (2Z), and all moving blades Various energy storage cycle coalescence engine that drives the turbine (8X).   Compressed air heat (28b) from around 900 degrees with heat pump (1G), intake air (28a) with recovery heat pump (1G), heat recovery with compression reduced diameter compression chamber mercury heat exchanger (2Z), and full blade turbine Various energy storage cycle coalescence engine that drives (8X).   Combustion gas (49) with a heat pump (1G) from about 900 degrees Celsius, intake air (28a) is recovered with a recovery heat pump (1G), heat is recovered with a compression-reduction-compression chamber mercury heat exchanger (2Z), and a full blade turbine Various energy storage cycle coalescing engines that drive (8X).   The heat pump (1G) recovers heat from around 900 degrees of intake air (28a) with the recovery heat pump (1G) and the heat with the compression / shrinkage compression chamber mercury heat exchanger (2Z) to drive the entire blade turbine (8X) Various energy conservation cycle coalescing engines.   Compressed air calorie (28b) from 900 degrees or more with heat pump (1G) Recovered heat pump (1G) with compression heat pump (1G), heat recovery with compression heat exchanger (2Z), and full blade turbine Various energy storage cycle coalescence engine that drives (8X).   Combustion gas (49) with a heat pump (1G) from a heat quantity of 900 degrees or more, intake air (28a) with a recovery heat pump (1G), heat recovery with a compression / reduction compression chamber mercury heat exchanger (2Z), and a full rotor blade turbine Various energy storage cycle coalescence engine that drives (8X).   The heat pump (1G) recovers heat from over 900 degrees of heat from the intake air (28a) by the recovery heat pump (1G) and the compression / shrinkage compression chamber mercury heat exchanger (2Z) to drive the all blade turbine (8X) Various energy conservation cycle coalescing engines.   Compressed air calorie (28b) from 900 degrees or less with heat pump (1G), intake air (28a) with recovered heat pump (1G), heat recovery with compression reduced diameter compression chamber mercury heat exchanger (2Z), and full blade turbine Various energy storage cycle coalescence engine that drives (8X).   Combustion gas (49) with a heat pump (1G) from an amount of heat of 900 degrees C or less, intake air (28a) with a recovery heat pump (1G), heat recovery with a compression / reduction compression chamber mercury heat exchanger (2Z), and a full rotor blade turbine Various energy storage cycle coalescing engines that drive (8X).   The heat pump (1G) heats up to 900 degrees Celsius or less, and the intake air (28a) recovers the heat with the recovery heat pump (1G) with the compression / reduction compression chamber mercury heat exchanger (2Z) to drive the all blade turbine (8X). Various energy conservation cycle coalescing engines.   Various energy storage cycle coalescing engines that recover high-temperature mercury (1d) exhaust heat with a heat pump (1G) and recover it to compression heat (52e).   Various energy storage cycle coalescing engines that recover the compressed air heat (28b) by the heat pump (1G) and recover the compressed heat to cold (52e).   Various energy storage cycle coalescing engines that use the heat pump (1G) to recover the combustion gas (49) heat and recover it to compression heat (52e).   Various energy storage cycle coalescence engine which collects heat with a heat pump (1G) and recovers compression heat to cool (52e).   Various energy storage cycle coalescing engines that recover high-temperature mercury (1d) with a heat pump (1d) from about 220 degrees of exhaust heat with the intake air (28a) and recover it to cold (52e).   Various energy storage cycle coalescing engines that recover heat from compressed air by the intake air (28a) from about 900 degrees of compressed air heat (28b) with a heat pump (1G) to cool (52e).   Various energy storage cycle coalesced engines that use the heat pump (1G) to recover the combustion gas (49) from about 900 degrees of heat with the intake air (28a) and recover the compression heat to cold (52e).   Various energy storage cycle coalescence engines that recover heat from around 900 degrees of heat with a heat pump (1G), recovering compressed heat with intake air (28a), and making it cool (52e).   Various energy storage cycle coalescing engines that recover heat from compressed air by using a heat pump (1G), recovering compressed heat from intake air (28a) from 900 ° C or higher (28b).   Various energy storage cycle coalesced engines that use the heat pump (1G) to recover the combustion gas (49) from the heat quantity of 900 degrees or more with the intake air (28a) and recover the compression heat to cold (52e).   Various energy storage cycle coalescing engines that recover heat from over 900 degrees of heat with a heat pump (1G), recovering compression heat with intake air (28a) and making it cool (52e).   Various energy storage cycle coalescing engines that recover heat from compressed air by using a heat pump (1G), recovering compression heat from intake air (28a) from 900 degrees or less (28b).   Various energy storage cycle coalescing engines that use the heat pump (1G) to recover the combustion gas (49) from the heat of 900 ° C. or less with the intake air (28a) to recover the cold (52e).   Various energy storage cycle coalescing engines that recover heat from 900 ° C or less with a heat pump (1G), recovering compressed heat with intake air (28a), and making it cool (52e).   Various energy storage cycle coalescing engines that convert high-temperature mercury (1d) exhaust heat with a recovery heat pump (1G) to cold (52e) with a heat pump (1G).   Various energy storage cycle coalescing engines that use the heat pump (1G) to recover the amount of compressed air heat (28b) by using the recovery heat pump (1G) to recover the heat of compression (52e).   Various energy storage cycle coalescing engines that use the heat pump (1G) to recover the combustion gas (49) calorie by the recovery heat pump (1G) and recover the heat to cold (52e).   Various energy storage cycle coalescing engines that use the heat pump (1G) to recover the amount of heat by using the recovery heat pump (1G) to recover the compression heat to cool (52e).   Various energy storage cycle coalescing engines that use high-temperature mercury (1d) with a heat pump (1G) and exhaust heat from around 220 degrees to recover the compression heat (52e) with intake air (28a) with a recovery heat pump (1G).   Various energy storage cycle coalescing engines that use compressed heat to recover the cold heat (52e) from the intake air (28a) with the recovery heat pump (1G) from around 900 degrees of the compressed air heat (28b) with the heat pump (1G).   Various energy storage cycle coalescing engines that use the heat pump (1G) to recover the combustion gas (49) from about 900 degrees Celsius by using the intake air (28a) and the recovered heat pump (1G) to recover the compression heat (52e).   Various energy storage cycle coalescing engines that use a heat pump (1G) to recover heat from around 900 degrees Celsius by suction air (28a) and recovery heat pump (1G) to cool (52e).   Various energy storage cycle coalescing engines that use the heat pump (1G) to recover the compressed air heat (28b) from 900 ° C. or higher with the intake air (28a) by the recovery heat pump (1G) to cool (52e).   Various energy storage cycle coalescing engines that use a heat pump (1G) to recover the combustion gas (49) from a heat quantity of 900 ° C. or higher to the intake air (28a) by the recovery heat pump (1G) and recover the cold (52e).   Various energy storage cycle coalescing engines that use a heat pump (1G) to recover heat from 900 degrees Celsius or higher using intake air (28a) and recovery heat pump (1G) to cool (52e).   Various energy storage cycle coalescing engines that use a heat pump (1G) to recover the heat of compression air (28b) from 900 degrees or less to the intake air (28a) with the recovery heat pump (1G) to cool (52e).   Various energy storage cycle coalescing engines that use a heat pump (1G) to recover combustion gas (49) from an amount of heat of 900 ° C. or less to intake air (28a) using a recovery heat pump (1G) and compress heat to cool (52e).   Various energy storage cycle coalescing engines that use a heat pump (1G) to recover heat from 900 degrees Celsius or less with intake air (28a) by using a recovered heat pump (1G) to recover heat to cold (52e).   Various energy storage cycle coalescing engines that use the heat pump (1G) to recover the amount of heat of compressed air (28b) by means of the recovery heat pump (1G) and recover the heat by using the compressed water heat exchanger (2Y) to cool (52e).   Various energy storage cycle coalescing engines that recover the combustion gas (49) by the heat pump (1G) and recover the heat (52e) by the recovered heat pump (1G) by the compressed water heat exchanger (2Y).   Various energy storage cycle coalescing engines that collect heat with a heat pump (1G) and recover heat with a compressed water heat exchanger (2Y) with a recovery heat pump (1G) to cool (52e).   Various types of high temperature mercury (1d) with heat pump (1G), exhaust heat quantity around 220 degrees, intake air (28a), recovery heat pump (1G) with compressed water heat exchanger (2Y), heat recovery to cold (52e) Energy conservation cycle coalescence engine.   Compressed air calorie (28b) from around 900 degrees with heat pump (1G) Various energy to recover heat to cold air (52e) with intake air (28a) with recovered heat pump (1G) with compressed water heat exchanger (2Y) Conservation cycle coalescence organization.   Various energies from the combustion gas (49) with the heat pump (1G) to the cold energy (52e) by recovering the heat with the intake air (28a) from the heat of about 900 degrees with the recovery heat pump (1G) with the compressed water heat exchanger (2Y) Conservation cycle coalescence organization.   Various energy storage cycle coalescing engines that use a heat pump (1G) to recover heat from around 900 degrees Celsius using the intake air (28a) and a recovered heat pump (1G) using a compressed water heat exchanger (2Y) to cool (52e).   Compressed air calorie (28b) from 900 degrees or more with heat pump (1G) Various energy to recover heat to cold air (52e) by collecting heat with suction air (28a) with recovered heat pump (1G) with compressed water heat exchanger (2Y) Conservation cycle coalescence organization.   Various energy from the combustion gas (49) with a heat pump (1G) to a cold heat (52e) by recovering heat with a recovery heat pump (1G) with a compressed water heat exchanger (2Y) with intake air (28a) from a heat quantity of 900 degrees or more Conservation cycle coalescence organization.   Various energy storage cycle coalescing engines that use a heat pump (1G) to recover heat from 900 degrees Celsius or higher with intake air (28a) with a recovery heat pump (1G) with a compressed water heat exchanger (2Y) to cool (52e).   Compressed air heat amount (28b) from 900 degrees or less with heat pump (1G) Various energy to recover heat to cold heat (52e) with intake air (28a) with recovered heat pump (1G) with compressed water heat exchanger (2Y) Conservation cycle coalescence organization.   Various energy from the combustion gas (49) with the heat pump (1G) to 900 ° C or less, the intake air (28a) with the recovery heat pump (1G), the heat recovery with the compressed water heat exchanger (2Y), and the cold energy (52e). Conservation cycle coalescence organization.   Various energy storage cycle coalescing engines that use a heat pump (1G) to recover heat to a cold (52e) from a heat quantity of 900 ° C. or less with intake air (28a) and a recovered heat pump (1G) with a compressed water heat exchanger (2Y).   High temperature mercury (1d) exhaust heat quantity with heat pump (1G) Recover heat pump (1G) with compression / reduction compression chamber mercury heat exchanger (2Z) to recover heat to cold energy (52e) Combined engine .   Compressed air heat quantity (28b) with heat pump (1G), recovery energy pump (1G) with compression / reduction diameter compression chamber mercury heat exchanger (2Z) recovers heat to cold energy (52e), combined with various energy storage cycle engines.   Various energy storage cycle coalescing engines that recover the combustion gas (49) by the heat pump (1G) by the recovery heat pump (1G) by the compression / reduction compression chamber mercury heat exchanger (2Z) to cool (52e).   Various energy storage cycle coalescing engines that recover heat with a heat pump (1G) and recover heat with a recovery heat pump (1G) with a compression / reduction compression chamber mercury heat exchanger (2Z) to cool (52e).   High-temperature mercury (1d) with a heat pump (1G), exhaust heat from around 220 ° C., intake air (28a) with a recovery heat pump (1G), heat recovery with a compression / reduction compression chamber mercury heat exchanger (2Z), and cooling (52e ) Various energy conservation cycle coalescing engines.   Compressed air calorie (28b) from around 900 degrees with heat pump (1G), intake air (28a) with recovery heat pump (1G), heat recovery with compression reduced diameter compression chamber mercury heat exchanger (2Z), and cold (52e) Various energy conservation cycle coalescing engines.   Combustion gas (49) with a heat pump (1G), heat from about 900 degrees C., intake air (28a) with a recovery heat pump (1G), heat recovery with a compression / reduction compression chamber mercury heat exchanger (2Z), and cooling (52e) Various energy conservation cycle coalescing engines.   Various types of energy storage from about 900 degrees of heat with a heat pump (1G) to intake air (28a) with a recovery heat pump (1G) and heat recovery with a compression / reduction compression chamber mercury heat exchanger (2Z) to cool (52e) Cycle coalescence engine.   Compressed air calorie (28b) from 900 ° C. or higher with heat pump (1G), recovered heat pump (1G) with compression heat pump (1G), heat recovery with compression heat exchanger (2Z), and cold (52e) Various energy conservation cycle coalescing engines.   Combustion gas (49) with a heat pump (1G) from an amount of heat of 900 degrees or more, intake air (28a) with a recovery heat pump (1G), heat recovery with a compression / reduction compression chamber mercury heat exchanger (2Z), and cooling (52e) Various energy conservation cycle coalescing engines.   Various kinds of energy storage from heat of 900 ° C or higher with heat pump (1G) to intake air (28a) with recovery heat pump (1G) and heat recovery with compression / reduction compression chamber mercury heat exchanger (2Z) to cool (52e) Cycle coalescence engine.   Compressed air calorie (28b) from 900 ° C. or less with heat pump (1G), recovered heat pump (1G) with compression heat pump (1G), heat recovery with compression heat exchanger (2Z), and cold (52e) Various energy conservation cycle coalescing engines.   Combustion gas (49) with a heat pump (1G) from an amount of heat of 900 degrees C or less, intake air (28a) with a recovery heat pump (1G), heat recovery with a compression / reduction compression chamber mercury heat exchanger (2Z), and cooling (52e) Various energy conservation cycle coalescing engines.   Various types of energy storage from heat of less than 900 degrees with heat pump (1G) to intake air (28a) with recovery heat pump (1G) and heat recovery with compression / reduction compression chamber mercury heat exchanger (2Z) to cool (52e) Cycle coalescence engine.   Various energy storage cycle coalescing engines that recover high-temperature mercury (1d) exhaust heat with heat pump (1G) and recover compression heat to heat (52d).   Various energy storage cycle coalescing engines that collect heat of compressed air (28b) with a heat pump (1G) and recover heat of compression air to heat (52d).   Various energy storage cycle coalescing engines that recover the combustion gas (49) calorie with a heat pump (1G) and recover it to heat (52d).   Various energy storage cycle coalescence engine which collects heat with a heat pump (1G) and recovers compression heat to heat (52d).   Various energy storage cycle coalescing engines that recover high-temperature mercury (1d) with a heat pump (1d) and recover heat from about 220 degrees of exhaust heat with intake air (28a) to heat (52d).   Various energy storage cycle coalescing engines that recover heat from compressed air by using intake air (28a) from around 900 degrees of compressed air heat (28b) by heat pump (1G).   Various energy storage cycle coalescing engines that use a heat pump (1G) to recover the combustion gas (49) from about 900 degrees of heat with the intake air (28a) and recover the compressed heat to warm (52d).   Various energy storage cycle coalescing engines that recover heat from around 900 degrees of heat with a heat pump (1G) and recover heat from compressed air with intake air (28a).   Various energy storage cycle coalescing engines that recover heat from compressed air heat (28b) from 900 ° C or higher with intake air (28a) by heat pump (1G) to heat (52d).   Various energy storage cycle coalescing engines that use a heat pump (1G) to recover combustion heat from combustion gas (49) from 900 ° C or higher with intake air (28a) to recover heat (52d).   Various energy storage cycle coalescing engines that recover heat from the heat of 900 degrees Celsius or higher by intake air (28a) and heat (52d) using a heat pump (1G).   Various energy storage cycle coalescing engines that recover heat from compressed air by using a suction pump (28a) from a heat quantity of compressed air (28b) below 900 degrees with a heat pump (1G).   Various energy storage cycle coalesced engines that use a heat pump (1G) to recover combustion heat from combustion gas (49) from a temperature of 900 degrees or less with intake air (28a) to recover warm heat (52d).   Various energy storage cycle coalescing engines that recover heat from recovered heat by using intake air (28a) and heat (52d) from heat of 900 ° C or less with heat pump (1G).   Various energy storage cycle coalescing engines that convert high-temperature mercury (1d) exhaust heat with a heat pump (1G) to compression heat with a recovery heat pump (1G) to generate heat (52d).   Various energy storage cycle coalescing engines that use the heat pump (1G) to recover the amount of heat of compressed air (28b) with the recovery heat pump (1G) to recover the heat (52d).   Various energy storage cycle coalescing engines that use combustion pump (1G) to recover the amount of heat from combustion gas (49) by collecting heat with compression heat pump (1G) to heat (52d).   Various energy storage cycle coalescing engines that use the heat pump (1G) to recover the heat by compressing heat with the recovery heat pump (1G) to make the heat (52d).   Various energy storage cycle coalescing engines that recover high-temperature mercury (1d) with a heat pump (1G) from about 220 degrees of exhaust heat and intake air (28a) with a recovery heat pump (1G) to recover heat (52d).   Various energy storage cycle coalescing engines that use compressed heat to recover heat (52d) by using a recovery heat pump (1G) with intake air (28a) from around 900 degrees of compressed air heat (28b) with a heat pump (1G).   Various energy storage cycle coalescing engines that use a heat pump (1G) to recover combustion gas (49) from a temperature of about 900 ° C. with intake air (28a) and a recovery heat pump (1G) to recover heat by heating (52d).   Various energy storage cycle coalescing engines that use a heat pump (1G) to recover heat from around 900 degrees Celsius by suction air (28a) and recovery heat pump (1G) to recover heat (52d).   Various energy storage cycle coalescing engines that recover heat from compressed air heat (28a) by using a recovery heat pump (1G) and heat (52d) from 900 degrees or more of compressed air heat (28b) with a heat pump (1G).   Various energy storage cycle coalescing engines that use the heat pump (1G) to recover the combustion gas (49) from 900 ° C. or higher to the intake air (28a) with the recovery heat pump (1G) to recover the heat (52d).   Various energy storage cycle coalescing engines that use a heat pump (1G) to recover heat from 900 degrees Celsius or higher using intake air (28a) and recovery heat pump (1G) to recover heat (52d).   Various energy storage cycle coalesced engines that use compressed heat to recover heat (52d) by using a recovery heat pump (1G) with intake air (28a) from 900 degrees or less of compressed air heat (28b) with a heat pump (1G).   Various energy storage cycle coalescing engines that use the heat pump (1G) to recover the combustion gas (49) from an amount of heat of 900 degrees or less to the intake air (28a) by the recovery heat pump (1G) to recover the heat (52d).   Various energy storage cycle coalescing engines that use a heat pump (1G) to recover heat from 900 degrees C or less to intake air (28a) with a recovery heat pump (1G) to recover heat (52d).   Various energy storage cycle coalescing engines that use the heat pump (1G) to recover the amount of heat of compressed air (28b) by using the recovery heat pump (1G) and recover the heat by using the compressed water heat exchanger (2Y).   Various energy storage cycle coalescing engines that recover the heat of combustion gas (49) with a heat pump (1G) and recover heat with a compressed water heat exchanger (2Y) with a recovery heat pump (1G).   Various energy storage cycle coalescing engines that recover heat from the heat pump (1G) and heat from the compressed water heat exchanger (2Y) by the recovery heat pump (1G) to heat (52d).   High temperature mercury (1d) with heat pump (1G) Exhaust heat from around 220 ° C Intake air (28a) Recovered heat pump (1G) Recovers heat with compressed water heat exchanger (2Y) to heat (52d) Energy conservation cycle coalescence engine.   Compressed air heat amount (28b) from around 900 degrees with heat pump (1G) Various energy to recover heat to heat (52d) with intake air (28a) with recovered heat pump (1G) with compressed water heat exchanger (2Y) Conservation cycle coalescence organization.   Various energy from the combustion gas (49) by the heat pump (1G) to the heat (52d) by recovering heat from the intake air (28a) by the recovered heat pump (1G) by the compressed water heat exchanger (2Y) from around 900 degrees Celsius. Conservation cycle coalescence organization.   Various energy storage cycle coalescing engines that use a heat pump (1G) to recover heat from a temperature of about 900 ° C. with intake air (28a) with a recovery heat pump (1G) with a compressed water heat exchanger (2Y) to heat (52d).   Compressed air heat quantity (28b) from 900 degrees or more with heat pump (1G) Various energy that recovers heat to hot heat (52d) by intake water (28a) with recovered heat pump (1G) and compressed water heat exchanger (2Y) Conservation cycle coalescence organization.   Various energy from the combustion gas (49) with the heat pump (1G) to heat (52d) by recovering the heat with the intake air (28a) from the heat quantity of 900 degrees or more with the recovered heat pump (1G) with the compressed water heat exchanger (2Y) Conservation cycle coalescence organization.   Various energy storage cycle coalescing engines that use heat pump (1G) to recover heat from over 900 degrees Celsius with intake air (28a) with recovery heat pump (1G) with compressed water heat exchanger (2Y) and heat (52d).   Compressed air heat quantity (28b) from 900 degrees or less with heat pump (1G) Various energy to recover heat to compressed air (28a) with recovered heat pump (1G) with compressed water heat exchanger (2Y) to heat (52d) Conservation cycle coalescence organization.   Various energy from the combustion gas (49) with a heat pump (1G) from 900 degrees C or less to the intake air (28a) with the recovery heat pump (1G) with the compressed water heat exchanger (2Y) to recover the heat (52d) Conservation cycle coalescence organization.   Various energy storage cycle coalescing engines that use a heat pump (1G) to recover heat from a temperature of 900 ° C. or less to intake air (28a) using a recovered heat pump (1G) and a compressed water heat exchanger (2Y) to generate heat (52d).   High temperature mercury (1d) exhaust heat quantity with heat pump (1G) Recover heat pump (1G) with compression / reduction compression chamber mercury heat exchanger (2Z) to recover heat to heat (52d) .   Compressed air heat quantity (28b) by heat pump (1G), recovery energy pump (1G), and compression / reduction diameter compression chamber mercury heat exchanger (2Z) recovers heat to combine with various energy storage cycle engines (52d).   Various energy storage cycle coalescing engines that recover the combustion gas (49) by the heat pump (1G) and recover the heat (52d) by the compression / reduction compression chamber mercury heat exchanger (2Z) by the recovery heat pump (1G).   Various energy storage cycle coalescing engines that recover heat with a heat pump (1G) and heat with a recovery heat pump (1G) with a compression / reduction compression chamber mercury heat exchanger (2Z) to produce warm heat (52d).   High-temperature mercury (1d) with a heat pump (1G) The exhaust heat quantity from around 220 ° C. The intake air (28a) is recovered with a recovery heat pump (1G) with a compression / reduction compression chamber mercury heat exchanger (2Z). ) Various energy conservation cycle coalescing engines.   Compressed air calorie (28b) from around 900 degrees with heat pump (1G) Heat is recovered by suction air (28a) with recovery heat pump (1G) with compression-reduction compression chamber mercury heat exchanger (2Z) and warm (52d) Various energy conservation cycle coalescing engines.   Combustion gas (49) with a heat pump (1G), heat from around 900 degrees, intake air (28a) with a recovery heat pump (1G), heat recovery with a compression / reduction compression chamber mercury heat exchanger (2Z), and heat (52d) Various energy conservation cycle coalescing engines.   Various types of energy storage from about 900 degrees of heat with heat pump (1G) to intake air (28a) with recovery heat pump (1G) and heat recovery with compression / compression chamber mercury heat exchanger (2Z) to heat (52d) Cycle coalescence engine.   Compressed air calorie (28b) from 900 ° C. or higher with heat pump (1G), recovered heat pump (1G) with compression heat pump (1G), heat recovery with compression heat exchanger (2Z), and heat (52d) Various energy conservation cycle coalescing engines.   Combustion gas (49) with a heat pump (1G) from an amount of heat of 900 degrees or more, intake air (28a) with a recovery heat pump (1G), heat recovery with a compression / reduction compression chamber mercury heat exchanger (2Z), and heat (52d) Various energy conservation cycle coalescing engines.   Various types of energy storage from heat of 900 ° C or higher with heat pump (1G) to intake air (28a) with heat recovery heat pump (1G) with compression / reduction compression chamber mercury heat exchanger (2Z) to heat (52d) Cycle coalescence engine.   Compressed air calorie (28b) from 900 ° C. or less with heat pump (1G), intake heat (28a) with recovery heat pump (1G), heat recovery with compression / reduction compression chamber mercury heat exchanger (2Z), and heat (52d) Various energy conservation cycle coalescing engines.   Combustion gas (49) with a heat pump (1G) from an amount of heat of 900 degrees or less, intake air (28a) with a recovery heat pump (1G), heat recovery with a compression-reduction-compression chamber mercury heat exchanger (2Z), and heat (52d) Various energy conservation cycle coalescing engines.   Various types of energy storage from heat of less than 900 degrees with heat pump (1G) to intake air (28a) with recovery heat pump (1G) and heat recovery with compression / reduction compression chamber mercury heat exchanger (2Z) to heat (52d) Cycle coalescence engine.   Various energy storage cycle coalescing engines that recover high-temperature mercury (1d) exhaust heat with a heat pump (1G) and recover compression heat to drive all blade turbines (8X) to drive and propel.   Various energy storage cycle coalescing engines that recover the compressed air heat amount (28b) with a heat pump (1G) and recover the compression heat to drive all the blade turbines (8X) to drive and propulsion.   Various energy storage cycle coalescence engines that recover the combustion gas (49) calorie with the heat pump (1G) and recover the compression heat to drive the whole rotor blade turbine (8X) to drive and propel.   Various energy storage cycle coalescing engines that recover the amount of heat with a heat pump (1G) and recover the compression heat to drive the entire rotor blade turbine (8X) to drive injection propulsion.   Various energy storage cycle coalescing engines that use the heat pump (1G) to recover high-temperature mercury (1d) exhaust heat from around 220 degrees with the intake air (28a) to recover the compression heat and drive the entire rotor blade turbine (8X).   Various energy storage cycle coalescing engines that use the heat pump (1G) to recover the compressed air heat (28b) from about 900 degrees of compressed air heat (28b) using the intake air (28a) to drive the entire rotor blade turbine (8X) to drive and propel it.   Various energy storage cycle coalescing engines in which the combustion gas (49) with a heat pump (1G) recovers compression heat with intake air (28a) from about 900 degrees of heat and drives the whole rotor blade turbine (8X) to drive and propulsion.   Various energy storage cycle coalescing engines that use the heat pump (1G) to recover the recovered compression heat with intake air (28a) from around 900 degrees of heat to drive the whole rotor blade turbine (8X) to drive and propel it.   Various energy storage cycle coalescing engines that use the heat pump (1G) to recover the compressed air from the amount of compressed air heat (28b) of 900 degrees or more with the intake air (28a) to drive the entire rotor blade turbine (8X) to drive and propel it.   Various energy storage cycle coalescing engines in which the combustion gas (49) with a heat pump (1G) recovers compression heat with intake air (28a) from 900 ° C. or more and drives all blade turbines (8X) to drive and propel.   Various energy storage cycle coalescing engines that use the heat pump (1G) to recover the collected compression heat from intake air (28a) from 900 ° C. or more to drive and drive all blade turbines (8X).   Various energy storage cycle coalescing engines that use the heat pump (1G) to recover the compressed heat of the compressed air by the intake air (28a) from the air temperature (28b) of 900 ° C. or less to drive the entire rotor blade turbine (8X).   Various energy storage cycle coalescing engines in which the combustion gas (49) with a heat pump (1G) recovers compression heat with intake air (28a) from an amount of 900 ° C. or less to drive all blade turbines (8X) to drive and propel.   Various energy storage cycle coalescing engines that use the heat pump (1G) to recover the recovered compression heat from intake air (28a) from a temperature of 900 degrees or less to drive all the blade turbines (8X).   Various energy storage cycle coalescence engines that drive high-temperature mercury (1d) exhaust heat with a heat pump (1G) and compression heat with a recovery heat pump (1G) to drive all blade turbines (8X) to drive and propel.   Various energy storage cycle coalescing engines that use the heat pump (1G) to recover the amount of compressed air heat (28b) with the recovery heat pump (1G) to recover the compression blade heat (8X).   Various energy storage cycle coalescing engines in which the combustion gas (49) calorie is recovered by the heat pump (1G) and the compression heat is recovered by the recovery heat pump (1G) to drive the entire rotor blade turbine (8X) to drive and propulsion.   Various energy storage cycle coalescing engines that use the heat pump (1G) to recover the amount of heat with the recovery heat pump (1G) to recover the compression heat to drive the propeller turbine (8X).   Various types of high-pressure mercury (1d) exhaust heat quantity with a heat pump (1G) from about 220 degrees, and intake air (28a) is recovered with compression heat with a recovery heat pump (1G) to drive all blade turbines (8X) to drive injection propulsion Energy conservation cycle coalescence engine.   Compressed air heat (28b) from around 900 degrees with heat pump (1G) Various energy for intake air (28a) to recover compression heat with recovery heat pump (1G) and drive all blade turbine (8X) to drive injection propulsion drive Conservation cycle coalescence organization.   Combustion gas (49) with a heat pump (1G) The amount of heat is about 900 degrees, and the intake air (28a) recovers compression heat with a recovery heat pump (1G) to drive all blade turbines (8X) to drive injection propulsion drive Conservation cycle coalescence organization.   Various energy storage cycle coalescing engines that use the heat pump (1G) to recover the compression heat of the intake air (28a) from the recovered air pump (1G) from about 900 degrees Celsius and drive all the blade turbines (8X) to drive and propel them.   Compressed air heat (28b) from 900 ° C or higher with heat pump (1G), and recovery energy pump (1G) recovers compression heat from intake air (28a) to make all blade turbine (8X) drive injection propulsion drive Conservation cycle coalescence organization.   Various energies for driving and propulsion driving of all rotor blade turbines (8X) by recovering compression heat from combustion gas (49) with a heat pump (1G) and a suction heat (28a) using a recovery heat pump (1G) from 900 ° C. Conservation cycle coalescence organization.   Various energy storage cycle coalescing engines that use the heat pump (1G) to recover the compression heat of the intake air (28a) from the heat quantity of 900 ° C. or higher using the recovered heat pump (1G) to drive the entire rotor blade turbine (8X).   Compressed air heat (28b) from 900 degrees or less with heat pump (1G), various energy to recover the compression heat with recovered heat pump (1G) with intake air (28a) to drive all rotor blade turbine (8X) Conservation cycle coalescence organization.   Various energies for driving and propulsion driving of all rotor blade turbines (8X) by recovering compression heat from the combustion gas (49) with a heat pump (1G) from 900 ° C. or less to intake air (28a) with a recovery heat pump (1G) Conservation cycle coalescence organization.   Various energy storage cycle coalescing engines that use the heat pump (1G) to recover the compression heat of the intake air (28a) from the heat quantity of 900 degrees C or less by the recovered heat pump (1G) to drive the entire rotor blade turbine (8X) to drive and propel it.   Compressed air calorie (28b) is recovered by heat pump (1G) and heat is recovered by compressed water heat exchanger (2Y) by recovered heat pump (1G), and all blade turbine (8X) is driven and driven by propulsion. Cycle coalescence engine.   Various types of energy storage to make combustion blade (49) calorific value with heat pump (1G) and recover heat pump (1G) with compressed water heat exchanger (2Y) to make all blade turbine (8X) drive drive propulsion drive Cycle coalescence engine.   Various energy storage cycle combined engines that recover heat from a heat pump (1G) and recover heat from a compressed water heat exchanger (2Y) using a recovery heat pump (1G) to drive the whole rotor blade turbine (8X) to drive and propel it.   High temperature mercury (1d) with heat pump (1G) Exhaust calorific value from around 220 ° C. Intake air (28a) with recovery heat pump (1G) with heat recovery with compressed water heat exchanger (2Y), all rotor blade turbine (8X) Various energy storage cycle coalescing engines that make the drive injection propulsion drive.   Compressed air calorie (28b) from around 900 degrees with heat pump (1G) From intake air (28a), recovered heat pump (1G) recovers heat with compressed water heat exchanger (2Y), and complete rotor blade turbine (8X) Various energy storage cycle coalescing engine with driving injection propulsion drive.   The combustion gas (49) with a heat pump (1G) recovers heat with an intake air (28a) from around 900 ° C. with a recovery heat pump (1G) and with a compressed water heat exchanger (2Y) to recover an all blade turbine (8X). Various energy storage cycle coalescing engine with driving injection propulsion drive.   Heat pump (1G) recovers heat from around 900 degrees of intake air (28a), recovered heat pump (1G) recovers heat with compressed water heat exchanger (2Y), and drives all blade turbine (8X) to drive jet propulsion Various energy conservation cycle coalescing engines.   Compressed air calorie (28b) from 900 degrees or more with heat pump (1G), intake air (28a) with recovered heat pump (1G), heat recovery with compressed water heat exchanger (2Y), and all rotor blade turbine (8X) Various energy storage cycle coalescing engine with driving injection propulsion drive.   The heat pump (1G) recovers heat from the combustion gas (49) with an intake air (28a) from a heat quantity of 900 ° C. or more, and the recovered heat pump (1G) recovers heat with the compressed water heat exchanger (2Y), thereby Various energy storage cycle coalescing engine with driving injection propulsion drive.   Heat pump (1G) heats from over 900 degrees, intake air (28a) recovers heat pump (1G) recovers heat with compressed water heat exchanger (2Y), drives all blade turbine (8X) to drive jet propulsion drive Various energy conservation cycle coalescing engines.   Compressed air calorie (28b) from 900 degrees or less with heat pump (1G) Recover heat pump (1G) with recovered heat pump (1G) with compressed water heat exchanger (2Y) to recover all blade turbine (8X) Various energy storage cycle coalescing engine with driving injection propulsion drive.   The heat pump (1G) recovers heat from the combustion gas (49) from an amount of heat of 900 ° C. or less to the intake air (28a), the recovered heat pump (1G) recovers heat from the compressed water heat exchanger (2Y), and the whole rotor blade turbine (8X) Various energy storage cycle coalescing engine with driving injection propulsion drive.   The heat pump (1G) heats up to 900 degrees Celsius or less, the intake air (28a) recovers heat with the recovered heat pump (1G), and the compressed water heat exchanger (2Y) recovers heat to drive the all blade turbine (8X) to drive injection propulsion. Various energy conservation cycle coalescing engines.   High-temperature mercury (1d) exhaust heat quantity is recovered by heat pump (1G) and heat recovery is performed by compression heat pump (1G) by compression / reduction compression chamber mercury heat exchanger (2Z) to drive all blade turbine (8X) Various energy conservation cycle coalescing engines.   Compressed air heat quantity (28b) is recovered by heat pump (1G) and recovered heat pump (1G) is heat recovered by compression / reduction compression chamber mercury heat exchanger (2Z) to drive all blade turbine (8X) to drive injection propulsion Various energy conservation cycle coalescing engines.   The combustion gas (49) calorie is recovered by the heat pump (1G), and the recovery heat pump (1G) recovers the heat by the compression / reduction compression chamber mercury heat exchanger (2Z) to drive the all rotor blade turbine (8X) to drive injection propulsion. Various energy conservation cycle coalescing engines.   Recover energy with heat pump (1G) Heat recovery with compression heat pump (1G) with compression / reduction compression chamber mercury heat exchanger (2Z) to make all blade turbines (8X) drive and propulsion drive various energy storage cycles Combined organization.   High temperature mercury (1d) with heat pump (1G), exhaust heat from around 220 degrees, intake air (28a) with recovery heat pump (1G), heat recovery with compression / reduction compression chamber mercury heat exchanger (2Z), and all moving blades Various energy storage cycle coalescing engines that use the turbine (8X) as a driving injection propulsion drive.   Compressed air calorie (28b) from around 900 degrees with heat pump (1G), intake air (28a) with recovery heat pump (1G), heat recovery with compression reduced diameter compression chamber mercury heat exchanger (2Z), and full blade turbine Various energy storage cycle coalescing engines that use (8X) as drive injection propulsion drive.   Combustion gas (49) with a heat pump (1G) from about 900 degrees Celsius, intake air (28a) is recovered with a recovery heat pump (1G), heat is recovered with a compression-reduction-compression chamber mercury heat exchanger (2Z), and a full blade turbine Various energy storage cycle coalescing engines that use (8X) as drive injection propulsion drive.   The heat pump (1G) recovers heat from around 900 degrees of intake air (28a) with the recovery heat pump (1G) and the heat with the compression / shrinkage compression chamber mercury heat exchanger (2Z) to drive the entire blade turbine (8X) Various energy storage cycle coalescing engines that are driven by injection propulsion.   Compressed air calorie (28b) from 900 degrees or more with heat pump (1G) Recovered heat pump (1G) with compression heat pump (1G), heat recovery with compression heat exchanger (2Z), and full blade turbine Various energy storage cycle coalescing engines that use (8X) as drive injection propulsion drive.   Combustion gas (49) with a heat pump (1G) from a heat quantity of 900 degrees or more, intake air (28a) with a recovery heat pump (1G), heat recovery with a compression / reduction compression chamber mercury heat exchanger (2Z), and a full rotor blade turbine Various energy storage cycle coalescing engines that use (8X) as drive injection propulsion drive.   The heat pump (1G) recovers heat from over 900 degrees of heat from the intake air (28a) by the recovery heat pump (1G) and the compression / shrinkage compression chamber mercury heat exchanger (2Z) to drive the all blade turbine (8X) Various energy storage cycle coalescing engines that are driven by injection propulsion.   Compressed air calorie (28b) from 900 degrees or less with heat pump (1G), intake air (28a) with recovered heat pump (1G), heat recovery with compression reduced diameter compression chamber mercury heat exchanger (2Z), and full blade turbine Various energy storage cycle coalescing engines that use (8X) as drive injection propulsion drive.   Combustion gas (49) with a heat pump (1G) from an amount of heat of 900 degrees C or less, intake air (28a) with a recovery heat pump (1G), heat recovery with a compression / reduction compression chamber mercury heat exchanger (2Z), and a full rotor blade turbine Various energy storage cycle coalescing engines that use (8X) as drive injection propulsion drive.   The heat pump (1G) heats up to 900 degrees Celsius or less, and the intake air (28a) recovers the heat with the recovery heat pump (1G) with the compression / reduction compression chamber mercury heat exchanger (2Z) to drive the all blade turbine (8X). Various energy storage cycle coalescing engines that are driven by injection propulsion.   Various energy storage cycle coalescing engines that recover high-temperature mercury (1d) exhaust heat with a heat pump (1G) and recover it to compression heat to produce ice-cooled heat (52e).   Combined engine for various energy storage cycles that collects heat of compressed air (28b) with a heat pump (1G) and recovers heat of compression to produce ice-cooled heat (52e).   Various energy storage cycle coalescing engines that recover the combustion gas (49) calorie with a heat pump (1G) and recover it to ice-cooled heat (52e).   Various energy storage cycle coalescence engine which collects heat quantity with heat pump (1G) and recovers compression heat to make ice cold heat (52e).   Various energy storage cycle coalescing engines that recover high-temperature mercury (1d) exhaust heat by using a heat pump (1G) from around 220 degrees of intake air (28a) and recover the compression heat to ice-cold heat (52e).   Various energy storage cycle coalescing engines that recover heat from compressed air by the intake air (28a) from about 900 degrees of compressed air heat (28b) with a heat pump (1G) to produce ice-cold heat (52e).   Various energy storage cycle coalesced engines that use the heat pump (1G) to recover the combustion gas (49) from about 900 degrees Celsius using the intake air (28a) and recover the compression heat to ice-cold heat (52e).   Various energy storage cycle coalescing engines that recover heat from around 900 degrees of heat with a heat pump (1G), recovering compression heat with intake air (28a), and making ice-cooled heat (52e).   Various energy storage cycle coalescing engines that recover heat from compressed air by using a heat pump (1G) from 900 ° C. or higher using intake air (28a) to recover ice-cooled heat (52e).   Various energy storage cycle coalesced engines that use a heat pump (1G) to recover combustion heat (900) from 900 ° C or higher with intake air (28a) to recover ice compression heat (52e).   Various energy storage cycle coalesced engines that recover heat of compression and heat by suction air (28a) from an amount of heat of 900 ° C or higher with a heat pump (1G) to produce ice-cold heat (52e)   Various energy storage cycle coalescing engines that recover heat from compressed air by using a heat pump (1G), recovering compressed heat from intake air (28a) from 900 degrees or less (28b) to ice-cooled heat (52e).   Various energy storage cycle coalesced engines that use the heat pump (1G) to recover the combustion gas (49) from the heat quantity of 900 degrees or less with the intake air (28a) to recover the ice compression heat (52e).   Various energy storage cycle coalescing engines that recover heat of compression and heat with suction air (28a) from an amount of heat of 900 degrees or less with a heat pump (1G) to produce ice-cold heat (52e).   Various energy storage cycle coalescing engines that convert high-temperature mercury (1d) exhaust heat with a heat pump (1G) into compression heat with a recovery heat pump (1G) to produce ice-cooled heat (52e).   Various energy storage cycle coalescing engines that use the heat pump (1G) to recover the amount of compressed air heat (28b) with the recovery heat pump (1G) to recover the ice-cooled heat (52e).   Various energy storage cycle coalescing engines that use the heat pump (1G) to recover the combustion gas (49) calorie by the recovery heat pump (1G) to recover the ice-cooled heat (52e).   Various energy storage cycle coalescing engines that use the heat pump (1G) to recover the amount of heat by using the recovery heat pump (1G) to recover the compression heat to ice-cold heat (52e).   Various energy storage cycle coalescing engines that use high-temperature mercury (1d) with a heat pump (1G) and exhaust heat from around 220 degrees to recover compression heat with intake heat (28a) with a recovery heat pump (1G) to produce ice-cold heat (52e).   Various energy storage cycle coalesced engines that use compressed heat to recover ice heat (52e) by using a recovery heat pump (1G) with intake air (28a) from around 900 degrees of heat of compressed air (28b) with a heat pump (1G).   Various energy storage cycle coalescing engines that use the heat pump (1G) to recover the combustion gas (49) from about 900 degrees Celsius and the intake air (28a) with the recovery heat pump (1G) to recover the compression heat to ice-cold heat (52e).   Various energy storage cycle coalescing engines that use a heat pump (1G) to recover heat from around 900 degrees Celsius by suction air (28a) with a recovery heat pump (1G) to recover ice-cooled heat (52e).   Various energy storage cycle coalescing engines that recover heat of compression air by using a recovery heat pump (1G) from an intake air (28a) from 900 ° C. or higher with a heat pump (1G) and an ice-cooled heat (52e).   Various energy storage cycle coalescing engines that use a heat pump (1G) to recover combustion gas (49) from an amount of heat of 900 ° C. or higher to intake air (28a) by a recovery heat pump (1G) to recover ice-cooled heat (52e).   Various energy storage cycle coalescing engines that use a heat pump (1G) to recover heat from over 900 degrees Celsius by suction air (28a) and recovery heat pump (1G) to recover ice-cooled heat (52e).   Various energy storage cycle coalescing engines that use compressed heat to recover the ice-cooled heat (52e) by using the recovered heat pump (1G) with the intake air (28a) from below 900 degrees of heat of compressed air (28b) with the heat pump (1G).   Various energy storage cycle coalescing engines that use the heat pump (1G) to recover the combustion gas (49) from an amount of heat of 900 ° C. or less to the intake air (28a) with the recovery heat pump (1G) to recover the ice-cooled heat (52e).   Various energy storage cycle coalescing engines that use the heat pump (1G) to recover the heat of compression from the heat quantity of 900 degrees C or less with the recovered heat pump (1G) using the intake air (28a) to produce ice-cold heat (52e).   Various energy storage cycle coalescing engines that use the heat pump (1G) to recover the heat of compressed air (28b) using the recovery heat pump (1G) and the heat recovered by the compressed water heat exchanger (2Y) to produce ice-cooled heat (52e).   Various energy storage cycle coalescing engines that use the heat pump (1G) to recover the heat of the combustion gas (49) by using the recovery heat pump (1G) and the heat from the compressed water heat exchanger (2Y) to produce ice-cooled heat (52e).   Various energy storage cycle coalescing engines that recover heat with a heat pump (1G) and heat with a compressed water heat exchanger (2Y) with a recovery heat pump (1G) to produce ice-cooled heat (52e).   High temperature mercury (1d) with heat pump (1G), exhaust heat from around 220 degrees, intake air (28a) with recovery heat pump (1G), heat recovery with compressed water heat exchanger (2Y), and ice cooling (52e) Various energy conservation cycle coalescence engine.   Compressed air calorie (28b) from around 900 degrees with heat pump (1G) Various types of heat is collected from intake air (28a) with recovered heat pump (1G) with compressed water heat exchanger (2Y) to produce ice-cooled heat (52e) Energy conservation cycle coalescence engine.   Various kinds of heat from the combustion gas (49) with a heat pump (1G) from about 900 ° C., intake air (28a), recovered heat pump (1G) with compressed water heat exchanger (2Y), and ice-cooled (52e) Energy conservation cycle coalescence engine.   Various energy storage cycle coalescence engine from about 900 degrees of heat with heat pump (1G) to intake air (28a) with recovered heat pump (1G) with compressed water heat exchanger (2Y) to recover ice-cooled heat (52e) .   Compressed air heat (28b) from 900 degrees or more with heat pump (1G) Various types of intake air (28a) recovers heat with compressed water heat exchanger (2Y) with recovered heat pump (1G) to make ice cold heat (52e) Energy conservation cycle coalescence engine.   Various kinds of heat from the combustion gas (49) with a heat pump (1G) of 900 ° C. or more to the intake air (28a), the recovered heat pump (1G) with the compressed water heat exchanger (2Y), and the ice-cooled heat (52e). Energy conservation cycle coalescence engine.   Various energy storage cycle coalescing engines that use a heat pump (1G) to generate heat from 900 degrees Celsius or higher and intake air (28a) with a recovery heat pump (1G) with a compressed water heat exchanger (2Y) to recover ice-cooled heat (52e) .   Compressed air heat amount (28b) from 900 degrees or less with heat pump (1G) Various types of intake air (28a) recover heat with compressed water heat exchanger (2Y) with recovered heat pump (1G) to make ice cold heat (52e) Energy conservation cycle coalescence engine.   Various kinds of heat from a combustion gas (49) with a heat pump (1G) from 900 ° C. or less to an intake air (28a) with a recovery heat pump (1G) with a compressed water heat exchanger (2Y) to produce ice-cooled heat (52e) Energy conservation cycle coalescence engine.   Various energy storage cycle coalescing engines that use heat pump (1G) to heat from 900 degrees C or less to intake air (28a), recover heat pump (1G) with compressed water heat exchanger (2Y), and use ice-cooled heat (52e) .   Combined with various energy storage cycles to recover high-temperature mercury (1d) exhaust heat with heat pump (1G) and recovery heat pump (1G) with compression / reduction compression chamber mercury heat exchanger (2Z) to produce ice-cold heat (52e) organ.   Compressed air heat (28b) with heat pump (1G) Recovered heat pump (1G) with compression / reduction diameter compression chamber Mercury heat exchanger (2Z) recovers heat to ice-cooled heat (52e) Combined engine .   Various energy storage cycle coalescence engines that recover the combustion gas (49) calorie with the heat pump (1G) and recover the heat with the compression / reduction compression chamber mercury heat exchanger (2Z) with the recovery heat pump (1G) to ice-cold heat (52e) .   Various energy storage cycle coalescing engines that recover heat with a heat pump (1G) and heat with a recovery heat pump (1G) with a compression / reduction compression chamber mercury heat exchanger (2Z) to produce ice-cooled heat (52e).   High-temperature mercury (1d) with a heat pump (1G) from about 220 degrees of exhaust heat, intake air (28a) is recovered with a recovery heat pump (1G) with a compression / reduction compression chamber mercury heat exchanger (2Z), and ice-cold heat ( 52e) Various energy storage cycle coalescing engines.   Compressed air calorie (28b) from around 900 degrees with heat pump (1G), intake air (28a) with recovery heat pump (1G), heat recovery with compression-reduction compression chamber mercury heat exchanger (2Z), and ice-cold heat (52e) ) Various energy conservation cycle coalescing engines.   With the heat pump (1G), the combustion gas (49) is heated from about 900 degrees Celsius with the intake air (28a) and with the recovery heat pump (1G) with the compression-reduction compression chamber mercury heat exchanger (2Z) to recover the ice cold heat (52e ) Various energy conservation cycle coalescing engines.   Various energy from about 900 degrees of heat with a heat pump (1G) to intake air (28a) with a recovery heat pump (1G) and heat recovery with a compression / reduction compression chamber mercury heat exchanger (2Z) to produce ice-cold heat (52e) Conservation cycle coalescence organization.   Compressed air calorie (28b) from 900 ° C. or higher with heat pump (1G), intake heat (28a) with recovery heat pump (1G), heat recovery with compression-reduction compression chamber mercury heat exchanger (2Z), and ice-cold heat (52e) ) Various energy conservation cycle coalescing engines.   With the heat pump (1G), the combustion gas (49) is heated from 900 degrees Celsius or higher with the intake air (28a), with the recovery heat pump (1G) with the compression-reduction compression chamber mercury heat exchanger (2Z) to recover the ice-cold heat (52e). ) Various energy conservation cycle coalescing engines.   Various energy from the heat quantity of 900 ° C or more with heat pump (1G) to intake air (28a) with recovery heat pump (1G) and heat recovery with compression / reduction compression chamber mercury heat exchanger (2Z) to make ice cold heat (52e) Conservation cycle coalescence organization.   Compressed air calorie (28b) from 900 ° C. or less with heat pump (1G) Recovered heat pump (1G) with compression heat pump (1G) using compression heat exchanger (2Z) to recover ice-cooled heat (52e) ) Various energy conservation cycle coalescing engines.   With the heat pump (1G), the combustion gas (49) is heated to 900 ° C. or less, and the intake air (28a) is recovered with the recovery heat pump (1G) with the compression-reduction compression chamber mercury heat exchanger (2Z), and the ice-cold ) Various energy conservation cycle coalescing engines.   Various energy from the heat quantity of 900 ° C or less with the heat pump (1G) to the intake air (28a) with the recovery heat pump (1G) and the heat recovery with the mercury heat exchanger (2Z) in the compression / reduction chamber to make the ice cold heat (52e) Conservation cycle coalescence organization.   Various energy storage cycle coalescing engines that collect high-temperature mercury (1d) exhaust heat with a heat pump (1G) and recover compression heat to superheated steam temperature (52d).   Various energy storage cycle coalescing engines that recover the amount of compressed air heat (28b) with a heat pump (1G) and recover the compression heat to superheated steam temperature (52d).   Various energy storage cycle coalescing engines that recover the combustion gas (49) calorie with a heat pump (1G) and recover the compression heat to superheated steam temperature (52d).   Various energy storage cycle coalescence engine which recovers heat quantity with heat pump (1G) and recovers compression heat to superheated steam temperature (52d).   Various energy storage cycle coalescing engines that recover high-temperature mercury (1d) with a heat pump (1d) from about 220 degrees of exhaust heat and recover the compression heat with intake air (28a) to produce superheated steam temperature (52d).   Various energy storage cycle coalescence engine which recovers compression heat with intake air (28a) from about 900 degrees of heat of compressed air (28b) with heat pump (1G) and converts to superheated steam temperature (52d).   Various energy storage cycle coalesced engines that use the heat pump (1G) to recover the combustion gas (49) from about 900 degrees of heat with the intake air (28a) and recover the compression heat to the superheated steam temperature (52d).   Various energy storage cycle coalescing engines that recover heat from around 900 degrees of heat with a heat pump (1G) and recover heat from compressed air with intake air (28a) to produce superheated steam temperature (52d).   Various energy storage cycle coalescing engines that recover heat from compressed air by using a heat pump (1G) from over 900 degrees of compressed air heat (28b) with intake air (28a) to generate superheated steam temperature (52d).   Various energy storage cycle coalesced engines that use the heat pump (1G) to recover the combustion gas (49) from an amount of heat of 900 degrees or more with the intake air (28a) and recover the compression heat to the superheated steam temperature (52d).   Various energy storage cycle coalescing engines that recover heat from over 900 degrees of heat with a heat pump (1G) and recover the compressed heat with intake air (28a) to produce superheated steam temperature (52d).   Various energy storage cycle coalescing engines that recover heat from compressed air by using a heat pump (1G) and recover heat from compressed air by using intake air (28a) from 900 degrees or less (28b).   Various energy storage cycle coalesced engines that use the heat pump (1G) to recover the combustion gas (49) from an amount of heat of 900 degrees or less with the intake air (28a) and recover the compression heat to the superheated steam temperature (52d).   Various energy storage cycle coalescing engines that recover heat from compressed air from intake air (28a) to heat superheated steam (52d) from heat of 900 degrees or less with heat pump (1G).   Various energy storage cycle coalescing engines that convert high-temperature mercury (1d) exhaust heat with a heat pump (1G) to compression heat with a recovery heat pump (1G) to produce superheated steam temperature (52d).